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STATISTICAL ANALYSIS OF WIND LOADINGS AND RESPONSES

OF A TRANSMISSION TOWER STRUCTURE

by SIEW HOCK LIEW, B.S.

A DISSERTATION

IN

CIVIL ENGINEERING

Submitted to the Graduate Faculty of Texas Tech University in Partial Fulfillment of the Requirements for the Degree of DOCTOR OF PHILOSOPHY

Approved

Accepted

May, 1988 ©1989

SIEW HOCK LIEW

All Rights Reserved ACKNOWLEDGMENTS

I wish to express my deepest appreciation to my committee chairman. Dr. H. Scott Norville, for his confi­ dence in me during the entire course of this researcr. project. His encouragement and valuable advice as a committee chairman, as a major advisor, and as a friend, has instilled a value of perseverance in me. I also ^-'ish to express my sincere appreciation to Dr. K. C. M^?nt^^, for his expertise and advice in wind engineering, to Dr. T. 0. Lewis for his advice in and in , to Dr. W. P. Vann and Dr. E. Blair for t-heir valuable suggestions and comments on this dissertation manuscript, and to Mr. M. L. Levitan for his permisf5ion to use some of the time histories plots. I am most grateful to my wife, Lily, for her patience and understanding throughout the course of my graduate work, and to my parents for their moral support -^nd instilling in me the value of education from the very beginning of my life.

11 TABLE OF CONTENTS

PAGE

ACKNOWLEDGMENTS i i

LIST OF TABLES vi

LIST OF FIGURES vii

1. INTRODUCTION 1

2. LITERATURE REVIEW 7

3. SITE DESCRIPTION, INSTRUMENTATION, AND

DATA COLLECTION SYSTEM 20 3.1 Introduction 20

3.2 Location 20

3.3 Instrumentation 27

4. STATISTICAL ANALYSIS OF TIME SERIES RECORD 35

4.1 Introduction 35

4.2 Data Handling 36

4.3 Time Series Analysis 38

4.4 Stationarity of a Time Series 43 4.5 Selected Time Histories 48

4.6 of Selected Time Histories 61 4.7 Cross Correlation of Selected Time Histories 79 4.S Discussion of Results 119

5. FREQUENCY DOMAIN ANALYSIS OF SINGLE

LOAD AND SINGLE RESPONSE SYSTEM 127

5.1 Introduction 127

i i i PAGE 5.2 Transfer Function Relating Loads With Responses 128

5.3 Power Spectra of Time Series 131

5.4 Cross Spectra of Bivariate Time Series 142 5.5 Frequency Response Function of a Linear System 146 5.6 Illustration and Applications of Frequency Response Function 149 5.6.1 Power Spectra Plots for Selected Time Histories 149 5.6.2 Frequency Response Function of Transmission Tower 163 5.6.3 Coherence Function of Transmission Tower 191 5.7 Conclusions and Discussion of Results 212

6. FREQUENCY RESPONSE FUNCTION OF MULTIPLE INPUTS AND A SINGLE OUTPUT 218 6.1 Introduction 218 6.2 General Requirements 220 6.3 Frequency Response Function Relating Two Loadings and One Response 223 6.4 Numerical Examples of Transmission Tower Subjected to Two Loadings and One Response 231 6.5 Discussion of Results 246

7. TIME SERIES ANALYSIS AND MODELING 252

7.1 Introduction 252 7.2 Definition of a Time Series 252

IV PAGE 7.3 Concept in Time Series Modeling 255 7.4 Models for Stationary and Nonstationary Time Series 258

7.5 Power Spectrum of a Linear Process 273 7.6 Numerical Examples of Time Series Modeling 277 7.6.1 Time Series Models 277 7.6.2 Power Spectra of Modeled Time Series 280

7.7 Discussion of Results 281

8. CONCLUSION 283 LIST OF REFERENCES 290 APPENDICES 297 A. TIME HISTORIES PLOTS 298 B. AUTOCORRELATION FUNCTIONS 324 C. CROSS CORRELATION FUNCTIONS 332 D. POWER SPECTRA 355 E. FREQUENCY RESPONSE FUNCTION 376

F. COHERENCE FUNCTION 399 G. MOVING AVERAGE PARAMETERS 411 LIST OF TABLES

TABLE PAGE

3.1 Twenty Three Segments of Data 21

3.2 File Description in Mode 22 28

4.1 Selected Records for Analysis 49

4.2 Load Values From The Conductors (kN) 56 4.3 Mean Swing Angles (Degrees) 56 4.4 Mean Transverse Load Values From the Conductors (kN) 57 4.5 Mean Longitudinal Load Values From the Conductors (kN) 57 4.6 Mean Leg Stresses of the Transmission Tower Due to Wind and Total Conductor Loads (MPa) 58 5.1 Lag aind Spectral Windows (Jenkins and Watts, 1968) 137 5.2 Properties of Spectral Windows (Jenkins and Watts, 1968) 140 7.1 General Models 271 7.2 Identification of Time Series Models 279 7.3 Chi-Square Statistics of the Autocorrelation of the Residuals 279

VI LIST OF FIGURES

FIGURE PAGE 3.1 Topography of Site and Orientation of Power Lines 22 3.2 Elevation Along the Test Line (Vertical Scale Exaggerated) 25 3.3 Schematic of Tower 16/4 26

3.4 Schematic Locations of Strain Gages Designated by the Corners of the Tower 32 4.1 Twenty Three Available Wind Records 37

4.2 Methodology for Time Series Analysis 39 4.3a Time History for Wind Speed at 34.7 m for Record N05 51 4.3b Time History for Wind Speed at 34.7 m for Record N07 51 4.4a Time History for Wind Speed at 34.7 m for Record NOS 52 4.4b Time History for Wind Speed at 34.7 m for Record N16 52 4.5 Locations of Selected Strain Gages for Analysis 55 4.6a Autocorrelation Functions of Original and First Differenced Series of WS05 for Record N05 63 4.6b Autocorrelation Functions of Original and First Differenced Series of WS05 for Record NOS 63 4.7a Autocorrelation Functions of LC03 for Record N05 65 4.7b Autocorrelation Functions of First Differenced Series of LC03 for Record N05 65

vii FIGURE PAGE 4.8a Autocorrelation Functions of LC04 for Record N05 67 4.8b Autocorrelation Functions of First Differenced Series of LC04 for Record N05 67 4.9a Autocorrelation Functions of LC05 for Record NOS 68 4.9b Autocorrelation Functions of First Differenced Series of LC05 for Record N05 68 4.lOa Autocorrelation Functions of Original and First Differenced Series of LC03 for Record NOS 69 4.lOb Autocorrelation Functions of Original and First Differenced Series of LC04 for Record NOS 69 4.11 Autocorrelation Functions of Original and First Differenced Series of LC05 for Record NOS 71 4.12a Autocorrelation Functions of Original and First Differenced Series of SG05 for Record N05 73 4.12b Autocorrelation Functions of Original and First Differenced Series of SGll for Record N05 73 4.13a Autocorrelation Functions of Original and First Differenced Series of SG06 for Record NOS 75 4.13b Autocorrelation Functions of Original and First Differenced Series of SG12 for Record NOS 75 4.14a Autocorrelation Functions of Original and First Differenced Series of SG05 for Record NOS 76

VI 1 1 FIGURE PAGE 4.14b Autocorrelation Functions of Original and First Differenced Series of SGll for Record NOS 76

4.ISa Autocorrelation Functions of Original and First Differenced Series of SG06 for Record NOS 77

4.15b Autocorrelation Functions of Original and First Differenced Series of SG12 for Record NOS 77

4.16a Cross Correlation Functions of WS05 and SG05 for Record NOS 83 4.16b Cross Correlation Functions of WS05 and SG06 for Record NOS S3 4.17a Cross Correlation Functions of WS05 and SG05 for Record NOS 85 4.17b Cross Correlation Functions of WS05 and SGll for Record NOS 85 4.ISa Cross Correlation Functions of WSOS and SG06 for Record NOS 86 4.18b Cross Correlation Functions of WSOS and SG12 for Record NOS 86 4.19a Cross Correlation Functions of Total Load Values From West Conductor and SGOS for Record NOS 90 4.19b Cross Correlation Functions of Total Load Values From West Conductor and SG06 for Record NOS 90

4.20a Cross Correlation Functions of Total Load Values From East Conductor and SGOS for Record NOS 91 4.20b Cross Correlation Functions of Total Load Values From East Conductor and SG06 for Record N05 91

IX FIGURE PAGE 4.21a Cross Correlation Functions of Total Load Values From Center Conductor and SGOS for Record NOS 92

4.21b Cross Correlation Functions of Total Load Values From Center Conductor and SG06 for Record NOS 92

4.22a Cross Correlation Functions of Total Load Values From West Conductor and SGOS for Record NOS 94

4.22b Cross Correlation Functions of Total Load Values From West Conductor and SG06 for Record NOS 94 4.23a Cross Correlation Functions of Total Load Values From West Conductor and SGll for Record NOS 96 4.23b Cross Correlation Functions of Total Load Values From West Conductor and SG12 for Record NOS 96 4.24a Cross Correlation Functions of Total Load Values From East Conductor auid SGOS for Record NOS 97 4.24b Cross Correlation Functions of Total Load Values From East Conductor and SG06 for Record NOS 97 4.2Sa Cross Correlation Functions of Total Load Values From East Conductor and SGll for Record NOS 98 4.25b Cross Correlation Functions of Total Load Values From East Conductor and SG12 for Record NOS 98

4.26a Cross Correlation Functions of Total Load Values From Center Conductor and SGOS for Record NOS 100 FIGURE PAGE 4.26b Cross Correlation Functions of Total Load Values From Center Conductor and SG06 for Record NOS 100 4.27a Cross Correlation Functions of Longitudinal Load Values From West Conductor and SGll for Record NOS 103 4.27b Cross Correlation Functions of Longitudinal Load Values From West Conductor and SG12 for Record NOS 103 4.2Sa Cross Correlation Functions of Longitudinal Load Values From East Conductor and SGll for Record NOS 104 4.2Sb Cross Correlation Functions of Longitudinal Load Values From East Conductor and SG12 for Record NOS 104 4.29a Cross Correlation Functions of Longitudinal Load Values From West Conductor and SGOS for Record NOS 106 4.29b Cross Correlation Functions of Longitudinal Load Values From West Conductor and SG12 for Record NOS 106 4.30a Cross Correlation Functions of Longitudinal Load Values From East Conductor and SGOS for Record NOS 107 4.30b Cross Correlation Functions of Longitudinal Load Values From East Conductor and SGll for Record NOS 107 4.31a Cross Correlation Functions of Longitudinal Load Values From Center Conductor and SGOS for Record NOS 108 4.31b Cross Correlation Functions of Longitudinal Load Values From Center Conductor and SGI2 for Record NOS 108

XI FIGURE PAGE 4.32a Cross Correlation Functions of Transverse Load Values From West Conductor and SGOS for Record NOS 110 4.32b Cross Correlation Functions of Transverse Load Values From West Conductor and SGll for Record NOS 110 4.33a Cross Correlation Functions of Transverse Load Values From East Conductor and SGOS for Record NOS 112 4.33b Cross Correlation Functions of Transverse Load Values From East Conductor and SGll for Record NOS 112 4.34a Cross Correlation Functions of Transverse Load Values From Center Conductor and SGOS for Record NOS 113 4.34b Cross Correlation Functions of Transverse Load Values From Center Conductor and SGI2 for Record NOS 113 4.3Sa Cross Correlation Functions of Transverse Load Values From West Conductor and SGOS for Record NOS 115 4.3Sb Cross Correlation Functions of Transverse Load Values From West Conductor and SGll for Record NOS 115 4.36a Cross Correlation Functions of Transverse Load Values From East Conductor and SGOS for Record NOS 116 4.36b Cross Correlation Functions of Transverse Load Values From Center Conductor and SGOS for Record NOS 116 4.37a Cross Correlation Functions of Transverse Load Values From Center Conductor and SGOS for Record NOS US

Xll FIGURE PAGE 4.37b Cross Correlation Functions of Transverse Load Values From Center Conductor and SGI2 for Record NOS 118

5.1 Schematic Representation of a Linear System Subjected to a Single Load and a Single Response 129

5.2a Plot of Lag Windows From Table 5.1 (Jenkins and Watts, 1968) 138 5.2b Plot of Spectral Windows From Table 5.1 (Jenkins and Watts, 1968) 138 S.3a Power Spectrum of Wind Speed at 34.7 m for Record NOS 151 S.3b Power Spectrum of Wind Speed at 34.7 m for Record NOS 151 S.4a Power Spectrum of Transverse Load From West Conductor for Record NOS 153 5.4b Power Spectrum of Transverse Load From East Conductor for Record NOS 153 S.Sa Power Spectrum of Transverse Load From West Conductor for Record NOS 154 S.Sb Power Spectrum of Transverse Load From East Conductor for Record NOS 154 S.Sa Power Spectrum of Transverse Load From Center Conductor for Record NOS 156 5.6b Power Spectrum of Transverse Load From Center Conductor for Record NOS 156 5.7a Power Spectrum of Main Strain Gage Located at SE Corner for Record NOS 159 5.7b Power Spectrum of Main Strain Gage Located at NW Corner for Record NOS 159 S.Sa Power Spectrum of Main Strain Gage Located at SE Corner for Record NOS 161 xi i i FIGURE PAGE

S.Sb Power Spectrum of Main Strain Gage Located at NW Corner for Record NOS 161 5.9a Frequency Response Function Relating Wind Speed and SE Diagonal Leg Strain Record for Record NOS 165 5.9b Frequency Response Function Relating Wind Speed and NW Diaigonal Leg Strain Record for Record NOS 165

5.10a Frequency Response Function Relating Wind Speed and SE Main Leg Strain Record for Record NOS 167

5.10b Frequency Response Function Relating Wind Speed and SE Main Leg Strain Record for Record NOS 167 5.11a Frequency Response Function Relating Wind Speed and SE Diagonal Leg Strain Record for Record NOS 168 5.lib Frequency Response Function Relating Wind Speed and NW Diagonal Leg Strain Record for Record NOS 168

5. 12a Frequency Response Function Relating Total Load From East Conductor and SE Main Leg Strain Record for Record NOS 170 5.12b Frequency Response Function Relating Total Load From East Conductor and NW Main Leg Strain Record for Record NOS 170

5. 13a Frequency Response Function Relating Total Load From East Conductor and SE Diagonal Leg Strain Record for Record NOS 172

S. 13b Frequency Response Function Relating Total Load From East Conductor and NW Diagonal Leg Strain Record for Record NOS 172

5. 14a Frequency Response Function Relating Total Load From Center Conductor and SE Main Leg Strain Record for Record NOS 173

xiv FIGURE PAGE 5. 14b Frequency Response Function Relating Total Load From Center Conductor and NW Main Leg Strain Record for Record NOS 173

5.15a Frequency Response Function Relating Total Load From West Conductor and SE Main Leg Strain Record for Record NOS 174 5.15b Frequency Response Function Relating Total Load From West Conductor and NW Main Leg Strain Record for Record NOS 174

5.16a Frequency Response Function Relating Total Load From East Conductor and SE Main Leg Strain Record for Record NOS 176 5.16b Frequency Response Function Relating Total Load From East Conductor and NW Main Leg Strain Record for Record NOS 176

5. 17a Frequency Response Function Relating Transverse Load From West Conductor and SE Main Leg Strain Record for Record NOS 178

5.17b Frequency Response Function Relating Transverse Load From West Conductor and NW Main Leg Strain Record for Record NOS 178

5. 18a Frequency Response Function Relating Transverse Load From East Conductor and SE Diagonal Leg Strain Record for Record N05 179

5.18b Frequency Response Function Relating Transverse Load From East Conductor and NW Diagonal Leg Strain Record for Record NOS 179

5.19a Frequency Response Function Relating Transverse Load From Center Conductor and SE Main Leg Strain Record for Record NOS 180

5. 19b Frequency Response Function Relating Transverse Load From Center Conductor and NW Diagonal Leg Strain Record for Record NOS 180

XV FIGURE PAGE 5.20a Frequency Response Function Relating Transverse Load From West Conductor and SE Main Leg Strain Record for Record NOS 182 S.20b Frequency Response Function Relating Transverse Load From West Conductor and NW Main Leg Strain Record for Record NOS 182 5.21a Frequency Response Function Relating Transverse Load From West Conductor and SE Diagonal Leg Strain Record for Record NOS 183 5.21b Frequency Response Function Relating Transverse Load From West Conductor and NW Diagonal Leg Strain Record for Record NOS 183 5.22a Frequency Response Function Relating Transverse Load From East Conductor and SE Main Leg Strain Record for Record N08 184 5.22b Frequency Response Function Relating Transverse Load From East Conductor and NW Main Leg Strain Record for Record NOS 184 5.23a Frequency Response Function Relating Transverse Load From West Conductor and SE Main Leg Strain Record for Record NOS 186 5.23b Frequency Response Function Relating Transverse Load From West Conductor and NW Main Leg Strain Record for Record NOS 186 5. 24a Frequency Response Function Relating Longitudinal Load From East Conductor and NW Main Leg Strain Record for Record NOS 187 5.24b Frequency Response Function Relating Longitudinal Load From Center Conductor and NW Main Leg Strain Record for Record NOS 187 5.2Sa Frequency Response Function Relating Transverse Load From West Conductor and SE Main Leg Strain Record for Record N08 189

XVI FIGURE PAGE

S.2Sb Frequency Response Function Relating Transverse Load From West Conductor and NW Main Leg Strain Record for Record NOS 189

5.26a Frequency Response Function Relating Transverse Load From East Conductor and SE Main Leg Strain Record for Record NOS 190 5.26b Frequency Response Function Relating Trainsverse Load From Center Conductor and SE Main Leg Strain Record for Record NOS 190

5.27a Coherence Function Relating Wind Speed and SE Diagonal Leg Strain Record for Record NOS 192

5.27b Coherence Function Relating Wind Speed auid NW Diaigonal Leg Strain Record for Record NOS 192 S.2Sa Coherence Function Relating Wind Speed and SE Main Leg Strain Record for Record NOS 194 5.28b Coherence Function Relating Wind Speed and SE Main Leg Strain Record for Record NOS 194 5.29a Coherence Function Relating Total Load From West Conductor and SE Main Leg Strain Record for Record NOS 196

S.29b Coherence Function Relating Total Load From West Conductor and SE Diagonal Leg Strain Record for Record N08 196

5.30a Coherence Function Relating Total Load From East Conductor and SE Main Leg Strain Record for Record NOS 198

5.30b Coherence Function Relating Total Load From East Conductor and NW Main Leg Strain Record for Record NOS 198

XVI 1 FIGURE PAGE 5.31a Coherence Function Relating Transverse Load From West Conductor and SE Main Leg Strain Record for Record NOS 199

5.31b Coherence Function Relating Transverse Load From West Conductor and SE Diagonal Leg Strain Record for Record NOS 199 5.32a Coherence Function Relating Transverse Load From West Conductor and NW Main Leg Strain Record for Record NOS 201

5.32b Coherence Function Relating Transverse Load From West Conductor and NW Diagonal Leg Strain Record for Record NOS 201 5.33a Coherence Function Relating Transverse Load From West Conductor and SE Main Leg Strain Record for Record NOS 202 5.33b Coherence Function Relating Transverse Load From West Conductor and SE Diagonal Leg Strain Record for Record NOS 202 5.34a Coherence Function Relating Transverse Load From West Conductor and NW Main Leg Strain Record for Record N08 204 5.34b Coherence Function Relating Transverse Load From West Conductor and NW Diagonal Leg Strain Record for Record NOS 204 S.3Sa Coherence Function Relating Transverse Load From East Conductor and SE Main Leg Strain Record for Record NOS 205

5.35b Coherence Function Relating Transverse Load From East Conductor and SE Diagonal Leg Strain Record for Record NOS 205

5.36a Coherence Function Relating Longitudinal Load From West Conductor and SE Main Leg Strain Record for Record NOS 207

XVI 11 FIGURE PAGE 5.36b Coherence Function Relating Longitudinal Load From West Conductor and SE Diagonal Leg Strain Record for Record NOS 207

5.37a Coherence Function Relating Longitudinal Load From East Conductor and SE Main Leg Strain Record for Record NOS 208 5.37b Coherence Function Relating Longitudinal Load From East Conductor and SE Diaigonal Leg Strain Record for Record NOS 208 5.38a Coherence Function Relating Longitudinal Load From East Conductor and NW Main Leg Strain Record for Record NOS 210

5.38b Coherence Function Relating Longitudinal Load From East Conductor and NW Diagonal Leg Strain Record for Record NOS 210

6.1 Schematic Diagram for Multiple Inputs and Single Output System 221 6.2 Schematic Representation of Two Loadings and One Response 224 6.3a Frequency Response Function Relating WSOS and SGOS With WSOS and LC03 as Loadings and SGOS as Response for Record NOS 233

6.3b Frequency Response Function Relating LC03 and SGOS With WSOS and LC03 as Loadings and SGOS as Response for Record NOS 233

6.4a Frequency Response Function Relating WSOS and SG06 With WSOS and LC03 as Loadings and SG06 as Response for Record NOS 235

6.4b Frequency Response Function Relating LC03 and SG06 With WSOS and LC03 as Loadings and SG06 as Response for Record NOS 235

S.Sa Frequency Response Function Relating LC03 and SGOS With LC03 and LC04 as Loadings and SGOS as Response for Record NOS 236

XIX FIGURE PAGE 6.5b Frequency Response Function Relating LC04 and SGOS With LC03 and LC04 as Loadings and SGOS as Response for Record NOS 236 6.6a Frequency Response Function Relating LC03 and SG06 With LC03 and LC04 as Loadings and SG06 as Response for Record NOS 238 6.6b Frequency Response Function Relating LC04 and SG06 With LC03 and LC04 as Loadings and SG06 as Response for Record NOS 238 6.7a Frequency Response Function Relating LC03 and SGll With LC03 and LC04 as Loadings and SGll as Response for Record NOS 240 6.7b Frequency Response Function Relating LC04 and SGll With LC03 and LC04 as Loadings and SGll as Response for Record NOS 240 S.Sa Frequency Response Function Relating LC03 and SGOS With LC03 and LCOS as Loadings and SGOS as Response for Record NOS 241 S.Sb Frequency Response Function Relating LCOS and SGOS With LC03 and LCOS as Loadings and SGOS as Response for Record NOS 241 6.9a Partial Coherence Function Relating LC03 and SG06 Given LC04 for Record NOS 243 6.9b Partial Coherence Function Relating LC04 and SG06 Given LC03 for Record NOS 243 6.10a Partial Coherence Function Relating LC03 and SGOS Given LC04 for Record NOS 245 6.10b Partial Coherence Function Relating LC04 and SGOS Given LCOS for Record NOS 245 6.11a Partial Coherence Function Relating LC03 and SGll Given LC04 for Record NOS 247 6.11b Partial Coherence Function Relating LC04 and SGll Given LCOS for Record NOS 247

XX FIGURE PAGE 7.1 Stages in Time Series Modeling Using Box-Jenkins Methodology 257 7.2 Generation of Time Series From White Noise Through a Linear Filter 260 7.3 Estimated euid Modeled Power Spectra of WSOS for Record NOS 282 A.la Time History of Load From West Conductor for Record NOS 298 A.lb Time History of Load From West Conductor for Record NO? 298 A.2a Time History of Load From West Conductor for Record NOS 299 A.2b Time History of Load From West Conductor for Record NIB 299 A.3a Time History of Load From East Conductor for Record NOS 300 A.3b Time History of Load From East Conductor for Record N07 300 A.4a Time History of Load From East Conductor for Record NOS 301 A. 4b Time History of Load From East Conductor for Record N16 301 A. 5a Time History of Load From Center Conductor for Record NOS 302 A.5b Time History of Load From Center Conductor for Record N07 302 A. 6a Time History of Load From Center Conductor for Record NOS 303 A. 6b Time History of Load From Center Conductor for Record N16 303

XXI FIGURE PAGE A.7a Time History for West Conductor Longitudinal Swing for Record NOS 304 A. 7b Time History for West Conductor Longitudinal Swing for Record N07 304 A. 8a Time History for West Conductor Longitudinal Swing for Record NOB 305 A. 8b Time History for West Conductor Longitudinal Swing for Record NIB 305 A. 9a Time History for West Conductor Transverse Swing for Record NOS 306 A. 9b Time History for West Conductor Transverse Swing for Record N07 30B A. 10a Time History for West Conductor Transverse Swing for Record NOS 307 A. lOb Time History for West Conductor Transverse Swing for Record NIB 307 A.11a Time History for East Conductor Longitudinal Swing for Record NOS 308 A.lib Time History for East Conductor Longitudinal Swing for Record N07 308 A.12a Time History for East Conductor Longitudinal Swing for Record NOB 309 A. 12b Time History for East Conductor Longitudinal Swing for Record NIB 309 A. 13a Time History for East Conductor Transverse Swing for Record NOS 310 A. 13b Time History for East Conductor Transverse Swing for Record N07 310 A.14a Time History for East Conductor Transverse Swing for Record NOS 311

XXll FIGURE PAGE A.14b Time History for East Conductor Transverse Swing for Record NIB 311 A.15a Time History for Center Conductor Longitudinal Swing for Record NOS 312 A.15b Time History for Center Conductor Longitudinal Swing for Record N07 312 A.16a Time History for Center Conductor Longitudinal Swing for Record NOB 313 A.IBb Time History for Center Conductor Longitudinal Swing for Record NIB 313 A.17a Time History for Center Conductor Transverse Swing for Record NOS 314 A.17b Time History for Center Conductor Transverse Swing for Record N07 314 A.18a Time History for Center Conductor Trsuisverse Swing for Record NOB 315 A.18b Time History for Center Conductor Transverse Swing for Record N16 315 A.19a Time History for Stress in Southeast Main Leg for Record NOS 316 A.19b Time History for Stress in Southeast Main Leg for Record N07 316 A.20a Time History for Stress in Southeast Main Leg for Record N08 317 A.20b Time History for Stress in Southeast Main Leg for Record NIB 317 A.21a Time History for Stress in Southeast Diagonal Leg for Record NOS 318 A. 21b Time History for Stress in Southeast Diagonal Leg for Record N07 318

XXI11 FIGURE PAGE A.22a Time History for Stress in Southeast Diagonal Leg for Record NOS 319 A.22b Time History for Stress in Southeast Diagonal Leg for Record N07 319 A.23a Time History for Stress in Northwest Main Leg for Record NOS 320 A.23b Time History for Stress in Northwest Main Leg for Record N07 320 A.24a Time History for Stress in Northwest Main Leg for Record NOS 321 A.24b Time History for Stress in Northwest Main Leg for Record NIB 321 A.2Sa Time History for Stress in Northwest Diagonal Leg for Record NOS 322 A.25b Time History for Stress in Northwest Diagonal Leg for Record N07 322 A.2Ba Time History for Stress in Northwest Diagonal Leg for Record NOB 323 A.2Bb Time History for Stress in Northwest Diagonal Leg for Record N16 323 B.la Autocorrelation Functions of Original and First Differenced Series of WSOS for Record N07 324 B.lb Autocorrelation Functions of Original and First Differenced Series of WSOS for Record NIB 324 B.2a Autocorrelation Functions of Original and First Differenced Series of LC03 for Record N07 325 B.2b Autocorrelation Functions of Original and First Differenced Series of LC04 for Record N07 325

XXIV FIGURE PAGE B.3a Autocorrelation Functions of Original and First Differenced Series of LCOS for Record N07 326 B.3b Autocorrelation Functions of Original and First Differenced Series of LC03 for Record NIB 326 B.4a Autocorrelation Functions of Original and First Differenced Series of LC04 for Record NIB 327 B.4b Autocorrelation Functions of Original and First Differenced Series of LCOS for Record NIB 327 B.5a Autocorrelation Functions of Original and First Differenced Series of SGOS for Record N07 328 B.Sb Autocorrelation Functions of Original and First Differenced Series of SGll for Record N07 328 B.Ba Autocorrelation Functions of Original and First Differenced Series of SGOB for Record N07 329 B.Bb Autocorrelation Functions of Original and First Differenced Series of SG12 for Record N07 329 B.7a Autocorrelation Functions of Original and First Differenced Series of SGOS for Record NIB 330 B.7b Autocorrelation Functions of Original and First Differenced Series of SGll for Record NIB 330 B.Ba Autocorrelation Functions of Original and First Differenced Series of SGOB for Record NIB 331

XXV FIGURE PAGE B.Bb Autocorrelation Functions of Original and First Differenced Series of SG12 for Record NIB 331 C.la Cross Correlation Function of WSOS and SGll for Record NOS 332 C.lb Cross Correlation Function of WSOS and SGI2 for Record NOS 332 C.2a Cross Correlation Function of WSOS and SGOS for Record N07 333 C.2b Cross Correlation Function of WSOS and SGll for Record N07 333 C.3a Cross Correlation Function of WSOS and SGOB for Record N07 334 C.3b Cross Correlation Function of WSOS and SGI2 for Record N07 334 C.4a Cross Correlation Function of WSOS and SGOS for Record NIB 335 C.4b Cross Correlation Function of WSOS and SGOB for Record NIB 335 C.Sa Cross Correlation Function of Total Load Values From West Conductor and SGll for Record NOS 336 C.Sb Cross Correlation Function of Total Load Values From West Conductor and SGI2 for Record NOS 336 C.6a Cross Correlation Function of Total Load Values From East Conductor and SGll for Record NOS 337 C.Bb Cross Correlation Function of Total Load Values From East Conductor and SGI2 for Record NOS 337

XXVI FIGURE PAGE C.7a Cross Correlation Function of Total Load Values From Center Conductor and SGll for Record NOS 338 C.7b Cross Correlation Function of Total Load Values From Center Conductor and SGI2 for Record NOS 338 C.Ba Cross Correlation Function of Total Load Values From West Conductor aind SGOB for Record N07 339 C.Bb Cross Correlation Function of Total Load Values From West Conductor and SGI2 for Record N07 339 C.9a Cross Correlation Function of Total Load Values From East Conductor and SGOB for Record N07 340 C.9b Cross Correlation Function of Total Load Values From Center Conductor and SGOB for Record N07 340 C.lOa Cross Correlation Function of Total Load Values From West Conductor and SGOS for Record NIB 341 C.lOb Cross Correlation Function of Total Load Values From West Conductor and SGll for Record NIB 341 C.11a Cross Correlation Function of Total Load Values From Center Conductor and SGOS for Record NIB 342 C.lib Cross Correlation Function of Total Load Values From East Conductor and SGOS for Record NIB 342 C.12a Cross Correlation Function of Longitudinal Load Values From West Conductor and SGOS for Record NOS 343

xxvii FIGURE PAGE C.12b Cross Correlation Function of Longitudinal Load Values From East Conductor and SGOS for Record NOS 343 C.13a Cross Correlation Function of Longitudinal Load Values From East Conductor and SGOS for Record N07 344 C.13b Cross Correlation Function of Longitudinal Load Values From West Conductor and SGOS for Record N07 344 C.14a Cross Correlation Function of Longitudinal Load Values From West Conductor and SG06 for Record N07 345 C.14b Cross Correlation Function of Longitudinal Load Values From East Conductor and SG06 for Record N07 345 C.ISa Cross Correlation Function of Longitudinal Load Values From West Conductor and SGI2 for Record N07 346 C.15b Cross Correlation Function of Longitudinal Load Values From East Conductor and SGI2 for Record N07 346 C.16a Cross Correlation Function of Transverse Load Values From Center Conductor and SGOS for Record NOS 347 C.16b Cross Correlation Function of Transverse Load Values From Center Conductor aind SGll for Record NOS 347 C.17a Cross Correlation Function of Transverse Load Values From East Conductor and SGll for Record NOB 348 C.17b Cross Correlation Function of Transverse Load Values From Center Conductor and SGll for Record NOB 348

XXVlll FIGURE PAGE C.18a Cross Correlation Function of Transverse Load Values From West Conductor and SGOS for Record NO? 349 C.18b Cross Correlation Function of Transverse Load Values From West Conductor and SGll for Record NO? 349 C.19a Cross Correlation Function of Transverse Load Values From West Conductor and SGOB for Record NO? 350 C.19b Cross Correlation Function of Transverse Load Values From West Conductor and SGI2 for Record NO? 350 C.20a Cross Correlation Function of Transverse Load Values From Center Conductor and SGOS for Record NO? 351 C.20b Cross Correlation Function of Transverse Load Values From East Conductor and SGOS for Record NO? 351 C.21a Cross Correlation Function of Transverse Load Values From Center Conductor and SG06 for Record NO? 352 C.21b Cross Correlation Function of Transverse Load Values From Center Conductor and SGI2 for Record NO? 352 C.22a Cross Correlation Function of Transverse Load Values From Center Conductor and SGOS for Record N16 353 C.22b Cross Correlation Function of Transverse Load Values From Center Conductor and SG06 for Record N16 353 C.23a Cross Correlation Function of Transverse Load Values From Center Conductor and SGll for Record N16 354

XXIX FIGURE PAGE C.23b Cross Correlation Function of Transverse Load Values From Center Conductor and SGI2 for Record NIB 354 D.la Power Spectrum of Wind Speed at 34.7 m for Record NO? 355 D.lb Power Spectrum of Wind Speed at 34.7 m for Record NIB 355 D.2a Power Spectrum of Total Load Values From West Conductor for Record NOS 356 D.2b Power Spectrum of Longitudinal Load Values From West Conductor for Record NOS 356 D.3a Power Spectrum of Total Load Values From East Conductor for Record NOS 357 D.3b Power Spectrum of Longitudinal Load Values From East Conductor for Record NOS 357 D.4a Power Spectrum of Total Load Values From Center Conductor for Record NOS 358 D.4b Power Spectrum of Longitudinal Load Values From Center Conductor for Record NOS 358 D.Sa Power Spectrum of Total Load Values From West Conductor for Record NO? 359 D.Sb Power Spectrum of Transverse Load Values From West Conductor for Record NO? 359 D.Ba Power Spectrum of Longitudinal Load Values From West Conductor for Record NO? 360 D.6b Power Spectrum of Total Load Values From East Conductor for Record NO? 360 D.?a Power Spectrum of Transverse Load Values From East Conductor for Record NO? 361 D.?b Power Spectrum of Longitudinal Load Values From East Conductor for Record NO? 361

XXX FIGURE PAGE D.Ba Power Spectrum of Total Load Values From Center Conductor for Record NO? 362 D.Bb Power Spectrum of Transverse Load Values From Center Conductor for Record NO? 362 D.9a Power Spectrum of Longitudinal Load Values From Center Conductor for Record NO? 363 D.9b Power Spectrum of Total Load Values From West Conductor for Record NOB 363 D.lOa Power Spectrum of Longitudinal Load Values From West Conductor for Record NOS 364 D.10b Power Spectrum of Total Load Values From East Conductor for Record NOB 364 D.11a Power Spectrum of Total Load Values From West Conductor for Record NIB 365 D.lib Power Spectrum of Transverse Load Values From West Conductor for Record N16 365 D.12a Power Spectrum of Longitudinal Load Values From West Conductor for Record N16 366 D.12b Power Spectrum of Total Load Values From East Conductor for Record N16 366 D.13a Power Spectrum of Transverse Load Values From East Conductor for Record N16 367 D.13b Power Spectrum of Longitudinal Load Values From East Conductor for Record N16 36? D.14a Power Spectrum of Total Load Values From Center Conductor for Record N16 368 D.14b Power Spectrum of Transverse Load Values From Center Conductor for Record N16 368 D.15a Power Spectrum of Longitudinal Load Values From Center Conductor for Record N16 369

XXXI FIGURE PAGE D.IBa Power Spectrum of Diagonal Strain Gage Located at SE Corner for Record NOS 370 D.IBb Power Spectrum of Diagonal Strain Gage Located at NW Corner for Record NOS 370 D.17a Power Spectrum of Main Strain Gage Located at SE Corner for Record NO? 371 D.l?b Power Spectrum of Main Strain Gage Located at NW Corner for Record NO? 371 D.IBa Power Spectrum of Diagonal Strain Gage Located at SE Corner for Record NO? 372 D.18b Power Spectrum of Diagonal Strain Gage Located at NW Corner for Record NO? 372 D.19a Power Spectrum of Diagonal Strain Gage Located at SE Corner for Record NOS 373 D.19b Power Spectrum of Diagonal Strain Gage Located at NW Corner for Record NOS 373 D.20a Power Spectrum of Main Strain Gage Located at SE Corner for Record NIB 374 D.20b Power Spectrum of Main Strain Gage Located at NW Corner for Record NIB 374 D.21a Power Spectrum of Diagonal Strain Gage Located at SE Corner for Record N16 375 D.21b Power Spectrum of Diagonal Strain Gage Located at NW Corner for Record N16 375 E.la Frequency Response Function Relating Wind Speed and NW Main Leg Strain Record for Record NOS 376 E.lb Frequency Response Function Relating Wind Speed and NW Main Leg Strain Record for Record NOB 376

XXXll FIGURE PAGE E.2a Frequency Response Function Relating Wind Speed and SE Main Leg Strain Record for Record NO? 377 E.2b Frequency Response Function Relating Wind Speed and NW Main Leg Strain Record for Record NO? 377 E.3a Frequency Response Function Relating Wind Speed and SE Diagonal Leg Strain Record for Record NO? 378 E.3b Frequency Response Function Relating Wind Speed and NW Diagonal Leg Strain Record for Record NO? 378 E.4a Frequency Response Function Relating Total Load From West Conductor and SE Main Leg Strain Record for Record N05 379 E.4b Frequency Response Function Relating Total Load From West Conductor and NW Main Leg Strain Record for Record NOS 379 E.Sa Frequency Response Function Relating Total Load From Center Conductor and SE Diagonal Leg Strain Record for Record NOS 380 E.Sb Frequency Response Function Relating Total Load From Center Conductor and NW Diagonal Leg Strain Record for Record NOS 380 E.Ba Frequency Response Function Relating Total Load From West Conductor and SE Main Leg Strain Record for Record NO? 381 E.Bb Frequency Response Function Relating Total Load From West Conductor auid NW Main Leg Strain Record for Record NO? 381 E.7a Frequency Response Function Relating Total Load From West Conductor suid SE Diagonal Leg Strain Record for Record NO? 382

XXXI11 FIGURE PAGE E.?b Frequency Response Function Relating Total Load From West Conductor and NW Diagonal Leg Strain Record for Record NO? 382 E.Ba Frequency Response Function Relating Total Load From East Conductor and SE Main Leg Strain Record for Record NO? 383 E.Bb Frequency Response Function Relating Total Load From East Conductor euid SE Diagonal Leg Strain Record for Record NO? 383 E.9a Frequency Response Function Relating Total Load From West Conductor and SE Diagonal Leg Strain Record for Record NOS 384 E.9b Frequency Response Function Relating Total Load From West Conductor and NW Diagonal Leg Strain Record for Record NOS 384 E.10a Frequency Response Function Relating Total Load From Center Conductor and SE Diagonal Leg Strain Record for Record NOB 385 E.10b Frequency Response Function Relating Total Load From Center Conductor and NW Diagonal Leg Strain Record for Record NOS 385 E.11a Frequency Response Function Relating Transverse Load From West Conductor and SE Diagonal Leg Strain Record for Record NOS 386 E.lib Frequency Response Function Relating Transverse Load From West Conductor and NW Diagonal Leg Strain Record for Record NOS 386 E.12a Frequency Response Function Relating Transverse Load From East Conductor and SE Main Leg Strain Record for Record NOS 387 E.12b Frequency Response Function Relating Transverse Load From East Conductor and NW Main Leg Strain Record for Record NOS 387

xxxiv FIGURE PAGE E.13a Frequency Response Function Relating Transverse Load From Center Conductor and SE Main Leg Strain Record for Record NOB 388 E.13b Frequency Response Function Relating Transverse Load From Center Conductor and NW Main Leg Strain Record for Record NOS 388 E.14a Frequency Response Function Relating Transverse Load From West Conductor and SE Main Leg Strain Record for Record NO? 389 E.14b Frequency Response Function Relating Transverse Load From West Conductor and NW Main Leg Strain Record for Record NO? 389 E.ISa Frequency Response Function Relating Transverse Load From West Conductor and SE Diagonal Leg Strain Record for Record NO? 390 E.15b Frequency Response Function Relating Transverse Load From West Conductor and NW Diagonal Leg Strain Record for Record NO? 390 E.IBa Frequency Response Function Relating Transverse Load From East Conductor and SE Main Leg Strain Record for Record NO? 391 E.IBb Frequency Response Function Relating Transverse Load From East Conductor and SE Diagonal Strain Record for Record NO? 391 E.17a Frequency Response Function Relating Transverse Load From Center Conductor and SE Main Leg Strain Record for Record NO? 392 E.17b Frequency Response Function Relating Transverse Load From Center Conductor eind NW Main Leg Strain Record for Record NO? 392 E. 18a Frequency Response Function Relating Longitudinal Load From West Conductor and SE Diagonal Leg Strain Record for Record NOS 393

XXXV FIGURE PAGE E.18b Frequency Response Function Relating Longitudinal Load From West Conductor and NW Diagonal Leg Strain Record for Record NOS 393 E.19a Frequency Response Function Relating Longitudinal Load From Center Conductor and SE Main Leg Strain Record for Record NOS 394 E.19b Frequency Response Function Relating Longitudinal Load From Center Conductor and SE Diagonal Leg Strain Record for Record NOS 394 E.20a Frequency Response Function Relating Longitudinal Load From West Conductor and SE Diagonal Leg Strain Record for Record NO? 395 E.20b Frequency Response Function Relating Longitudinal Load From West Conductor and NW Diagonal Leg Strain Record for Record NO? 395 E.21a Frequency Response Function Relating Longitudinal Load From East Conductor and SE Main Leg Strain Record for Record NO? 396 E.21b Frequency Response Function Relating Longitudinal Load From East Conductor and NW Main Leg Strain Record for Record NO? 396 E.22a Frequency Response Function Relating Longitudinal Load From Center Conductor and SE Main Leg Strain Record for Record NO? 397 E.22b Frequency Response Function Relating Longitudinal Load From Center Conductor and SE Diagonal Leg Strain Record for Record NO? 397

XXXVl FIGURE PAGE E.23a Frequency Response Function Relating Longitudinal Load From Center Conductor and SE Diagonal Leg Strain Record for Record NOB 398 E.23b Frequency Response Function Relating Longitudinal Load From Center Conductor and NW Main Leg Strain Record for Record NOS 398 F.la Coherence Function Relating Wind Speed and NW Main Leg Strain Record for Record NOS 399 F.lb Coherence Function Relating Wind Speed and NW Main Leg Strain Record for Record NOB 399 F.2a Coherence Function Relating Wind Speed and SE Main Leg Strain Record for Record NO? 400 F.2b Coherence Function Relating Wind Speed and NW Main Leg Strain Record for Record NO? 400 F.3a Coherence Function Relating Wind Speed and SE Diagonal Leg Strain Record for Record NO? 401 F.3b Coherence Function Relating Wind Speed and NW Diagonal Leg Strain Record for Record NO? 401 F.4a Coherence Function Relating Total Load From West Conductor and SE Main Leg Strain Record for Record NO? 402 F.4b Coherence Function Relating Total Load From West Conductor and NW Main Leg Strain Record for Record NO? 402 F.Sa Coherence Function Relating Total Load From West Conductor and SE Diagonal Leg Strain Record for Record NO? 403

XXXVll FIGURE PAGE F.Sb Coherence Function Relating Total Load From West Conductor and NW Diagonal Leg Strain Record for Record NO? 403 F.Ba Coherence Function Relating Total Load From East Conductor and SE Main Leg Strain Record for Record NO? 404 F.Bb Coherence Function Relating Total Load From East Conductor and SE Diagonal Leg Strain Record for Record NO? 404 F.?a Coherence Function Relating Total Load From Center Conductor and SE Diagonal Leg Strain Record for Record NOB 405 F.7b Coherence Function Relating Total Load From Center Conductor and NW Diagonal Leg Strain Record for Record NOS 405 F.Sa Coherence Function Relating Transverse Load From Center Conductor euid SE Main Leg Strain Record for Record NO? 406 F.8b Coherence Function Relating Tranverse Load From Center Conductor and NW Main Leg Strain Record for Record NO? 406 F.9a Coherence Function Relating Transverse Load From East Conductor and SE Main Leg Strain Record for Record NO? 40? F.9b Coherence Function Relating Tranverse Load From East Conductor and SE Diagonal Leg Strain Record for Record NO? 40? F.lOa Coherence Function Relating Transverse Load From West Conductor and NW Main Leg Strain Record for Record NOS 408 F.10b Coherence Function Relating Tranverse Load From West Conductor and NW Diagonal Leg Strain Record for Record NOS 408

XXXVlll FIGURE PAGE F.11a Coherence Function Relating Longitudinal Load From West Conductor euid SE Diagonal Leg Strain Record for Record NO? 409 F.lib Coherence Function Relating Longitudinal Load From West Conductor and NW Diagonal Leg Strain Record for Record NO? 409 F.12a Coherence Function Relating Longitudinal Load From East Conductor and SE Main Leg Strain Record for Record NO? 410 F.12b Coherence Function Relating Longitudinal Load From East Conductor and NW Main Leg Strain Record for Record NO? 410

xxxix CHAPTER 1 INTRODUCTION

Transmission towers and conductors form an integral part of the national grid voltage networks. The primary responsibility of the transmission towers and conductors within the national grid voltaige networks is to transmit electricity from electric power plants to consumers. Therefore, continuous, uninterrupted, and proper func­ tioning of transmission towers and conductors are essen­ tial in order to meet the power demand in the nation. The structural reliability and the integrity of trans­ V mission towers and conductors are important facets of the national grid voltage networks. Therefore, a high stan­ dard for design must be enforced to preclude any struc­ tural failure even when the transmission towers and con­ ductors are subject to severe loading conditions. The locations of the transmission towers and conduc­ tors are diverse in nature. There are two extreme cases in which the locations of the transmission towers and conductors may vary. In the first extreme case, the transmission towers and conductors may be located in the isolated country-side far from the nearest civilization. In the second extreme case, the transmission towers and conductors may be located near densely populated metropolitan areas. These two extreme cases result in different geographical terrains which the transmission towers and conductors may encounter. The design of transmission tower structural members is dictated by the locations and the geographical terrains in which the transmission towers are to be erected. The design of the trainsmission towers is highly sen­ sitive to geographical terrain and geographical location of the transmission towers. In an effort to curtail the the perils faced by transmission tower structures under actual field conditions, two methods may be employed to \y perform the tasks. The first method involves a conserva­ tive design using standard design guidelines. The second method involves a proper in-depth study and research into the behavior of the transmission tower structures and conductors under various loading conditions. The former approach facilitates a design which may be overly con­ servative. The latter allows the designer to analyze the behavior of the transmission tower under static and dynamic loads. The results obtained from the analysis are then incorporated into the design of the transmission tower. Transmission towers and conductors are more sensitive to dynamic loads than to static loads. On the other V hand, dynamic loads, such as those produced by wind, tend to be stochastic in nature. The effect of dynamic load ings on trainsmission towers suid conductors must be thoroughly studied and fully understood before an effi­ cient design may be obtained. Dynamic loads are any loads for which the magnitude, direction, position, or any combination of these varies with time. Dynamic loads can be characterized as either deterministic or non-deterministic. If the time varia­ tion of the loads is fully known, then they are classi­ fied as deterministic loads. When the time variation of the loads is not fully known, then they are classified as non-deterministic or stochastic loads. Non-deterministic loads can be treated as random processes because at any point in time, these loadings are random variables. Wind loads on structures are characterized as dynamic loads because their magnitude, direction, and position varies with time. Wind loadings are stochastic because no two records of wind speed or wind direction resemble one another. Since they are stochastic, wind loads are treated as random processes. Because wind loadings are stochastic, the responses of transmission towers and conductors acted upon by wind loadings are stochastic, also. This is true for the responses of any flexible structure subjected to stochastic loads. The design of important structures to resist wind loads is an important topic in structural engineering. In most building codes, wind loadings are treated as quasi-static loads. For example, the ANSI ASS.1-1982 provides methodology to analyze wind loads acting on a structure. However, if serious doubt exists in designing structures highly sensitive to wind loads, the designer can resort to wind tunnel tests or perform a full-scale wind-structure interaction test. The wind tunnel tests or a full-scale wind structure interaction test permits the designer to simulate the actual field conditions. Ideal­ ly, the results obtained from such studies, represent the actual responses of a structure due to wind-structure interaction. The results obtained from such studies are expected to enhance the actual design of the transmission towers. Therefore, a more efficient and a more reliable design are obtained. Wind loads act on a transmission tower in two ways. First, the wind loads act directly on the transmission v/ tower itself. Second, the wind loads act on the con­ ductor which in turn transmits these loads to the trans­ mission tower. The latter case is thought to be more severe than the former. However, both cases are im- port2u:it in ascertaining the overall effect of wind loads on the transmission tower. The nature of this research is to study the statis­ tical properties of the wind and response data on a transmission line tower. These data were collected by the Bonneville Power Administration (BPA) in Oregon. These data consist of wind speed and direction records as well as associated response records of full-scale trans­ mission tower structure and conductors. The primary objectives are: (1) to study wind speed and associated load and response records for the transmission line system, (2) to determine the stationarity of the afore­ mentioned records, (3) to study the frequency content of these records, (4) to relate a single loading to a measure of response in the frequency domain by estimating the frequency response function, (5) to relate two loadings to a measure of response in the frequency domain and compare the quality of this relationship to that obtained previously for a single loading, and (6) to model wind speed time histories using time series method­ ology.

The outline of the material presented is as follows. A literature review of statistical and time series work, simulation techniques, and stochastic modeling of sta­ tionary and non-stationary processes performed in the past in engineering and non-engineering fields is pre­ sented in Chapter 2. The data collection and instru­ mentation system is described in Chapter 3. In Chapter 4, statistical analysis of selected time series records are performed. The frequency responses of single input- single output structural system are described in Chapter 5. The frequency responses of multiple inputs-single output structural system are described in Chapter 6. Time series modeling and simulation are performed in Chapter 7 Finally, the discussion of results obtained auid the directions of future research are described in Chapter 8. CHAPTER 2 LITERATURE REVIEW

A large volume of literature exists concerning wind- structure interaction and responses, random responses of structures, statistical analysis of random physical data, stochastic modeling and simulation of time series, and the application of spectra in engineering design and analysis. The data describing any random physical process are usually functions of time and are termed "time histo­ ries. " In order to study the frequency contents of a time history, a mathematical technique capable of trans­ forming information obtained in the time domain to the frequency domain must be utilized. The mathematical development of the Fast Fourier Transform (FFT) has enabled researchers to study the frequency contents of any realizable time history in the frequency domain. The FFT has the advantage over the classical Fourier Trans­ form in that the former has a smaller number of computa­ tions involved. Cooley, Lewis, and Welch (1967) provided an overview of the development of the FFT in data analysis and described the contributions of other inves­ tigators in the development of the FFT. Helms (1967) described two methods for using the FFT to reduce the 8 number of arithmetic operations. The first method is capable of formulating a filtering operation so that a simulation of independent variables can be handled by the second method known as the "overlap-adding" version of the FFT. Cooley, Lewis, and Welch (1969) defined the elementary properties of the finite Fourier Transform such as the convolution and term-by-term product opera­ tions. Their results were then used to give a simple derivation of the FFT algorithm. Holmes (1977) concluded that the frequency domain approach was the easiest to use and was the most efficient method when coupled with an Inverse FFT algorithm in simulating random wind data. The cornerstone of time series analysis is the con­ cept that the sequence of observations making up a time series constitutes a realization of jointly distributed random variables. This concept enables the analyst to model a time series based on its statistical properties. Box and Jenkins (1976) comprehensively described the techniques involved in the modeling of time series in the time domain. They considered three models which may be used to describe time series. These three models are the (AR), the moving-average model (MA), and the mixed model (ARMA, ARIMA). In the AR model, forecasting of a current observation in a time series is dependent on past observations plus a random shock or a white noise. In the MA model, fore­ casting of a current observation in a time series is dependent on a past observation plus several random shocks or white noises. In the mixed model, ARMA or ARIMA, forecasting of a current observation is dependent on past observations plus the random shocks or white noises. Box and Jenkins (1976) also presented the mathe­ matical techniques to obtain the proper transfer function in the time domain and the frequency response function in the frequency domain based on modeled time series of the input imposed upon a physical system and its associated output.

The advent of modern computers enabled the analyst to apply the theoretical mathematical development of the Fourier Transform and time series modeling to practical problems. Nau, Oliver, and Pister (1980) described the use of ARMA models to simulate and analyze real and artificial earthquake accelerograms. The results of the analysis indicated that a discrete-time ground accelera­ tion model consisting of a linear filter whose parameters were piecewise-constant on five second intervals was useful in structural response studies. This simulation, 10 coupled with white noise input modulated by a non- parametric variance envelope, provided a useful and prac­ tical characterization of the non-stationary features of earthquake accelerograms. Reed and Scanlan (1983) considered full-scale wind velocity and wind pressure time series data collected on two hyperbolic cooling towers. They utilized time series analysis and modeling to simulate wind loadings and to predict the transfer function models in the time domain with wind velocity as the input and wind pressure- differences as the output. Hamilton and Watts (1978) mathematically studied the behavior of the partial autocorrelation function of sea­ sonal time series based on a partial autocorrelation pattern. This pattern acted as a signature of the regu­ lar component of the model which is a simple composite of the autocorrelation and partial autocorrelation functions of the regular component. Newbold (1980) showed the adequacy of a fitted ARMA model based on a Lagrange multiplier test and on analysis of residual autocorrela­ tions. Ljung and Box (1978) considered the overall test for lack of fit in ARMA models using models proposed by Box and Pierce (1970). They considered the power of the tests and the test capabilities when non-normal series 11 were encountered. Similar modifications in the overall tests used for transfer function noise models were proposed. Godfrey (1979) considered the problem involved in testing the adequacy of an ARMA time series model. He proposed the use of Monte Carlo results on samples of finite size. Rao and Tong (1973) provided a method using the frequency domain approach to furnish tests to deter­ mine the time dependence of a tranfer function of a linear system. Hannan (1979) discussed the identification and parameterization of ARMA systems in relation to the use of certain canonical forms. Stanton (1965) estimated the frequency responses for transfer functions occurring in a multivariate block diagram representation of a turboalternator. He modeled the turboalternator as a linear system. The availability of Fourier Transforms enables most researchers to study the frequency content of a physi­ cally realizable time series. The transformation of a physically realizable time series into the frequency domain yields the power spectrum of the time series. Newbold (1981) gave an overview of some research in time series analysis with an emphasis on the methodological problems in linear model building and spectral analysis. 12

The analysis of both single and multiple time series was considered. Parzen (1961) gave a full account of the mathematical considerations involved in the estimation of spectra. Jenkins (1961) provided a set of general guide­ lines in the analysis of spectra. Hashish and Abu-Sitta (1974) described a procedure which considered the fre­ quency distribution of the pressure spectra and response spectra to predict the dynamic response of a cooling tower under the action of turbulent wind. Steinmetz, Billington, and Abel (1978) studied the dynamic behavior of a hyperbolic cooling tower subjected to wind using specific wind records and stochastic analysis of wind pressure spectra. They concluded that the results ob­ tained supported the quasi-static assumption normally used for cooling tower wind loading. Loh (1985) obtained the spectra of wind data collected from a typhoon. He estimated the turbulence spectra and cross spectra of horizontal typhoon wind fluctuations. Norville, Mehta, and Farwagi (1985) studied the wind load and response characteristics of several wind records acting on a traunsmission line tower. They also obtained the power spectra and the cross spectra of the records. Bhansali (1980) described the mathematics underlying the analysis of the inverse correlation function of a 13 with emphasis on window methods for estimating this function. Cleveland (1972) estimated the inverse of a time series using the auto­ correlations associated with the inverse of a spectral density estimate. He utilized autoregressive and spectral smoothing methods to obtain the estimates. The estimation of parameters used in modeling of time series is often tedious and time consuming. Most modern computing techniques for modeling time series use numerical solutions to increase computational efficiency. Reilly (1980) presented a computer-based procedure to identify the form and the characteristics of outliers by combining univariate methods proposed by Box and Jenkins (1976) with outlier detection to enheuice the analysis and the forecasting of time series data. Reilly (1981) des­ cribed a general algorithm for the Box-Jenkins modeling process. He related Box-Jenkins procedures to regression models which consisted of the identification, the estima­ tion and verification, and the forecasting phases. Next, literature involving practical engineering applications of the response of structures to random loadings, the response of structures due to wind-structure interaction, and the response of structures in full-scale testing are discussed. 14

Vibration of mechanical and structural systems has received attention in engineering requirements and prac­ tices. The engineering profession has recognized the random characteristics of physical vibrations which in­ troduce complexity in actual design of important struc­ tures. Crandall and Mark (1963) presented a very thor­ ough treatment of the raindom vibration of mechanical systems. They discuss extensively the characterization of random vibration, the transmission of random vibra­ tion, and the problem of failures resulting from random vibration of mechanical systems. Lin (1967) emphasized the analyses of the responses of practical structures of importance to civil engineers to random excitations. Bycroft (1960) investigated the suitability of white noise as a representation of earthquake excitation. All the literature reported herein discusses the random and stochastic nature of structural loadings and structural responses. The effects of wind forces on structures are an important design consideration for most engineered struc­ tures. Researchers in the area of wind engineering have recognized the fact that wind speed is random in nature and have attributed to the difficulty in studying the effect of wind-structure interaction to the randomness of 15 wind speed. Therefore, researchers in wind engineering have used simulation and stochastic modeling techniques to study the responses of structures to wind loads. Smith (1985) studied the dynamic response of tall stacks subjected to wind forces using a stochastic model. He identified critical and transcritical flow regimes using wind-force spectra. Matheson and Holmes (1980) simulated wind velocities using a Monte Carlo technique based on an Inverse Fast Fourier Transform and the equations of motion of the line were then solved numerically using a finite difference method. They concluded that at high velocities, dynaunic response is suppressed by high aero- dynaunic damping. Using wind records from several weather stations in the United States, Grigoriu and Longo (1985) described a statistical method to evaluate wind records and to estimate the wind speeds of various return periods using simplified non-stationary models. The design of structures to resists wind loads has been incorporated in most building codes at local and national levels for structures which are sensitive to wind loads or for structures in which the design of the structural members is highly dependent on the wind loads. ANSI ASS.1-1982 described quite comprehensively the design aspect of wind-structure interaction. ANSI 16

ASS.1-1982 is the most common reference for the designer to determine the magnitude of wind load which a struc­ ture will experience. The Guidelines for Transmission Line Structural Loading were prepared by the American Society of Civil Engineers' Committee on Electrical Transmission Structures in 1984. The purpose of the guidelines is to provide transmission line designers with procedures for the selection of design loads and load factors based on the latest research and state-of-the-art design techniques. The concepts of probability based design, and the nature and variability of loads used to design transmission line structures, were reviewed and discussed. In particular, the guidelines deal comprehen­ sively with wind loads on transmission line structures. Other loadings such as the conductor galloping effect, conductor longitudinal loads, and vibrations were also described.

The physical behavior of latticed structures such as transmission towers subjected to raindom loadings can be obtained by proper instrumentation of the structures to measure external loadings acting on the structures and the associated structural responses. The Electric Power Research Institute (EPRI) has, through the years, pub­ lished literature in the area of on-site instrumentation 17 of latticed structures. On-site instrumentation is still by far the primary of evaluating both analysis methods and failure criteria. Arnold (1985) described the proper procedures in using strain gages as a major source for collecting important structural data on full- scale electric trauismission structures for the EPRI Transmission Line Mechanical Research Facility. These structural data were the member loads, the bending mo­ ments in latticed towers, and the stress distributions in steel poles. He also described proper gaiging procedures, calibration techniques, and error ainalysis of the strain gage data. Tuan, Potter, and Jackman (1985) installed load transducers and monitoring equipment used for data acquisition on a 161 kV steel pole. The data obtained were used to establish load statistics in reliability design practices. Kempner and Laursen (1979) investigated the effect of wind loadings on a 500 kV AC single circuit latticed transmission tower. They performed data analyses in an attempt to characterize the wind forces acting on the tower. Other related statistical properties calculated were power spectral densities, turbulence intensities, and wind gust factors. Stationarity tests were also performed on wind records. Kempner (1980) conducted full 18 scale structural tests on a non-energized mechanical test line transmission tower structure to characterize the static behavior of the structure and of the 1200 kV eight-conductor bundle. He obtained the torsional stiff­ ness values of the structure from the field data to be approximately twice as large as the theoretical values. Kempner (1980) performed structural dynamic tests on a non-energized mechanical test line traunsmission tower and 1200 kV conductor bundle system. He obtained the dynamic mode shapes, the tower structural daunping coefficients, the conductor bundle modal frequencies, and the tower longitudinal and transverse frequencies.

Chiu and Taoka (1971) computed the dynamic response of a 150 foot high free-standing, three-legged, latticed steel tower using actual wind velocity records, and digi­ tally simulated wind records. They found that for free­ standing structures the fundaimental mode of vibration predominates. In the fundamental mode of vibration, the structure has a fairly low daunping ratio. Peyrot (1985) derived a Load Resistance Factor Design format for high voltage electric transmission lines using a reliability approach. He assigned relative levels of reliability to different lines, to different structures within one line, and to different components within one structure. 19

Results obtained from the literature review indicate that: (a) modeling of physical time series is helpful in forecasting and in predicting future characteristics and responses of a system, (b) spectral analysis gives a very useful representation of the power distribution of random physical data in the frequency domain, and (c) frequency domain analysis for transfer functions is more meaningful in the context of interpretation because most dynamic analyses of structures use calculations and results in the frequency domain. An investigation of the behavior of transmission tower responses to wind loads will expand our knowledge concerning the behavior of transmission towers. In the next chapter, the on-site data collection system and instrumentation of the full-scale transmission tower structure are described in detail. CHAPTER 3 SITE DESCRIPTION, INSTRUMENTATION, AND DATA COLLECTION SYSTEM

3. 1 Introduction The Bonneville Power Administration (BPA) has con­ ducted studies on wind load response of transmission line systems by collecting and ainalyzing wind and response related data on a test line in the field. The location of the transmission line system and the structural configu­ ration of the transmission tower are described in section 3.2. The instruments used in collecting wind and related response data are described in section 3.3. The wind and the types of response data collected are also described in section 3.3. BPA has given special emphasis to data handling, data processing and filing because each record contains over 300,000 data points. Table 3.1 provides general information concerning the twenty-three records collected at BPA test site.

3^2 Location The BPA test site is located in Northern Oregon, between the Dalles and More, east of the Cascade Moun­ tains, and approximately 1.5 km east of the Deschutes River as shown in Figure 3.1. The terrain to the east of

20 21

Table 3.1 Twenty Three Segments of Data

MEAN WIND MEAN WIND RECORD DATE TIME DIRECTION SPEED (DEGREES) (MPS)

NOl 12/02/81 01.31.57 212 18.33 N02 12/05/81 06.42.45 179 17.43 NOS 12/15/81 16.11.48 224 15. 20 N04 12/16/81 08.30.32 — 1.34 NOS 12/16/81 16.10.28 81 15.65 NOS 01/14/82 10.57.52 300 15. 20 N07 01/16/82 19.04.51 258 23.25 NOS 01/31/82 07.36.32 300 20.56 N09 02/03/82 14.11.35 77 3. 13 NIO 02/14/82 13.05.39 268 14. 31 Nil 02/15/82 23.26.40 270 20. 12 N12 02/15/82 10.29.05 258 14.31 N13 02/16/82 00.38.56 277 20. 12 N14 03/08/82 16.03.42 — 0.00 NIS 03/11/82 14.52.13 267 17.88 N16 03/12/82 16.13.50 229 S.OS N17 04/12/82 01.10.26 243 15.65 NIS 04/13/82 15.29.13 253 18.32 N19 04/17/82 17.57.11 289 12.96 N20 04/20/82 22.03.35 100 14.31 N21 04/23/82 11.58.38 280 15.65 N22 04/28/82 12.28.13 286 16.54 N23 05/07/82 14.19.51 282 12.96 22

Figure 3.1 Topography of Site and Orientation of Power Lines 23 the measurement site consists mostly of smooth, rolling Wheatland. That portion of the terrain to the east which is uncultivated is covered with grass and shrubs. The terrain to the west of the measurement site consists of a deep wide canyon. The test site is located in this area for two major reasons. First, strong winds are frequent at the chosen site. Second, winds from the southwest direction are funneled up the side of the canyon which tends to provide wind patterns which are different from normal. These funneling effects were investigated by Kempner aind Laursen in 1979. The general topology in the vicinity of test lines and their orientation are shown in Figure 3.1. Three lines, orientated at an angle of about 8 degrees west of true north, form part of the Pacific Northwest-Southwest Intertie System. The first two lines east of the Des­ chutes River are 500 Kv energized lines. These two lines are referred to as John Dao^-Grizzly 1 (JD-G 1) and John Day-Grizzly 2 (JD-G 2). The third line is a non- energized mechanical test line. It was constructed in 1976 to study the behavior of 1100 Kv conductor bundles. This line is parallel to the other two lines, and is referred to as the MORO test line. 24

The perpendicular distances between JD-G 1 and JD-G 2, and between JD-G 2 and the mechanical test line are 150 feet and 125 feet, respectively. The distance between JD-G 1 and the Deschutes River is approximately 1.5 km. There are 5 towers located on line JD-G 2. These towers are numbered from 1 to 5, tower 1 being the tower at the northern end of the site. The distance between towers 4 and 5 is 1475 feet and this represents the longest span (Kempner and Laursen, 1977). Figure 3.2 presents a sche­ matic plaui of conductor spans between towers 3 and 4, and between towers 4 and 5. Tower 4 is an instrumented, delta configured tower. It is referred to as tower JD-G 16/4 because it is lo­ cated on mile 16 of JD-G 2. Tower 4 is similar to that shown in Figure 3.3. Tower 4 supports central, east, and west conductors. Overhead ground wires (OHGW) which are smaller in diauneter than conductors are located at a height of 111 feet. All the conductors are paired up in twin bundles, whereas overhead ground wires are single cables. The west conductor group bundle is 9 inches lower than the east conductor group bundle. This ar­ rangement reduces subconductor oscillations which occur during west winds. Tower 3 is located at a distance of 825 feet north of tower 4 of JD-G 2. Tower 3 also has a 25

N- -^

* effective half span lengths of conductors (Kadaba, 1988)

Figure 3.2 Elevation Along the Test Line (Vertical Scale Exaggerated) Anemometer (34.7 m) 9.1 m

Load ceil and Swing angle indicators

41 mm cfiameter

West conductor

Figure 3.3 Schematic of Tower 16/4 27 delta configuration, wheareas tower 5 has a non-delta configuration. The change in configurations between towers 4 and 5 results in the insulator assemblies of the outer phases at the test tower to be suspended in a non- vertical position (Kempner and Laursen, 1977).

3i_3 Instrumentation The Data Acquisition System is comprised of a mini­ computer, a soft magnetic disk and requisite signal con­ ditioning equipment to activate the entire system. The activated system can record data from 256 channels of instrumentation. All devices used in measuring wind and response related data are located on tower JD-G 16/4 and on towers 3,4, and 5 of JD-G 2. A total of 256 channels are available to collect wind and tower response data. Rather than recording all 256 channels simultaneously, various recording modes, comprised of several selected channels were established in the modes selected to record static or dynamic phenomena of interest. The data used in the research reported herein are recorded in Mode 22. Mode 22 is comprised of 38 channels for recording wind and associated structural response data. Table 3.2 gives an overall description of Mode 22. The 38 channels are used to record the following data: 3 conductor loads and 28

Table 3.2 File Description in Mode 22 FILE CHANNEL INSTRUMENT, LOCATION, HEIGHT LCOl 78 LOAD CELL 1 JD-G 16/4 EAST OHGW LC02 79 LOAD CELL 2 JD-G 16/4 WEST OHGW LCOS 80 LOAD CELL 3 JD-G 16/4 WEST CONDUCTOR LC04 81 LOAD CELL 4 JD-G 16/4 EAST CONDUCTOR LCOS 82 LOAD CELL 5 JD-G 16/4 CENTER CONDUCTOR SAOl 83 SWING ANGLE 1 JD-G 16/4 EAST OHGW +X DIR. SA02 84 SWING ANGLE 2 JD-G 16/4 EAST OHGW +Y DIR. SA03 85 SWING ANGLE 3 JD-G 16/4 WEST OHGW +X DIR. SA04 86 SWING ANGLE 4 JD-G 16/4 WEST OHGW +Y DIR. SA05 87 SWING ANGLE 5 JD-G 16/4 WEST COND +X DIR. SA06 88 SWING ANGLE 6 JD-G 16/4 WEST COND +Y DIR. SAO? 89 SWING ANGLE 7 JD-G 16/4 EAST COND +X DIR. SA08 90 SWING ANGLE 8 JD-G 16/4 EAST COND +Y DIR. SA09 91 SWING ANGLE 9 JD-G 16/4 CENT COND +X DIR. SAIO 92 SWING ANGLE 10 JD-G 16/4 CENT COND +Y DIR. SGOl 66 STRAIN GAGE 1 JD-G 16/4 NW 1 DIA SG02 67 STRAIN GAGE 2 JD-G 16/4 NE 2 MAIN SGOS 68 STRAIN GAGE 3 JD-G 16/4 NW 2 MAIN SG04 69 STRAIN GAGE 4 JD-G 16/4 SE 1 DIA SGOS 70 STRAIN GAGE 5 JD-G 16/4 SE 2 MAIN SGOS 71 STRAIN GAGE 6 JD-G 16/4 SE 3 DIA SGO? 72 STRAIN GAGE 7 JD-G 16/4 NW 2 MAIN SGOS 73 STRAIN GAGE 8 JD-G 16/4 SW 2 MAIN SG09 74 STRAIN GAGE 9 JD-G 16/4 NW 2 MAIN SGIO 75 STRAIN GAGE 10 JD-G 16/4 NW 1 DIA SGll 76 STRAIN GAGE 11 JD-G 16/4 NW 2 MAIN SG12 77 STRAIN GAGE 12 JD-G 16/4 NW 3 MAIN WDOl 159 WIND DIRECTION ANEM TWR 3, 47.4 M WD02 163 WIND DIRECTION ANEM TWR 4, 41.4 M WD03 168 WIND DIRECTION ANEM TWR 5, 39.3 M WD04 179 WIND DIRECTION ANEM JD-G 16/4, 34.7 M WDOS 181 WIND DIRECTION ANEM JD-G 16/4, 10.9 M WSOl 156 WIND SPEED IiOT WIRE ANEM, ATOP LIGHT POLE WS02 158 WIND SPEED PROP ANEM, MORO TWR 3, 47 .4 M WSOS 161 WIND SPEED PROP ANEM, MORO TWR 4, 41 .5 M WS04 16? WIND SPEED PROP ANEM, MORO TWR 5, 39 .3 M WSOS 178 WIND SPEED ]PRO P ANEM, JD-G 16/4, 34.'7 M WSOS 180 WIND SPEED PROP ANEM, JD-G 16/4, 10.<0 M 29

2 OHGW loads from load cells, 10 swing angles, 12 sets of strains, 5 wind directions, and 6 wind speeds. The following two requirements must be met simulta­ neously to trigger the data acquisition system to collect » and store data: 1. the wind speed must be equal to or greater than a triggering value of 18 mps (40.5 mph) for one minute, and 2. the ambient temperature must be equal to or greater than 39.2 degrees Fahrenheit (4 degrees Celsius). Once the system is activated, the recording mode samples the data for 10 or 12 minutes, depending upon the sam­ pling rate. At the end of the sampling time, the system cannot be automatically triggered again for 60 minutes. The system can be manually triggered within this 60 minute time period from terminals either on the site or at BPA Headquarters in Portland. Two sampling rates are used in data collection: 10 samples per second (sps) or 20 sps. In Table 3.2, LCOl, LC02, and SG01-SG12 are sampled at 20 sps. All other channels are sampled at 10 sps. In monitoring wind speeds, hot wire and propeller vane anemometers are used. The hot wire anemometer is 30 mounted on top a light pole at a height of 10 meters from the ground. The light pole is located at a distance of 200 feet ENE of tower 2. The exposed resistor of the hot wire anemometer acts as a voltage sensor. Changes in voltage associated with changes in windspeed are trans­ mitted to the Data Acquisition System. The main advan­ tage of using the hot wire anemometer is because of its high sensitivity; stalling speed is low since no friction is encountered by interacting mechanical parts. The propeller-vane anemometers measure both wind speed and direction. One of these anemometers is mounted at a height of 33.5 feet (10.21 m) from the ground on the northwest leg of tower JD-G 16/4. The other anemometer is located at an elevation of 110 feet (33.53 m) on the west side of tower JD-G 16/4. In the measurement of wind speed, the three blade propeller has a threshold speed of 19.12 mph (8.5 mps) and a distance constant of 10.35 feet (4.6 m). The distance constant of an anemometer is the length of air column necessary to pass a wind sensor after a stepwise change in speed for the sensor to regis­ ter 63 percent of the change in speed (Kempner and Laursen, 1981). The directional sensitivity of the ane­ mometers is 4.95 mph (2.2 mps) at 8 degrees with a 31 distance constant of 34.12 feet (10.4 m). The orientation of wind direction is such that:

1. a zero degree reading represents true north, and

2. a clockwise rotation corresponds to an increase in the wind direction reading (Kempner and Laursen, 1979).

Internal heaters enable the propeller anemometers to operate under cold weather conditions.

Strain gages are welded to main and diaigonal members of the base of the tower. The orientation auid locations of the strain gages are such that only axial strains in the members were measured. Strain gaiged members are designated by the corner of the tower in which they are located. The numbering of the strain gaged members is from left to right by looking at a main leg in the center of the tower. Member 2 is the main leg, whereas members 1 and 3 are the diagonal legs. Figure 3.4 represents schematic locations of strain gaiges described in Table 3.2. The accuracy of the strain readings is controlled by the installation of the strain gages. Signal condi­ tioning units located on the tower are used transmit strain gage signals to the Data Acquisition System. Norville, Mehta, and Farwagi (1985) described the mounting of strain gages on the members. 32

N e SGOl (NW 1 Dia) SGOS (NW 2 Main) SG07 (NW 2 Main) SG09 (NW 2 Main) SGIO (NW 1 Dia) NE SG02 (NE 2 Main) SGll (NW 2 Main) SG12 (NW 3 Dia)

SG04 (SE 1 Dia) SGOS (SW 2 Main) SGOS (SE 2 Main) SGOS (SE 3 Dia)

Figure 3.4 Schematic Locations of Strain Gages Designated by the Corner of the Tower 33

Load cells measure the maignitudes of the loads trans­ mitted to the tower attachment points by the conductors and the overhead ground wires. Axial loads can be meas­ ured in the insulator assemblies connected to the east and west groundwires, aind to the east, center and west conductors. The load cells in the overhead ground wires (OHGW) have a sampling rate of 20 sps, whereas the load cells in the 3 conductors have a sampling rate of 10 sps. Baldwin-Lima-Hamilton (BLH) strain gage load cells are used. BLH Type T3P1, rated at 5000 pounds, were used on the OHGW and BLH Type T2P1, rated at 20000 pounds, were used on the conductors (Kempner and Laursen, 1981).

Swing-angle indicators are used to measure the di­ rection of swing in the conductors and OHGW. The swing angle indicators measure longitudinal (parallel to line) and transverse (perpendicular to line) swings. Humphrey CP17-0601-1 pendulum swing-angle indicators are used. The maximum swing angle in either direction which the indicators can measure is 45 degrees. The zero position is vertical (Kempner and Laursen, 1979). Load cells and swing-angle indicators were installed in the linkage between the insulator string and the tower.

The twenty three available records are now considered for analysis. Four of the twenty three records were 34 selected for analysis purposes. The statistical analyses of these four records are described in detail in Chapter 4. The criteria used in selecting these four records from those available are also described in Chapter 4. CHAPTER 4 STATISTICAL ANALYSIS OF TIME SERIES RECORDS

4.1 Introduction The statistical analyses of selected time series records are discussed in this chapter. Table 3.2 summa­ rized the types of wind and response data collected by BPA for any one particular record. These wind and re­ sponse data were in the form of time series. In particu­ lar, these time series were the time series of conductor loads, swing angles of conductors, strain gages, wind directions, aind wind speeds. All the time series de­ scribed herein are stochastic in nature. Since these time series are stochastic, they can only be assessed in probabilistic terms. Therefore, statistical analyses were used to define the descriptive properties of the selected time series. The descriptive statistical properties of a selected time series are the mean, variaince, autocovariance func­ tion, and autocorrelation function. If two separate and causally related time series are analyzed, cross covari- ance functions and cross correlation functions are used as additional descriptive statistical properties.

35 36

4.2 Data Handling All the time series records used in subsequent auialy- sis were recorded on 9-track unlabeled, 1600 bytes per inch (BPI) magnetic tapes. There are twenty-three avail­ able wind auid trainsmission tower response records which were collected between December 1981 and Mao^ 1982 at the test site. Twenty-one of these records were collected under strong wind conditions. The other two records were obtained during relatively calm conditions to establish zero values as a reference in subsequent analysis. The average wind speeds amd directions of the twenty-three available records are shown in Figure 4.1. As discussed in section 3.3, each tape is divided into 38 channels. Each channel performs a different task and is labeled accordingly. Each recording number constitutes an index including 38 files. For example, N02.WS06 refers to the sixth wind speed file in record number 2. Files sampled at 20 sps contained 12000 observations and have a 10- minute record length. Files sampled at 10 sps contained 7200 observations and have a 12-minute record length. Section 3.3 provides information concerning sampling rates of the files. 37

N

300* • 60'

270' 90'

• 120' 240

JD-G 2

Figure 4.1 Twenty Three Available Wind Records 38

4i.3 Time Series Analysis

A time series is a collection of observations made sequentially in time. The sequence of N observations, X, X, , X making up a time series as a realiza- 1 2 N tion of jointly distributed random variables are usually taken at discrete time points equally spaced with time interval, Zjkt. In time series analysis, information per­ taining to the time series may be obtained in the time and in the frequency domain. Both domains provide useful engineering and statistical properties to the analyst. Figure 4.2 summarizes a general methodology used in time series analysis. The literature review discussed in Chapter 2 indicated that both time and frequency domains analyses are widely used in engineering analyses of time series. This chapter discusses only the time domain anal­ ysis of time series. In time domain analysis, the first step is to gener­ ate a time series plot. A time series plot is a plot of observations versus time. Visual inspection of the time series plot will often indicate statistical consistency of a time series. Features such as trends, periodicity, and discontinuities in the time series should be appar­ ent. Such features often assist in preliminary assess­ ment and validation of a time series. Validation of a 39 DOMRI N FREQUENC Y

od C < m £ 01 CK (D Ui O r 1 »-t u. 01 en I > Z2 Z (D O I ^ *" Uo . QC

O

0) TIM E TIM E CM HISTOR Y DOMRI N

cc oz CD •- O cr •-• 03 CO cn o z QC UI 40 time series is important if the results obtained from basic descriptive statistical analyses are to be meaning­ ful.

A statistical phenomenon that evolves in time ac­ cording to probabilistic laws is called a . In analyzing a time series, the time series is regarded as a realization of a stochastic process.

The time series to be analyzed can then be thought of as one particular realization produced by the underlying stochastic process. After plotting the time series, basic descriptive statistical properties of the time series maiy be obtained. The mean and the variance are the basic statistical properties of the time series. The mean X of a time series can be estimated by Equation 4.1 as:

I ^ X = E[X ] = lT-2x ('^•l^ t '^ t=l t where N denotes the total number of observations in the time series. X defines the level about which the time series fluctuates. The variance of a time series meas­ ures the dispersion about the mean and is estimated by

Equation 4. 2: 41 2 2 , N (J = E[(X -X) ] =7rT-S(x -X) . (4.2) t N-'t=l t

The between x and x separated by k inter- t t+k vals in time may be estimated by:

C = E[(X -X)(X -X)] k t t+k , N-K

^ t=l t t+k

Equation 4.3 is also referred to as the autocovariance function. Box and Jenkins (1969) suggested that the autocovariance function should be calculated for k=0,1,2, ,K, where K is not larger than N/4. Simi­ larly, the autocorrelation function can also be calcu­ lated from Equation 4.3. In most cases, the autocorrela­ tion function is used to describe the correlation in a time series because it is the normalized form of the autocovariance function. The autocorrelation function of a time series may be estimated by:

r = C /rr^ (4.4) k k' where -1 ^ r i 1 k 42

Since r = r , the autocorrelation function is neces- k -k sarily symmetric about zero, hence it is necessary only to consider that portion of the function for k > 0. In many instances, two separate time series are anal­ yzed jointly and the statistical properties are calcu­ lated. If X , X , , X comprise the observations 12 N from the first time series, and y ,y , ,y comprise 12 N the observations from the second time series, then the cross covariance functions between the two time series of the bivariate process at laig +k can be written as:

C (k) = EC(X -X)(Y -Y)] xy t t+k , N-K _ = Tr S (^ -^>(y -^^ (4.5a) •^ t»l t t+k and

C (k) = E[(Y -Y)(X -X)] yx t t+k N-K = J- y (y -Y)(x -X) (4.Sb) N ^^ t t+k where k=0, 1,2, . N Y = f^?, "t C (k) = C (-k) . xy yx 43

Since C (k)= C (-k), we need only define one function xy yx C (k) for k=0,+l,+2,+ The cross covariance xy function can be expressed in a normalized form. The cross correlation function is a normalized form of cross which is estimated by Equation 4.6

r (k) = C (k)/!^ (4.6) xy xy /^X^Y

where

N 2 CT - V. ^X N- 1 t = l t

N 2 (T> - V,i - V^fv -Y^ ^r N-l J. . +-

The cross correlation function is not symmetric about k=0 since it is not an even function. In general, the statistical analysis of a time series is not complete without examining the stationarity of the time series. In the following section, a brief dis­ cussion of stationarity of a time series is given.

^-•-i Stationarity of a Time Series A time series can either be stationary or non- stationary. In general, if a time series is stationary, its statistical properties -are independent of the time 44 origin. If a time series is non-stationary, its statis­ tical properties are dependent on the time origin. Nel­ son (1972) indicated that stationarity is a very strong condition to impose on a time series since stationary time series rarely exist in practice. A stationary time series may be categorized as either strictly stationary or weakly stationary. Most computations of descriptive statistical properties of a time series assume stationa­ rity. In the case of a non-stationary time series, the method advanced by Box and Jenkins (1976) may be used. This method is discussed in Chapter 7.

A stochastic process x is strictly stationary or t stationary in the strict sense if the higher-order mo­ ments and joint moments of the stochastic process x are t time invariant. For a stochastic process to be strict­ ly stationary, two conditions must be met: 1. the statistics of a process x must be the same t for any time lag k, that is, the statistical prop­ erties of X and x are the same, t • t+k 2. the joint distribution of a process x must be t invariant with regard to a displacement in time. If k and m represent any integers in time lags,

then P (x , , X ) = P (x , , X ). t t+k t+m t+k+m 45

These two criteria ma^^ be used to test whether or not two stochastic processes are strictly stationary. If x and t y represent two stochastic processes, then stationarity t in the strict sense requires that the joint statistics of X and y to be the same as the joint statistics of x t t t+k and y t+k A stochastic process is weadtly stationary if the moments through some specified order are invariant over time. Generally, if the first and second moments of a stochastic process are time invariant, then the sto­ chastic process is weaikly stationary. The general re­ quirements for a stochastic process to be weakly sta­ tionary are: 1. the expected values and the variances are the same for any lag k, that is

E(x ) = E(x ), and t t+k Var(x ) = Var(x ) t t+k 2. the autocorrelation depends only on time lag m, i.e.,

E[(x -X)(x -X)] = C . t t+m m The above criteria can be extended to two causally re­ lated stochastic processes. For two causally related 46 processes to be weakly stationarity requires that: 1. the cross correlation between two processes de­ pends only on time lag m, i.e.,

E[(x -X)(y -Y) = C (m). t t+m xy It is impossible to obtain a physical time series which is strictly stationary. Most physical time series are nonstationary in nature or at the very most, weakly stationary. In order to apply Equations 4. 1 through 4.6, it is necessary to assume or to obtain a time series which is weakly stationary. There are other available statistical methods of checking for stationarity of a stochastic process. The method proposed by Box and Jen­ kins (1976) is discussed below. Box and Jenkins (1976) suggesLcd using autocorrela­ tion plots as a means to check for stationarity. In general, a stationary time series tends to have an auto­ correlation function which dies off rapidly with in­ creasing time lags. The autocorrelation values are con­ sidered to be zero at laig greater than q if

^ 2 1/2 |r 1^ 2/fr: [l+2y!r] j>q- (4.7) .i "^/N it^ i 47

In many instances, if a time series is not stationary, the autocorrelation function tends to have high numerical values at large time lags. In other words, the auto­ correlation function dies off with increasing time lags very slowly, if at all, for a non-stationary time series. High values of the autocorrelation function at high time lags indicate that some form of non-stationarity exists. In many cases, taking the first difference of a non- stationary time series will often produce a stationary time series. This technique is used widely by statisti­ cians to model stationary time series from actual time histories which are non-stationary because the mathe­ matics involved in taiking the first difference of a non- stationary time series are less complicated. The auto­ correlation of the time series produced by taking the first difference of the original time series tends to die off rapidly if this results in a stationary time series. In general, a set of new observations is generated by first differencing of the original time series. The first difference of the original time series may be written as

z = X - X (4.8) t t t-1 48 where z is the new observation at time step t. A t complete discussion on time series modeling is given in Chapter 7.

4.5 Selected Time Histories Table 3.1 provided information regarding record num­ bers, dates, and times when the instrumentation system was activated, mean wind directions, and mean wind speeds during the recording process. Among these twenty-three available records, N04 and N14 represent zero wind speed recordings. The selected records used for analyses in the re­ search reported herein are shown in Table 4.1. Records N07, NOS, and N16 were recorded during west winds. Record NOS was recorded during an east wind. Four crite­ ria were used in selecting records NOS, N07, NOS, and N16. These criteria are: 1. One record with the highest mean wind speed from all west wind records was selected, i.e., record N07. 2. One record with the second highest mean wind speed from all west wind records was selected, i.e., record NOS. 49

Table 4.1 Selected Records for Analysis

Mean Wind Mean Wind Record Date Time Direction Speed (Degrees) (Meters/Second)

NOS 12/16/81 16.10.28 93.0 15.79 NO? 01/16/82 19.04.51 215.0 22.31 NOS 01/31/82 01.36.32 282.0 21.42 N16 03/12/82 15.13.50 220.0 9.99

Note: Wind speeds are monitored at 34.7 m height so

3. One record with the lowest non-zero mean wind speed from all west wind records was selected, i.e., record N16. 4. One record with the highest mean wind speed from all east wind records was selected, i.e., record NOS. Records NO? and NOS were obtained through the automatic triggering of the data acquisition system. On the con­ trary, records N16 and NOS were obtained by manually triggering the data acquisition system. In general, record NOS is from the WNW direction, record NO? is from the WSW direction, record N16 is from the SSW direction, and record NOS is from the east direction. The time history plots for one second interval averaiges of wind speeds at 34.7 m height are shown in Figures 4.3a, 4.3b, 4.4a, and 4.4b. Associated with these wind speeds, the time history plots of the conductor load values (LCOS, LC04, and LCOS) for west, east, and center conductors are given in Appen­ dix A (Figures A.1 through A.6). Similarly, the time history plots of the associated swing angles of the conductors (SAOS through SAIO) are shown in Appendix A 51 NOS. WSOS la/ia/Bi «.J0.j* nor BTTc 00/07/W INST. MI - la.u ira Tt>« - l.2flT UN 15.7« »n IHT. im s I6.7S ITS TOt = I.2S] KIN leT ST1I EV o.a »n Iter. MiN - it.zz m TtJt - S.UW RIN iwr TTOcev iKT. MIN - m.37 m T[>€ - S.SQO HIN M« »»TV1IIT 10 TIfC HISTIKT POR 1.000 XCtfO IKTBrfPL RVEKflGES Rn

(D 0. N

2 d-i UJ a. a

10 12 TIME (MINUTES!

Figure 4.3a Time History for Wind Speed at 34.7 m for Record NOS

N07.WS05 oi/ifl/aa ia.o«.si Nim attu rtar r««Mtcim JiMr IH<^ Hr=9i.Hr=9l.7 Nn fTDT UHlt OO/IIT/TJU «.51 tri wax. KW - 32.B i« TT>« - i.flsa NtN »€«» 3.70 r« IKT. HTK = 31.81 ITS TDC = 2.967 KIN IBT STU OEY = INST. MIN - 8.99 m ^Mr. - i.ryn NIN Iin 3TTJ DfV • 3.aj m INT. NiN - ta.aa m TI>€ - 7.OBI HIN Mfi PTVm • to TIW HI3TBRT R» 1.000 SECtJK] IHTERIPl RVtHCES

q a s TIME (MINUTES)

Figure 4.3b Time History for Wind Speed at 374 m for Record NO? 52 NOS. WSOS 01/31/82 01.38.32. Mi»a 3Tcn rior FNUWCIEK JO-* IB/H m=»i.maw. 77 N nor ORTC 0B/TJ7/'W IN3T. mx - 29.33 ITS TTM: - 0.733 KIN «(3R im? w-3 IMT. ¥F9. = 2B.73 HP3 TI>C = 0.750 NIN INSr STTJ DEV = 3.13 fTS INST. WN - B.os rr3 TDt - B.Rn NIN INT 5TD OCV - 3.0D ft-3 INT. NIN - fl.aa MPS TOt. - 1.883 NIN NW PT3/IirT • 10 TIW KISTORT RK 1.000 SECOO (MTEm. flVERnCES

TIME (MINUTESl

Figure 4.4a Time History for Wind Speed at 34.7 m for Record NOS

N16.WS05 03/13/82 1S.13.SQ. MiMi JLEU rtar muuciiK JD-* IB/^ Mr=w.7 N nor nmc 0B/TJ7/TJO 0.99 wa IM3T. MW - 13.3t Tt>e - l.isa NIN »CPM IMT. HPK = (3.21 m TOC = B.167 NtN tier 3Tn IEV 1.23 trs 1.33 m INST. MIN > B.BB m TTfC • S.02S UN INT STO otv INT. NIN - NPS TI>€ - 1.033 NIN fW PTS/JNT 10 Tl« HISTOTT MR 1.000 SECOO IMTEmn. RVCKflGES

to

== I*-

liJ a(n "^kAr^/^i^

-T 10 12 TIME (MINUTES)

Figure 4.4b Time History for Wind Speed at 34.7 m for Record N16 S3

(Figures A.7 through A.IS) and the time history plots of selected strain gages are shown in Figures A.19 through A.26. All the time histories plotted in Appendix A are for selected channels only. These channels are used for analysis purposes in subsequent sections. The selected channels are WSOS for wind speeds, LCOS-LCOS for conduc­ tor loads, SAOS-SAIO for swing angles, and SGOS, SG06, SGll, and SG12 for strain gages. Except for the selected strain gaiges, all other selected channels are used as inputs to the transmission tower structural system. The selected strain gages are used as outputs or responses from the transmission tower structural system. Strain gaiges 5 and 6 were mounted on the main member and the diaigonal member on the southeast corner of the transmission tower, respectively. Strain gaiges 11 and 12 were mounted on the main member and the diagonal member on the northwest corner of the transmission tower, res­ pectively. Earlier research by Norville, Mehta, and Farwagi (1984) in validating wind and response related data indicated that strain readings recorded by strain gages 3, 4, 7, 9, and 10 were erroneous. The most viable choice is to select strain gaiges 5 and 6 because both of these strain gages are located on the southeast corner. 54

Further, strain gage 5 is mounted on the main leg member whereas strain gage 6 is mounted on the diaigonal leg member. Similarly, strain gaiges 11 and 12 are selected because they are located on the northwest corner of the transmission tower. Additionally, strain gage 11 is mounted on the main leg member whereas strain gage 12 is mounted on the diagonal leg member. Figure 4.5 shows the locations of the selected strain gaiges.

Table 4.2 gives the mean values of the selected load records from the conductor. Table 4.3 gives the mean of the swing angles associated with the conductor motions in which the conductor is capable of swinging in the longi­ tudinal and transverse directions. Since the conductors can swing freely in the longitudinal and in the trans­ verse directions, the mean transverse and longitudinal load values are summarized in Table 4.4 and in Table 4.5, respectively. Table 4.6 gives the mean of the selected stresses from the strain gages mounted on the trans­ mission tower structural members. In Table 4.2, differences in load values for the same load cell can be attributed to different wind speeds and wind directions which affected the swing angles. Table 4.3 presents the results of mean swing angles. In Table 4.3, the mean swing angles associated with the 55

SGll (NW 2 Main) SG12 (NW 3 Dia) NW- -NE

N

<> SW- •SE SGOS (SE 2 Main) SG06 (SE 3 Dia)

Figure 4.5 Locations of Selected Strain Gages for Analysis 56

Table 4.2 Mean Load Values From The Conductors (kN)

Load Cell Records Number NOS NO? NOS N16

LCOS 29.00 27.07 28.41 28.85 LC04 26.25 28.09 28.26 28. 58 LCOS 28.25 27.28 28. 15 28. 16

Table 4.3 Mean Swing Angles (Degrees)

Swing Angle Records : Number NOS NO? NOS N16

SAOS 0.88 -0.49 -0.28 0. 19 SA06 -8.30 9.02 7.67 -1.25 : SAO? 1.59 1.08 1.58 1.96 : SAOS -2.02 9.99 19.98 5.97 : SA09 2.85 1.99 2.95 2.94 : SAIO -5.34 8.50 11.49 1.99 : 57

Table 4.4 Mean Transverse Load Values From the Conductors (kN)

Load Cell Records Number NOS NO? NOS N16

LC03 -2.84 2.82 5. 15 0.72 LC04 -2.62 2.80 4.82 0.80 LCOS -2.77 2.94 5.47 0.81

Table 4.5 Mean Longitudinal Load Values From the Conductors (kN)

Load Cell Records Number NOS NO? NOS N16

LC03 0. 30 0.70 0.60 0.40

LC04 0.25 0.50 0. 26 0. 35

LCOS 0. 12 0.60 0.39 0.37 58

Table 4.6 Mean Leg Stresses of the Transmission Tower Due to Wind and Total Conductor Loads (MPa)

Strain Gage Records ; Number NOS NO? NOS N16

SGOS -7.02 6.04 14.01 1.49 : SG06 0.59 -0.49 0.58 1.97 : SGll 8.64 -3.46 -14.69 0. 41 : SG12 0.59 -1. 16 -0.66 0.23 : 59 the transverse direction for swing angle indicators SA06, SAOS, and SAIO are generally larger than the mean swing angles associated with the longitudinal direction for swing angles indicators SAOS, SA07, and SA09 for the selected records. Since the transverse swing angles are larger than the longitudinal swing angles, it is expected that the transverse loads from the conductors are gener­ ally larger than the longitudinal loads from the same conductors. Negative values of the swing angles indicate that the conductors are s\faying to the west. Table 4.4 presents the mean transverse loads from the conductor. The transverse load at any instant is calcu­ lated by the following equation:

F = P(coscb)sin9 (4.9) T where P is the total conductor load recorded by the load cell, (b is the longitudinal angle recorded by the longi­ tudinal swing angle indicator, and Q is the transverse angle recorded by the transverse swing angle indicator. The highest transverse loads amongst the selected records occurred in record NOS. Table 4.5 presents the mean longitudinal loads from the conductor. The horizontal load at any instant is 60 calculated by the following equation:

F = P(sincb)cos9 (4. 10) H where P,

4. 6 Autocorrelation of Selected Time Histories In this section, only autocorrelations of selected time histories are described. In particular, one west wind and one east wind record are used as examples of the autocorrelation functions for all time histories. The autocorrelations of records NOS and NOS are described in this section, whereas the autocorrelations of records NO? and N16 are shown in Appendix B. As described in section 4.2, the autocorrelation function is a normalized version of the autocovariance function. The autocovariance function given in Equation 4.3 states that the covariance between observations X t and X is the expected product of their deviations from t+k the mean of the time histories. Qualitatively, if a higher than averaige observation tends to be followed by another higher than averaige observation k periods later, and likewise for lower than averaige observations, then the autocovariance between X and X is positive. The t t+k autocovariance is negative if a higher than average ob­ servation tends to be followed by a lower than average observation k periods later and vice versa. Such an interpretation of the autocorrelation function plots of a time series aids in understanding the nature of the time series. 62

If the original time series are stationary, further differencing of the original time series will produce another stationary time series. In other words, the autocorrelations of the original and first differenced series cut off and die off rapidly. The general auto­ correlation shapes for the original and first difference series would then be approximately identical to each other if the original series is stationary. In all the autocorrelation functions plots presented herein, two horizontal lines representing two standard errors are plotted. These two lines which are slightly above and below zero correlation horizontal line represent Equation 4.7. In most cases, it was found that the autocorrela­ tion values are considered zero beyond 150 to 300 lags.

The autocorrelation functions of the wind speed (WSOS) for records NOS and NOS are shown in Figures 4.6a and 4.6b, respectively. In both figures, the autocorre­ lation functions are plotted for the original and first differenced series of WSOS. For both records, all obser­ vations for the wind speed were used to calculate the autocorrelation values. In both plots, the autocorrela­ tion functions of the original wind speed time series die off very slowly. On the contrary, the autocorrelation functions of the first differenced series die off 63 AUTOCORRilATION VALUES OP N05.WS06 OMioouL Aim rasT oarxiatnx SMRTSS FOM ISO LACS SAMPUHeJUTM m tOSPS

Original

First Differenced

y^\/\,f*j\^y^'-'-i^^\^ry

-ca •p^T^TT^^^yTTTT w IB If w^»tPWf>yT^wryy^>YT^^py^N^yy^TWtft^ ^^^T'^rvw^rv

Lua.x Figure 4.6a Autocorrelation Functions of Original and First Differenced Series of WSOS for Record NOS

iUTOCORBELATION VALUES OF N08.WS05 CMOHAL Aim FVfST DOTSKMMC* SKWSS rOM 160 LAGS SAUPWfC XAJM " to SPS

tL* Original

•.I

•L2 First Differenced

na y^v\,j^-^Vy^\/\,^

-t.a ^^^^^^^^yy^i m i» n'w ••! •••^^y w^w^r^^yv^^^^^tn y> »m»• >• |• ^^^r^rn w *i ••yi ry tOB UB lAOS. r

Figure 4.6b Autocorrelation Functions of Original and First Differenced Series of WSOS for Record NOS 64 rapidly. The autocorrelation function of the original wind speed time series indicate that the wind speeds for records NOS and NOS are non-stationary. Similarly, Fig­ ures B. la and B. lb in Appendix B indicate that the wind speeds for records N07 and N16 are also non-stationary. The first differenced series of WSOS for records NOS, N07, NOS, and N16 intersect zero between 5 to 10 lags for the first time.

Next, the autocorrelation functions of conductor loads are calculated using all the observations available in the load cell time histories. The plots of the auto­ correlation functions of conductor loads for records N07 and N16 are given in Appendix B. The autocorrelation functions of the original and first differenced series of load cell (LCOS) for record NOS are shown in Figures 4.7a and 4.7b, respectively. Periodic fluctuation is noticed in the autocorrelation function of the original time history. The autocorrela­ tion function of the original time history dies off very slowly. On the contrary, the autocorrelation function of the first differenced series dies off with increasing lag in a periodical manner. The term "die off" in the con­ text presented herein refers to autocorrelation functions which exhibit gradual decrease in magnitude of the 65 AUTOCORRELATION VALXJBS OF NOft.LCOS ouaiNAL sours FOR tso LAGS SAMPlUfC JUIM m (OSPS

LB IB UBxr

Figure 4.7a Autocorrelation Functions of LC03 for Record NOS

AUTOCORRHAnON VALTJBS OF H0ft.LC03 FIRST DlFTKUFHCg SBUTS rOH 100 LAGS SAUPLUfC JIAJM ^ tOSPB

i.t

•.t

ft.a

LiLJLtilll. It .t. tj. tf jk !ii ,,iMtm «.• iiiiii'U ifrii.tiriiiijii nil If Ji.'iriii-iwiiiiii']fli';rii,ii'ij livi [|M[ii(fpr !'* MI '^ ^

-*.» 1 1 1' m tm iM Laos, K

Figure 4.7b Autocorrelation Functions of First Differenced Series of LCOS for Record NOS 66 correlation with increasing time lag. This decrease in magnitude of the autocorrelation functions can be rapid or slow with increasing time laig. Further, the auto­ correlation functions can decrease in magnitude either positively, negatively, or even in a daanped sinusoidal fashion.

The autocorrelation functions of the original and first differenced series of load cell (LC04) for record NOS are shown in Figures 4.Sa and 4.Sb, respectively. The autocorrelation function of the original time history exhibits periodical fluctuation and dies off very slowly. On the contrary, the autocorrelation function of the first differenced series dies off in a periodical manner. The autocorrelation functions of the original and first differenced series of load cell (LCOS) for record NOS are shown in Figures 4.9a and 4.9b, respectively. Again, the autocorrelation function of the original time history dies off slowly and exhibits a periodic fluctua­ tion. Also, the autocorrelation function of the first differenced series dies off in a periodic manner. The autocorrelation functions of the original and first differenced series of LCOS and LC04 are shown in Figures 4.10a and 4.10b, respectively. In both plots, the autocorrelation functions of the original time 67 AUTOCOBSELATION VALUES OF N0ft.LCC4 oaiaitAL ssFiss rott mo LACS SAMPLUteJUTM' tOSFS

\r Figure 4.Sa Autocorrelation Functions of LC04 for Record NOS

AUTOCORBEUnON VALUES OF N05.LC04 pmsTDifrKxgfrcK sgRas ron tso LAGS SAuruKCJuram tosps i.a

a.t

OJ

prFF"

-•.a rw999^wwjww9% m9mw^m^r^^wwfw^^wwww9y^^9^^9t9 p ninmifi^iBw >»•! i m i» iAes.r

Figure 4.8b Autocorrelation Functions of First Differenced Series of LC04 for Record NOS 68 AUTOCORRELATION VALVES OF NOft.LCOft oaiGif/AL ^iias roR iso LAGS SAUPLUfCJUTM - tOSPS

1.8 4

«k«

a.a

^pwv^r^i^^ww^wqr* F^PW*Y»^fT.W*.*T^rw»».ww^ \r Figure 4.9a Autocorrelation Functions of LCOS for Record NOS

AUTOCORREIATION VALUES OF N0&.LC09 FasTDOrxxgircs sgnas /CM tao LAGS SCAUrUMCJUTM' tOSPB

-«.a

LtBa,X

Figure 4.9b Autocorrelation Functions of First Differenced Series of LCOS for Record NOS 69 AUTOCORRELATION VALUES OF }}OS.I C03 SNCS^AL SBSIS^ rr>K fSO LACS FmaTDirrsxrNcg stjuws ran iso LACS SAUPUSe JUTM m iOSPS

a.a Original

a.a

a.t

OJ First Differenced

ii7

Ltas.r

Figure 4.lOa Autocorrelation Functions of Original and First Differenced Series of LCOS for Record NOS

AUTOCORRELATION VALUES OF N06.LC04 OUGDIAL SBHaS rOK tao LACS /jRSTlurrKRgfrcs SgRas ran tao LAGS SAUPUHC JUn ~ to SPS La

na Original

a.a

a.1

First Difference a.2

j(iiiiiiiMBiriBiirt«'.jt;tii>'kiiu'tvii*-:i M »* J» « ' t-J* • H \* \

-».» ^•^.^rvT^r^^^* I |l T I" ua *• uea.r

Figure 4.lOb Autocorrelation Functions of Original and First Differenced Series of LC04 for Record NOS 70 histories die off slowly. Also, the autocorrelation functions of the first differenced series oscillate about zero and die off slowly in a periodic manner in both plots. The autocorrelation function of the original time history shown in Figure 4.10a is similar to the auto­ correlation function of the original time history shown in Figure 4.10b. Similarity between the first differ­ enced series of LCOS and LC04 is also noticed.

Figure 4.11 shows the autocorrelation functions of the original and first differenced series of LCOS for record NOS. Again, the autocorrelation function of the original time history dies off slowly in a periodic manner. However, the autocorrelation function of the first differenced series oscillates about zero and dies off slowly in a periodic manner. In Figures 4.7 (a and b) through 4.11, the autocorre­ lation functions of the original time histories die off slowly in a periodic manner. Such periodic variations in the autocorrelation functions may be attributed to the fact that the conductors are oscillating at their own natural frequencies. Since the autocorrelation functions tend to exhibit a periodic cycle or seasonal variation, all the load cell time histories are non-stationary. In most cases, the autocorrelation functions of original 71

AUTOCORREIATION VALUES OF N08.LCC9 oaientdL sgRsts FOR lao LACS nUSTDirTJSXBJf eg SERBS FOR tao LAGS SAurtaejun - to SPS t-»4

Original

•J First Differenced

.«^ rJ.k *2»i II .t.iiiitiii*iiiiit.iic.«,*.«iiiiiiii:tt llJf^lfWlUflUlMW •*ntt

-«.« jvwv^F9^^f^'99m^^^yfw^wwwW9 9wjwwww9wmwwfm a>»aa^»a | w w 9WI a^a ^mww^

lABB. K

Figure 4.11 Autocorrelation Functions of Original and First Differenced Series of LCOS for Record NOS 72 time histories of LCOS, LC04, and LCOS for records NOS, N07, NOS, and N16 indicated two distinct lags due to periodic variations of the autocorrelation functions. These periods are approximately 24 and SO lags ( 2.4 and 8.0 seconds, respectively). The response of the transmission tower is represented in the form of stresses experienced by the structural members. First, the strain readings from the selected strain gaiges mounted on the main leg members (SGOS and SGll) and on the diagonal leg members (SGOS and SG12) are obtained. These strain readings are then converted into stresses using prescribed conversion factors for each strain gage under consideration. All the observations in the time histories of the strain gages were used to calculate the autocorrelation functions of SGOS, SG06, SGll, and SG12. The autocorrelation functions of the original and first differenced series of SGOS and SGll for records NOS are shown in Figures 4.12a and 4.12b. In both figures, the autocorrelation functions of the original time histo­ ries are similar to each other and die off slowly in a periodic manner. On the contrary, the autocorrelation functions of the first differenced series of SGOS and 73 AUTOCORBELATICN VALUES OP N0O.SGO6 QJUOOtAL Am FIRST DOTTRgttar SgRTSS rOM ISO LACS SAUPtOfC RATS - 20 SPS

iifst Differenced

-9.2

-•.«

yvff^F^^rwY'^^^^^^n^^^^^^^^^^^^^^^y^^^^^n^^^

\x

Figure 4.12a Autocorrelation Functions of Original and First Differenced Series of SGOS for Record NOS

AUTOCORREIATION VALUES OP N09.SG11 OMOOULJim FIRST DIFFKRgtlCg SgRTSS FOR ISO LACS SAUPLoreRATg'iasps

i.a4

a.a' Original

ua

a.a

oa First Differenced

m^t *^\^WY * n r»p •A.2

-•.«

-•.a .^ii.i w II H I j |i I 1 1 " *

LU9. K

Figure 4.12b Autocorrelation Functions of Original and First Differenced Series of SGll for Record NOS 74

SGll for record NOS oscillate about zero correlation and die off quickly. Figures 4.13a and 4.13b present the autocorrelation functions of the original and first differenced series of SG06 and SG12 for record NOS, respectively. The auto­ correlation functions of the original time histories for both plots are similar to one another, and are periodic in nature. The autocorrelation functions of the first differenced series for both plots die off in a periodic manner. Figures 4.14a and 4.14b present the autocorrelation functions of the original and first differenced series of SGOS and SGll for record NOS, respectively. Similarities between the autocorrelation functions of SGOS and SGll are noticed. The autocorrelation functions of the origi­ nal time histories die off slowly, wheareas the auto­ correlation functions of the first differenced series die off extremely slowly in a periodic manner. The autocorrelation functions of the original and first differenced series of SGOS and SG12 for record NOS are shown in Figures 4.ISa and 4.ISb. Similarity is again observed for the autocorrelation functions of the original time histories. The autocorrelation functions of the first differenced series in both figures die off 75 AUTOCORRELATION VALUES OP prOfl.S^»« QJUGDUL Jim FIRST DOTgRgtrOf SgRIgS FOR ISO lACS SJUtPUMG RAJg ~ 20 SPS

-*.i ^First Differenced -a.t

-•.a

-a.a • iBBin iaw^aaway • s lAoa.g Figure 4.13a Autocorrelation Functions of Original and First Differenced Series of SGOS for Record NOS

AUTOCORRELATION VALUES OP N00.SG12 OXOOUL Aim FIRST DOTgRMhnS SgRfSS FOR ISO [ACS SAMFlMCRAlg - Sn SPS

I.a4

f»Uly*u^Y »i Y * i? » *

First Differenced

•1 |i..ii..in Iiiii "I ' 0 ••«a«iDOLaDiaM UBS. X

Figure 4.13b Autocorrelation Functions of Original and First Differenced Series of SG12 for Record NOS 76 AUTOCORRELATION VALUE:J OP N08.SGO0 OJUaOiAL Aim FIRST DOTgRgtfCX SgRfSS FOR ISO UCS SAUKJ)ieRAIg^2aSPS

t.a

A.a riginal

ua

a.t First Differenced

tua

a.a

-a-s

-•.t

-a.a

-•.a fV^W^MW^vwwv^if «*^F^^wr*vvvw«^^wvwwv«|«*v««f«««f f ««•» •••^ HiVaMill

uaa,g

Figure 4.14a Autocorrelation Functions of Original and First Differenced Series of SGOS for Record NOS

AUTOCORRELATION VALUES OP N06.SG1 \ OJUODiiLAim FIRSTDOTgRgtia SgRfSS FOR 160 UCS SAHPLUfCRATg - 2A £RS

Original

Ltaa.x

Figure 4.14b Autocorrelation Functions of Original and First Differenced Series of SGll for Record NOS 77 AUTOCORRELATION VALUES OP NOd.SGOd QIUGIHAL Aim FIRST DIFFSRgtfCg SgRTSS FOR ISO LACS SAia>tJJ/eRATg'20SPS

i.a

La t 1 ^^ Original

•.a'

a.t

OLS t I ' 1 JN IT XA fl i aj>. m I

-a.2

-%A First Differenced -a.a

-a.a • ai ai • » ua ua M> M Ltaa.g Figure 4.ISa Autocorrelation Functions of Original and First Differenced Series of SGOS for Record NOS

AUTOCORRELATION VALUES OP N08.SG12 OIUOOUL Aim FIRST DlFFgRgMCg SgRTSS FOR ISO UCS SAUPLU/C RAIg - J0 SPS

La 4 •Original a.a'

ika

a.t

iLa

a.a

-a.i

-a.t First Differenced -a.a

-a.a ...... iH..y»^y^^.i| .11 fi ittwmwwf^w |wi.ii.ii| a a m « toa Ui •> » LtBS, g

Figure 4.ISb Autocorrelation Functions of Original and First Differenced Series of SG12 for Record NOS 78 in a periodic manner. Also, except for the magnitude, the autocorrelation functions of the first differenced series are similar to the autocorrelation functions of the original time histories in both figures. In Figures 4. 12a through 4.15b, similarity between the autocorrelation functions of SGOS and SGll are observed. Also, similarities between the autocorrelation functions of SGOS and SG12 are noticed. This similarity is attributed to the fact that SGOS and SGll are the strain gaiges located on the main members which are oppo­ sitely configured to one another of the transmission tower. Similarly, SG06 and SG12 are located on the diaigonal members which are also oppositely configured to one another of the transmission tower (see Figure 4.5). A periodic trend of approximately 48 lags (2.4 second) was observed for SGOS and SGll, and a periodic trend of 20 lags (1.0 second) was observed for SGOS and SG12 for record NOS. For record NOS, no distinct lag was detected for SGOS and SGOS. However, a periodic trend of approxi­ mately 22 lags (1.1 second) was detected for SG06 and SG12. In all the selected strain gages, the autocorrela­ tion functions of the first differenced series indicate that the values of autocorrelation functions fluctuate about zero. This indicates that apart from differencing 79 the original time histories once, seasonal variations or trend must be considered in modeling the time histories. Finally, the autocorrelation functions of the original and first differenced series of SGOS, SG06, SGll,and SG12 for records NO? and N16 are shown in Figures B.Sa through B.Sb in Appendix B. The last step in time domain analysis involves studying the input and output statistical relationships of the time histories. The studies of these statistical relationships may be achieved through cross correlation functions of the causally related inputs and outputs.

4^7 Cross Correlation of Selected Time Histories In this section, cross correlation functions of the selected time histories are discussed. In particular, only the cross correlation functions between the selected inputs and the selected outputs are considered. The cross correlation functions are described by Equation 4.6. In calculating the cross correlation functions between any two selected time series, the sampling rate for the first time series should be equal to the sampling rate for the second time series. This enables a one to one statistical comparison between the first time series and the second time series. As discussed earlier, only so the cross correlation functions between the time series of the selected inputs, i.e., wind speed and load cells, and the time series of the selected outputs, i.e., strain gages need to be calculated. All the cross correlation functions are plotted for 300 lags (30 seconds) in this section. In calculating the number of cross correlation sets, all possible cross correlation sets between input and output must be considered. In the research reported here­ in, one common notation is used to describe any cross correlation functions between two causally related time histories. For example, the notation WSOS-SGOS is used to represent the cross correlation relating the input time history, WSOS, with the output time history, SGOS. For each record considered, only cross correlation sets between the selected input time histories and the select­ ed output time histories are calculated. Hence, there are 40 possible cross correlation sets. These cross correlation sets are as follow: 1. 4 sets relating wind speed (WSOS) with strain gages (SGOS, SGOS, SGll, and SG12), i.e., WS05-SG06, , WS0S-SG12. 2. 4 sets each relating total load cells values (LCOS, LC04, and LCOS) with strain gages (SGOS, 81

SGOS, SGll, and SG12), i.e., LC03-SG0S, , LC03-SG12, LC04-SG0S, , LC04-SG12, LCOS- SG03, , LC0S-SG12. 3. 4 sets each relating transverse load cell values (LCOS, LC04, and LCOS) with strain gages (SGOS, SG06, SGll, and SG12). The possible combinations in this case are similar to the combinations de­ scribed in 2 above. 4. 4 sets each relating longitudinal load cell values (LC03, LC04, and LCOS) with strain gages (SGOS, SG06, SGll, and SG12). The possible combi­ nations in this case are similar to the combina­ tions described in 2 above. The . transverse and longitudinal load values may be obtained by resolving the total load cell value into its transverse and its longitudinal components vjtilizing the transverse and longitudinal swing angles as described in the previous section. This enables finer details to be seen in calculating the cross correlation functions between load cells (total, transverse, and longitudinal) and strain gages. Since there are 160 possible cross correlation functions for all 4 selected records, only cross correlation functions of significant importance are presented. Most of the plots of the cross correlation 82 functions of the total load values from the conductors and the strain gaiges for the selected records which are not given in this section are given in Appendix C. Figures 4. 16a and 4.16b present the cross correlation functions relating WSOS with SGOS and WSOS with SG06, respectively, for record NOS. The cross correlation function relating WSOS with SGOS is negatively corre­ lated, dies off with increasing lag, and peaks at zero lag. The cross correlation function relating WSOS with SG06 for the same record does not peak at zero lag and the magnitudes of the cross correlation function are relatively smaller compared to the cross correlation function relating WSOS with SGOS for any time lag. This indicates that the wind speed has an immediate effect on the main members of the transmission tower. There is a time laig involved before the diaigonal members experience the effect of the wind speed since the cross correlation function relating WSOS with SG06 does not peak at zero laig. In the context presented herein, "time lag" refers to the time taken for the cross correlation functions to achieve an absolute maximum numerical value. Similar­ ly, the effect of the wind speed on the main member is more significant than the effect of the wind speed on the CBOSS CORSSIATION BBTWESN M09.WS0gMm M4.SC0S 83 SdMPUirajurs • t4 SPS

Figure 4. 16a Cross Correlation Functions of WSOS and SGOS for Record NOS

CROSS CORSBIATION BffTYEEN iR>e.gse6Afm Mog.soot aAMPUNoiun 3 f SPS

Figure 4.16b Cross Correlation Functions of WSOS and SG06 for Record NOS 83 CROSS CORRSUTION BKTWESN SAMFfJltaiUTg m to SPS

Figure 4.16a Cross Correlation Functions of WSOS and SGOS for Record NOS

CROSS CORRELATION BETWEEN ARM. WSOS AND MOO.SCOO aAMPUHaiLATB = to SPS

Figure 4. 16b Cr^^ss Correlation Functiuas uf WSOS and SG06 for Record NOS 84 diagonal member since the cross correlation function relating WSOS with SGOS has a larger maignitude. Figures 4. 17a and 4.17b present the cross correlation functions relating WSOS with SGOS and WSOS with SGll, respectively, for record NOS. The cross correlation function relating WSOS with SGOS is positively corre­ lated, and it does not die off quickly with increasing lag. On the contrary, the cross correlation function relating WSOS with SGll is negatively correlated. Fig­ ures 4.17a and 4.17b are similar to one another but in an opposite sense. The cross correlation functions for both cases have peak values at approximately zero laig. The cross correlation functions relating WSOS with SGOS and WSOS with SG12 for record NOS are shown respec­ tively in Figures 4.ISa and 4.18b. In both cases, the cross correlation functions are negatively correlated, and they are similar in shape. Also, the cross correla­ tion functions for Figures 4.18a and 4.ISb do not peak at zero lag. Figures C.la through C.4b in Appendix C give the plots of the cross correlation functions relating wind speed with strain gaiges for the selected records not shown in this section. Higher magnitudes of the cross correlation functions are observed relating wind speed with strain gages 85 CROSS CORRELATION BPTVEEN ifOO, WS09 Aim lt0t.SC06 SAMPUNC KATE • tO SPS

4.7

%l

a.a I • a laa iia ua Ma JM SB aa

Figure 4.17a Cross Correlation Functions of WSOS and SGOS for Record NOS

CROSS COREtEUTION BETWEEN MM. WSOS AND itOa.SCI t SAMPfJNClUTg - to SPS

ILO

-aa

-i 0 I I } I I " I I M • • LSi la lao tia

Figure 4.17b Cross Correlation Functions of WSOS and SGll for Record NOS 86 CROSS CORRELATION BTTWESN »IM.WS08 AND JfOt.SCOt SAMMJNOIUTt = to SPS -aku

-a IB •*.»

-aa -«a ^a

A m tt M IB lii IM ail M

Figure 4.ISa Cross Correlation Functions of WSOS and SGOS for Record NOS

CROSS CORREUTION BETWEEN )foo.wsosANDint.seit aAldFUHClUTB » to SPS

Figure 4. 18b Cross Correlation Function.s of '-JoOo and SG12 for Record NOS 87 mounted on main leg members of the transmission tower than with strain gaiges mounted on diagonal leg members of the transmission tower for records NOS and NOS. On the contrary, higher magnitudes of the cross correlation functions are observed relating wind speed with strain gages mounted on diagonal leg members of the transmission tower than with strain gages mounted on main leg members for records NO? and N16. The cross correlation functions relating wind speed with strain gages mounted on main leg members of the transmission tower peak almost immediately for records NOS and NOS. However, the cross correlation functions relating wind speed with strain gages mounted on diaigonal leg members of the transmission tower do not peak imme­ diately but at a later time. Lag times of approximately 3.0 and 21.0 seconds are observed for record NOS and NOS, respectively. On the contrary, the cross correlation functions relating wind speed with strain gages mounted on both main and diagonal leg members of the transmission tower peak almost immediately for records NO? and N16. This means that the effect of wind speed is felt by both main and diagonal leg members immediately for records N07 and N16. If the cross correlation functions relating WSOS with SGOS are positively correlated, then the cross 88 correlation functions relating WSOS with SGll are nega­ tively correlated and vice versa. This relationship is expected since SGOS is located on the southeast corner of the transmission tower and SGll is located on the north­ west corner of the transmission tower (see Figure 4.5) and they are located diagonally opposite to one another. However, if the cross correlation functions relating WSOS with SGOS are positively correlated, then the cross cor­ relation functions relating WSOS with SGI2 are also posi­ tively correlated and vice versa. The next set of inputs to consider are the load cell values. The cross correlations relating load cells with strain gaiges may be performed for three cases. First, the cross correlations relating total load values with selected strain gaiges are performed. Second, the cross correlations relating longitudinal load values with se­ lected strain gaiges are performed by resolving the total load values into their longitudinal components utilizing the respective swing angles. Finally, the cross correla­ tions relating transverse load values with selected strain gaiges are performed by resolving the total load values into their transverse components utilizing the respective swing angles (see Equation 4.8). 89

The cross correlation functions relating load cells with strain gages may be obtained by first considering the total load values. The total load values are the load values obtained from the instrument without con­ sidering the effect of swing angles. The cross corre­ lation functions relating LC03 with SGOS and LCOS with SGOS are shown respectively in Figures 4.19a and 4. 19b for record NOS. The cross correlation function relating LCOS with SGOS indicate a definite periodic correlation. This periodic correlation tends to oscillate back and forth from negative correlation to positive correlation about the maignitude of zero correlation. Similarly, the cross correlation function relating LCOS with SGOS also indicates a definite periodic correlation. For both cases, the time taken from peak to peak of the cross correlation functions is about 25 laigs (2.5 seconds). Figures 4.20a and 4.20b present the cross correlation functions relating LC04 with SGOS and LC04 with SG06, respectively, for record NOS. Both cases indicate defi­ nite periodic correlation. Figures 4.21a and 4.21b present the cross correlation functions relating LCOS with SGOS and LCOS with SG06, respectively, for record NOS. Again, periodic correla­ tion occurs in both cases. Comparison is made between CROSS CORRBIATION BETWEEN RO^UOafTOtAL) Am ilO0.SG06 90 SAUPUHOHJOB - fO SPS

Figure 4.19a Cross Correlation Functions of Total Load Values From West Conductor and SGOS for Record NOS

CROSS CORRELATION BETWEEN MOgJJCOa(TtJtAL)AilD HOO-SOOO aAMPUWRATE m tO SPS

Figure 4.19b Cross Correlation Functions of Total Load Values From West Conductor and SG06 for Record NOS CROSS CORRELATION BETWEEN 91 JMiCX£0

Figure 4.20a Cross Correlation Functions of Total Load Values From East Conductor and SGOS for Record NOS

CROSS CORRELATION BETWEEN M00.£C04(T0tJiL) AJID MOO.SCOO SAMPintaiufB - to SPS

Fi.^ure 4. 20b Cross Correlation F'lnctions of To^.^.l Load Values From East Conductor ana SGC6 for Record NOS 92 CROSS CORRELATION BETWEEN H00.LCWS(TOtXL) AilD NOH.SGOS SAJUPLDfaiUTB » ^« SPS

-«L00

Am

i ^la l-^iM

-aia

w^^^^^^^^r^ • a tt tt la liA III 311

Figure 4.21a Cross Correlation Functions of Total Load Values From Center Conductor and SGOS for Record NOS

CROSS CORRELATION BETWEEN g00.lC09(TOtAL) Aim MOO.SGOO SJUUPUJtaiUTB - *0 SPS

Figure 4.21b Cross Correlation Functions of TJ-.3I1 Load Values From Center Conductor and SG06 for Record NOS 93

Figures 4.19a, 4.20a, and 4.21a. No similarity in the shape of the cross correlation functions is noticed. Similar observation is obtained when comparison is made between Figures 4.19b, 4.20b, and 4.21b.

Discussion is now made pertaining to the cross corre­ lation functions relating total load values from the conductors with the strain gaiges. In Figures 4.19a through 4.21b, periodical cross correlation is expected because the conductor tends to oscillate at a certain frequency about its point of attachment when subjected to wind forces. Also, the cross correlation functions rela­ ting total load values from the conductors with the strain gages peaJk almost instantly. In general, the time taken from pealt of the cross correlation functions relating total load values from the conductors with strain gages is shorter for the strain gages mounted on the diagonal leg members than for those on the main leg members of the transmission tower. The cross correlation functions relating LCOS with SGOS and LCOS with SG06 for record NOS are shown respec­ tively in Figures 4.22a and 4.22b. In both cases, the time taken from peak to peak of the cross correlation functions is approximately 10 lags (1.0 second), and the cross correlation functions are periodic in nature. The 94 CROSS CORREUTION BETWEEN g0g.LC03fTOnL) AM) mO^SGOS SAidnorasAis - to SPS

Figure 4.22a Cross Correlation Functions of Total Load Values From West Conductor and SGOS for Record NOS

CROSS CORREUTION BETWEEN )Ut,LC0»(TOtiL) AMD MOO.SCOt SAidPinta JUTS - to SPS

Figure 4.22b Cross Correlation Functions o: To'il Load Values From West Conductor and SGOS for Record NOS 95 cross correlation function shown in Figure 4.22b oscil­ lates back and forth from positive correlation to nega­ tive correlation about zero value. Figures 4.23a and 4.23b present the cross correlation functions relating LCOS with SGll and LC03 with SG12, respectively, for record N08. In both cases, the cross correlation functions are periodic in nature. The cross correlation function shown in Figure 4.23a is mainly negatively correlated. Figures 4.24a and 4.24b present the cross correlation functions relating LC04 with SGOS and LC04 with SGOS, respectively, for record NOS. The cross correlation functions in both cases are periodic in nature. Figure 4.24a shows that the cross correlation function is mainly positively correlated. Also, Figure 4.24b indicates that the cross correlation function oscillates back and forth about zero value. The cross correlation functions relating LC04 with SGll and LC04 with SG12 for record NOS are shown res­ pectively in Figures 4.2Sa and 4.25b. The cross correla­ tion functions are periodic in nature in both cases. Similarities are noted when comparison is made for Fig­ ures 4-24b and 4.2Sb. 96 CROSS CORREUTION BETWEEN M0m.LC0a(TOTXL) AMD »O0.SGi 1 SAMPUHOKATB » tO SPS

Figure 4.23a Cross Correlation Functions of Total Load Values From West Conductor and SGll for Record NOS

CROSS CORREUTION BETWEEN )(0a.LC0a(TOtAL) AMD HOO.SGtZ SAUPiaaRATE m to SPS

'l 11 • ••I I" • na

Figure 4.23b Cross Correlation Functions of Total Load Values From West Conductor and SG12 for Record NOS 97 CROSS CORREUTION BETWEEN Ma.I£04fTOtLL) AMD MO0,SO06 SAidPUNaiUTE 'to SPS

-t.fl' I t I I I ta BO la IB aa

Figure 4.24a Cross Correlation Functions of Total Load Values From East Conductor and SGOS for Record NOS

CROSS CORREUTION BETWEEN MOa.LC04(TOTJLL) AMD MOO.SCOt SAUPLOfOJUTS 'to SPS

Figure 4 24b Cross Correlation Functions of To^al Load Values From East Conauoior and SGOS for Record NOS 98 CROSS CORRSUTION BETWEEN M0a.l£04^ntAL) AMD MOO.SGt 1 SJLiOfJMaiUTS • to SPS

ta la aa na

Figure 4.2Sa Cross Correlation Functions of Total Load Values From East Conductor and SGll for Record NOS

CROSS CORREUTION BETWEEN M0t.LC04(TOtiL) AMD nOO.SCtt SAMPLOfOlUTB - tO SPS

UB

Figure 4.25b Cross Correlation Functions of Total Load Values From East Conductor and SG12 for Record NOS 99

Figures 4.26a and 4.26b present the cross correlation functions relating LCOS with SGOS and LC05 with SG06 respectively for record NOS. Again, the cross correla­ tion functions are periodic in nature in both cases. Comparison of Figures 4.22b, 4.24b, and 4.26b indicate that the cross correlation functions are similar to one another. Figures C.Sa through C.lib in Appendix C give the cross correlation functions of the total load values from the conductors and the strain gages for the selected records which are not shown in this section. The general discussions of the cross correlation functions of the total load values and the strain gaiges are now given for west wind records. The cross correlation functions relating total load values from the conductors with strain gaiges mounted on main leg members of the transmission tower peak almost immediately. The time taken from peak to peak of the cross correlation functions is consistently 10 lags or 1.0 second. Little variation is noticed in the shape of the cross correlation functions when the same strain gage is cross correlated with the total load values from different conductors. The cross correlation functions relating a particular total conductor load with the main strain gaiges are alwao's similar but in an opposite sense. CROSS CORREUTION BETWEEN 100 M0t.iJC0a(TOtlL) AMD MO0.SG06 aAMPUHOKATE - tO SPS

^ w *T !'• »*»T

Figure 4.26a Cross Correlation Functions of Total Load Values From Center Conductor and SGOS for Record NOS

CROSS CORREUTION BETWEEN MOt.Leoa(TOtlL) AMD MO0.SO00 aAUPLBtaiUTE 'to SPS

Figure 4.26b Cross Correlation Functions of To^al Load Values From Center Conductor and SG06 for Record NOS 101

Also, the values of the cross correlation functions rela­ ting total conductor loads with strain gages mounted on main leg members of the transmission tower are generally higher than the cross correlation functions relating total conductor loads with strain gaiges mounted on diago­ nal leg members. Finally, the explanation of the period­ ical nature of the cross correlation functions cannot be well accomplished without performing a frequency domain analysis. Any attempt to explain the periodic cycles will be addressed in the chapter dealing with frequency domain analysis. However, if the values of the cross correlation functions are positive, then the input is ahead of the response or output. On the other hand, if the values of the cross correlation functions are nega­ tive, the input is lagging behind the output. Upon obtaining the cross correlation relating total load cell values with strain gaiges, the swing angles of the load cells must be considered. The swing angles enable the load values to be resolved into the longitudi­ nal and transverse components. Next, the longitudinal load values are cross correlated with the strain gages and results obtained can be compared to the results obtained using only total load cell values. This gives 102 an added in-depth analysis into the behavior of the transmission tower system. Figures 4.27a and 4.27b present the cross correlation functions relating LC03 with SGll and LCOS with SG12 respectively for record NOS. In Figure 4.27a, the cross correlation function indicates a definite periodic corre­ lation. The time taken from peak to peak of the cross correlation function is approximately 20-25 lags (2.0-2.5 seconds). Although the cross correlation function is predominantly negatively correlated, small magnitudes of positive correlation occur. The cross correlation func­ tion continue to decrease periodically with increasing lags indicating that correlation eventually dies off with increasing lags. In Figure 4.27b, no definite period can be detected. The cross correlation function tend to oscillates about zero correlation and eventually dies off with increasing lag. The cross correlation functions relating LC04 with SGll and LC04 with SG12 for record NOS are shown respec­ tively in Figures 4.2Sa and 4.28b. In Figure 4.28a, the cross correlation function is negatively correlated, and it eventually dies off with increasing lags. No definite period can be detected. In Figure 4.2Sb, the cross corre­ lation function is negatively correlated. Also, no 103 CROSS CORREUTION BETWEEN Moesa>a(UiNG.)jLjmMoe.sGtt SAMPUNORATS = tO SPS

Figure 4.27a Cross Correlation Functions of Longitudinal Load Values From West Conductor and SGll for Record NOS

CROSS CORREUTION BETWEEN i»eaj£oafi4UfG.) AMB Moe.sGiz SAMPUNOIUTB - tO SPS

Figure 4.27b Cross Correlation Functions of Longitudinal Load Values From West Conductor and SG12 for Record NOS CROSS CORREUTION BETWEEN 104 M0aM»4(L0NG,) AMD M06.SG11 3AMPUK0RATE • tO SPS

Am

i Aa

I^a a,a

'"I T»*'"! |inn f f faia^aya im fnp^y « fl M a la 10 m M M 9ft M

Figure 4.2Sa Cross Correlation Functions of Longitudinal Load Values From East Conductor and SGll for Record NOS

CROSS CORREUTION BETWEEN M0gM»4fL0Ma)AM» M0e.SG1t SAidKBiOlUTt 'to SPS

Figure 4.2Sb Cross Correlation Functions of Longitudinal Load Values From East Conductor ,ind SGl'C for Record NOS 105 definite period can be detected, and the cross corre­ lation function eventually dies off with increasing lag. In the case of west wind record NOS, Figures 4.29a and 4.29b present the cross correlation functions rela­ ting LC03 with SGOS and LCOS with SG12, respectively. The cross correlation functions shown in both figures osci­ llate about zero correlation and they eventually die off with increasing lag. Figures 4.30a and 4.30b present the cross correla­ tion functions relating LC04 with SGOS and LC04 with SGll respectively for record NOS. The cross correlation func­ tion shown in Figure 4.30a is positively correlated, and it eventually dies off with increasing lag. The cross correlation function shown in Figure 4.30b is negatively correlated, and it eventually dies off with increasing lag. Also, the cross correlation function shown in Figure 4.30a is similar, but in an opposite sense, to the cross correlation function shown in Figure 4.30b. Figures 4.31a and 4.31b present the cross correlation functions relating LCOS with SGOS and LCOS with SG12, respectively, for record NOS. In both figures, the cross correlation functions oscillate about zero correlation. Also, the cross correlation function shown in Figure 4.31a is similar to the cross correlation function shown 106 CROSS CORREUTION BETWEEN MOOMafSfLOIfC.) AMD M09.SCOW SAMPLING RATW « 10 SPS

Figure 4.29a Cross Correlation Functions of Longitudinal Load Values From West Conductor and SGOS for Record NOS

CROSS CORREUTION BETWEEN tfOOJJCOS^LONC J AND JVO«.SCtX SAMPLING RATg '10 SPS xa (La xa. a.n ».m xm X9 t,m ba a.a

•«,m

•*m

^^»^'^r^*'F"^^B^^^^^^^^^^^a^^^ '" •!

.,1 Figure 4.29b Cross Correlation Functions of Lotigi •A - Load Values From West Conductor and SG12 for Record NCS 107 CROSS CORRSUTION BETWEEN N90MX4(L0NG.} AND N00.SCOS SAMPtntG RATX ' 10 SPS

CM 1.17 xm %m cm cia

a.aa a.ai ^v^r*T^'^^^T'**T^'**T''^*'^.f^ ^FVX*.*v*VT*v^ Ma

Figure 4.30a Cross Correlation Functions of Longitudinal Load Values From East Conductor and SGOS for Record NOS

CROSS CORREUTION BETWEEN NVJJCOAiLONC) AND UOB^SCII SAMPtntG RATX '10 SPS

-«a

-ft 17

^f^w^^^ \ I rw^^mT^^-^^ I I I I'

Figure 4.30b Cross Correlation Functions of Longitudinal Load Values From East Conductor and SGll for Record NOS 108 CROSS CORREUTION BETWEEN NOOUJCOefLONG.) AND N00.SG09 SAMPLING RATg '10 SPS

Figure 4.31a Cross Correlation Functions of Longitudinal Load Values From Center Conductor and SGOS for Record NOS

CROSS CORREUTION BETWEEN NMLCCOOfUWC.; AND N00.SG12 SAMPLIMGRATg ' 10 SPS

ii 11 I • • I

Figure 4.31b Cross Correlation Functions of Longitudinal Load Values From Center Cond'^ctor and SGI2 for Record NOS 109 in Figure 4.31b. Finally, Figures C.12a through C.15b in Appendix C present the cross correlation functions rela­ ting longitudinal load values from the conductors with strain gages which are not shown in this section.

For all the selected records, the cross correlation functions indicate no definite period. Unless stated, all inferences are valid for the selected records. The cross correlation functions relating the longitudinal load values with the strain gages mounted on main leg members of the transmission tower die off with increasing lag. However, the cross correlation functions relating the longitudinal load values with the strain gages mounted on diagonal leg members of the transmission tower oscil­ late about zero correlation. For record N07, the cross correlation functions relating longitudinal load values with the strain gages mounted on diaigonal leg members aie similar to one another. Finally, the cross correlation functions relating transverse load values with strain gages are performed to complete the time domain input- output analysis. Figures 4.32a and 4.32b present the cross correlation functions relating LCOS with SGOS and LC03 with SGll, respectively, for record NOS. In both figures, the cross correlation functions are periodic in nature and they 110 CROSS CORRSUTION BETWEEN M06.LCOa(TRAMaT.)JND M06.SGOa SAMPUNCIUTS ' to SPS

Figure 4.32a Cross Correlation Functions of Transverse Load Values From West Conductor and SGOS for Record NOS

CROSS CORREUTION BETWEEN MOt.Leoa(TRAM3r.)JND X0e.SGI1 SAMPLOraiUTS ' to SPS

Figure 4.32b Cross Correlation Functions of 'r 11. s verse Load Values From West Conductor and SGll for Record NOS Ill eventually die off. The cross correlation function rela­ ting LC03 with SGOS shown in Figure 4.32a is mainly positively correlated. However, the cross correlation function relating LC03 with SGll shown in Figure 4.32b is mainly negatively correlated. Also, in both figures, the cross correlation functions are similar, but in an opposite sense, to one another.

The cross correlation functions relating LC04 with SGOS and LC04 with SGll for record NOS are shown respec­ tively in Figures 4.33a and 4.33b. The cross correlation function relating LC04 with SGOS shown in Figure 4.33a is positively correlated. However, the cross correlation function relating LC04 with SGll shown in Figure 4.33b is negatively correlated. The cross correlation function shown in Figure 4.33a is similar, but in an opposite sense, to the cross correlation function shown in Figure 4.33b. Figures 4.34a and 4.34b present the cross correlation functions relating LCOS with SGOS and LCOS with SG12, respectively, for record NOS. The cross correlation functions shown in Figures 4.34a and 4.34b are not simi­ lar. Also, the magnitudes of the cross correlation func­ tions shown in Figures 4.34a and 4.34b are relatively 112 CROSS CORREUTION BETWEEN X04.LC04(TRAMar.)AND Jf0(LSCO6 SAMPLBtaRAIS ' tO SPS

Figure 4.33a Cross Correlation Functions of Transverse Load Values From East Conductor and SGOS for Record NOS

CROSS CORREUTION BETWEEN M06.LeoMrRAirsr.)AND MOO^SGI 1 SIAJUPLWaJUTB ' to SPS

-ftOS

I:: i Am

I-fta J.»17 ^a

• •I I la II

Figure 4.33b Cross Correlation Functions of Transverse Load Values From East Conductor and SGll for Record NOS 113 CROSS CORRSUTION BETWEEN Jf06.LC0a(TRAMSr. )JND M06.SCOO SAitPLBiOIUTE - tO SPS

0.0

C4B

a.a

•*.m

-B.ai

a a M a <•

Figure 4.34a Cross Correlation Functions of Transverse Load Values From Center Conductor and SGOS for Record NOS

CROSS CORREUTION BETWEEN JfOALeoa(TRAMSr.)AND M06.SCI2 SAMPLBtaRATE ' tO SPS

-au

-«a

y^^^^^^^^^^^^^^^^^^^^ i»^yT»aa>y»aaii| |iiii 19 la la aa

Figure 4.34b Cross Correlation Functions of Transverse^ Load Values From Center Conductor and SGl^ for Record NOS 114 small in comparison with the maignitudes of the cross correlation functions shown in Figures 4.33a and 4.33b. Figures 4.3Sa and 4.35b present the cross correlation functions relating LCOS with SGOS and LCOS with SGll, respectively, for record NOS. In both figures, the mag­ nitudes of the cross correlation functions are high. Also, the cross correlation functions die off with increasing laig in both figures. The cross correlation function relating LC03 with SGOS shown in Figure 4.3Sa is positively correlated. However, the cross correlation function relating LC03 with SGll shown in Figure 4.3Sb is negatively correlated. The cross correlation function shown in Figure 4.35a is similar, but in an opposite sense, to the cross correlation function shown in Figure 4.35b. The cross correlation functions relating LC04 with SGOS and LCOS with SGOS for record NOS are shown in Figures 4.36a and 4.36b, respectively. In both figures, the maignitudes of the cross correlation functions are high and die off with increasing lag. The cross correla­ tion function relating LC04 with SGOS shown in Figure 4.36a is positively correlated. Similarly, the cross correlation function relating LCOS with SGOS shown in Figure 4.36b is also positively correlated. Th^ cross CROSS CORRSUTION BErWEBN lis Rotj^oacnuNs.) AND Noa.sGoa SAUPLOfajtATE ' to SPS (La 4

0.7

xa

aa

I ^'^^'^^T^^^^^T^^'^'^T^^^^^T^'^*^^ I I i f a ua iM la aia

Figure 4.SSa Cross Correlation Functions of Transverse Load Values From West Conductor and SGOS for Record NOS

CROSS CORREUTION BETWEEN NOgJjCOafTRANS.) AMD N00.SG11 BAMPUHCRATE ' tO SPS

11'

e I

\- a a 17

-1.0' ^««v>»f^w^^^^^wvyv^ivvv>f« rwj^mwwmjnv aaa y T*

Figure 4.3Sb Cross Correlation Functions of Transverse Load Values From West Conductor and SGll for Record NOS CROSS CORRSUTION BETWEEN 116 mgJJC04CFRANS.) AMD N0O.SCO6 SAMPUMO RATS ' tO SPS

Figure 4.36a Cross Correlation Functions of Transverse Load Values From East Conductor and SGOS for Record NOS

CROSS CORREUTION BETWEEN N0gJ£O0(TRANS.) AMD N0a.SGOe SAiOUMa RATE ' tO SPS

0.9

CI

T^^^^^l.i • i i ^^^^^wf^^^'r^T^'w^-^^r^ IIIII I ) I I .i i 11 I I I I a a BiaaiMi^iMMSi

Figure 4.36b Cross Correlation Functions of Trrnsverse Load Values From Center Conductor and -fC^OS for Record NOS 117 correlation functions shown in Figures 4,SSa, 4.36a, and 4.36b are similar to one another. Figures 4.37a and 4.37b present the cross correlation functions relating LCOS with SGOS and LCOS with SG12 for record NOS, respectively. In both figures, the cross correlation functions are periodic in nature, and they are similar to one another. Also, the magnitudes of the cross correlation functions shown in Figures 4.37a and 4.37b are relatively small in comparison with the magni­ tudes of the cross correlation functions shown in Figures 4.35a through 4.36b. The general discussions regarding the cross correlation functions relating transverse load values and strains measured from gages are now given. Unless stated, inferences made are valid for all of the selected records. The maignitudes of the cross correlation functions of transverse load values and strains measured using gages mounted on main leg members of the transmission tower are higher than the magnitudes of the cross correlation func­ tions relating transverse load values and strains meas­ ured using gaiges mounted on diagonal leg members of the transmission tower except for record N07. Record NO? has •significantly higher magnitudes of cross correlation functions relating transverse load values and strains CROSS CORRSUTION BETWEEN lis N0gJ£06(7RANS.) AMD NOa,SGOO aAMPUNORATB ' tO SPS

-OCB .a.

-«.a -ftU -fta e AIM |-o»

|-ai7 j-oa

a a -a,

-aa

1 11 a a SB

Figure 4.37a Cross Correlation Functions of Transverse Load Values From Center Conductor and SGOS for Record NOS

CROSS CORREUTION BETWEEN MOgJ£0«(TRANS.)AMD N0O.SG12 aAltPlBfa RATE ' to SPS

Figure 4.37b Cross Correlation Functions of Transverse Load Values From Center Conductor and SG12 for Record NOS 119 measured using gages mounted on diagonal leg members of the transmission tower when compared with other records. Also, the cross correlation functions relating transverse load values with strains measured using gaiges mounted on main leg members are similar, but in an opposite sense, to one another for the same record. No similarity or trend is observed for the cross correlation functions relating transverse load values and strains measured using gaiges mounted on diagonal leg members for the same record.

The time taken from peak to peaLk of the cross corre­ lation functions relating transverse load values with strains measured for west wind records is approximately 10 lags (1.0 second). On the contrary, no definite lag is noticed for east wind record. Next, discussion of results obtained in this section is given in the follow­ ing section.

4^8 Discussion of Results In this section, the results obtained from sections 4.5 and 4.6 are discussed. Unless stated, the discussions given in this section are valid for all the selected records. The discussions based on the results of the autocorrelation functions presented in section 4.5 are considered first. 120

The autocorrelation functions of the wind speed time histories die off slowly with increasing lag. On the contrary, the autocorrelation functions of the first differenced series of the wind speeds die off rapidly with increasing time laig. This indicates that the time histories of the wind speed are non-stationary, and the first differenced series of the wind speed time histories are stationary. Also, the shapes of the autocorrelation functions of the wind speed time histories are similar to one another for the selected records. The autocorrelation functions of the conductor loads display periodic fluctuation and die off slowly with increasing time laig. Two distinct periodic time varia­ tions of the autocorrelation functions of the conductor loads are obtained. The period refers to the time between peaks of the autocorrelation functions. These two periods are 2.4 and 8.0 seconds. Also, the auto­ correlation functions of the first differenced series of the conductor loads die off in a periodic manner. There­ fore, the time histories of the conductor loads are non- stationary. The autocorrelation functions of the first differenced series of the conductor loads are stationary and periodic in nature. Hence, the time histories of the conductor loads are also periodic, or seasonal, which 121 must be accounted for when the time histories of the conductor loads are modeled in Chapter 7. The general shapes of the autocorrelation functions for LC03 and LC04 are similar to one another for all the selected records. The general shape of the autocorrelation functions of LCOS are not similar to the autocorrelation functions of LCOS and LC04. The autocorrelation functions of the strain records are periodic and die off slowly with increasing lag. On the contrary, the autocorrelation functions of the first differenced series of the strain gages die off with increasing lag. Two distinct periodic time variations are present in these autocorrelation functions. The autocorrelation functions of SGOS and SGll exhibit a period of 2.4 seconds, and the autocorrelation functions of SGOS and SG12 exhibit a period of 1.0 second. The shapes of the autocorrelation functions of SGOS and SGll are similar to one another for the selected records. Similarly, the shapes of the autocorrelation functions of SG06 and SG12 are similar to one another for the selected records. Next, a discussion of the cross correlation functions is given. The cross correlation functions for the selected records are discussed in four ways. First, discussions 122 concerning the cross correlation functions relating wind speed and strain records are given. Second, discussions concerning the cross correlation functions relating total load values from the conductors and strain records are considered. Third, discussions concerning the cross correlation functions relating longitudinal load values from the conductors and strain records are given. Finally, discussions concerning the cross correlation functions relating transverse load values from the con­ ductors and strain records are considered. The two cross correlation functions relating WSOS with SGOS and WSOS with SGll peak immediately. The cross correlation functions relating WSOS with SG06 and WSOS with SG12 do not peak immediately. This indicates that the effect of the wind speed is felt quickly by the main leg members of the transmission tower. However, a certain lag time elapses before the effect of the wind speed is felt by the diagonal leg members of the trans­ mission tower. Also, the magnitudes of the cross corre­ lation functions relating WSOS with SGOS and WSOS with SGll are much higher than the the magnitudes of the cross correlation functions relating WSOS with SG06 and WSOS with SG12, except for record NO?. For record N07, the magnitudes of the cross correlation functions relating 123

WSOS with SG06 and WSOS with SG12 are larger than the magnitudes of the cross correlation functions relating WSOS with SGOS and WSOS with SGll. The former indicates that wind speed is more significant on the response of main leg members of the transmission tower for records NOS, NOS, and N16. The latter indicates that wind speed is also significant in the response of diagonal leg members of the transmission tower for record N07.

The shape of the cross correlation functions relating WSOS with SGOS and WSOS with SGll are similar to one another but in an opposite sense, except for record NO?. For record NO?, the shape of the cross correlation func­ tions relating WSOS with SG06 and WSOS with SG12 are also similar. This supports the observation that wind acting on the transmission tower in the direction which is parallel to the conductors has a relatively higher effect on the response of diagonal leg members of the trans­ mission tower. The cross correlation functions relating total load values from the conductors and the strain gages are periodic in nature and die off with increasing lag. The cross correlation functions relating total load values from the conductors and strain records from main leg members of the transmission tower peak almost instantly. 124

However, a lag time elapses before the cross correlation functions relating total load values and strain records peak. In general, the conductor loads affect the main leg members of the transmission tower first and the diagonal leg members second. The cross correlation functions relating total load values and strain records from main leg members are similar to one another but in an opposite sense for the selected records. Except for record N07, the cross cor­ relation functions relating total load values and strain records from diaigonal leg members are not similar to one another. The cross correlation functions relating longitudinal load values from the conductors and strain records from main leg members show no similarity with one another, except for record N07. For record N07, the cross corre­ lation functions of longitudinal load values and the strain records from diagonal leg members are similar to one another. In general, the effects of the longitudinal loads are not significant to the responses of the main leg members of the transmission tower but are slightly significant to the responses of the diagonal leg members of the transmission tower. 125

The maignitudes of the cross correlation functions relating transverse loads from the conductors and the strain records from the main leg members of the trans­ mission tower are much larger than the maignitudes of the cross correlation functions relating transverse loads from the conductors and the strain records from diagonal leg members of the transmission tower. This indicates that transverse conductor loads have a more significant effect on the response of main leg members than on that of the diaigonal leg member. Also, the cross correlation functions relating transverse load values from the con­ ductors and strain records from the main leg members are similar, but in an opposite sense, to one another for the same record. No similarity or trend is observed for the cross correlation functions relating transverse loads from the conductors and strain records from diagonal leg members for the selected records. In general, the time taken from peak to peak of the cross correlation functions relating transverse load values from the conductors and strain gages is approxi­ mately 1.0 second. Further comments and discussions pertaining to sections 4.5 and 4.6 cannot be completed without considering a frequency domain analysis of the 126 time histories. The frequency domain analysis of the time histories is performed in the following chapter. CHAPTER 5 FREQUENCY DOMAIN ANALYSIS OF SINGLE LOAD AND SINGLE RESPONSE SYSTEM

5. 1 Introduction In the probabilistic analysis of stochastic loads and responses, statistical properties of the loads and responses are used to describe the nature of the loads and responses that may occur in any time interval. Since most structural dynaunic methodologies involve frequency domain analysis, the frequency response functions of the transmission tower structural system is used to investi­ gate the random behavior of the transmission tower in this report. In the dynamic analysis of a transmission tower, the transmission tower is considered to be the structural system. Wind loads acting on a transmission tower and conductor are considered to be the input to the struc­ tural system. In addition, conductor loads acting on a transmission tower at the point of attachment are also considered to be the input to the structural system. The responses, particularly stresses in structural mem­ bers of the tower, of the structural system are consid­ ered as the output from the structural system. The presence of a dynamic relationship between the input and

127 128 the output on the structural system provides a method to predict the response of the structural system. The dynamic response is described in terms of the transfer function relating the loading and the structural re­ sponse. The following section presents discussion of the transfer function of a transmission tower.

5.2 Transfer Function Relating Loads With Responses The dynaunic characteristics of a constant-parauneter linear system can be described by a weighting function h(T ). In particular, the response of a dynamic system with a well defined load producing a well defined re­ sponse is the sum of all the products of the weighting functions, h(T), on the entire time series of the load. The dynaonic model of a linear system, as shown sche­ matically in Figure 5.1, can be estimated from the load time series record x (t) and the response time series 1 record x (t). As discussed earlier, for any load x (t), 2 1 the system response x (t) is given by a weighted linear 2 sum over the entire time series of the load x (t). 1 Therefore, for any arbitrary input x (t), the system 1 output X (t) is given by the superposition or convolution 2 integral as 129

h(r ) Load Transmission Tower Response ^ X (t) Structural System X (t) 1 2

Figure 5.1 Schematic Representation of a Linear System Subjected to a Single Load and a Single Response 130

X (t) = h(r)x (t-r) dr (s.i) 2 1 0 where h(T)=0 for T < 0 for a constant-parameter linear system. The transfer function H(p) for a constant-parameter linear system is the Laplace transform of the unit impulse response function, h(r), which describes the system shown in Figure 5.1. The mathematical relation­ ship between H(p) and h(r ) maiy be written as (Bendat and Piersol, 1980) as: rco H(P) = h(r)e dr (5.2) -^0 where p = a + ib.

The real part of p, which is a, is not restricted to be zero. In Equation 5.2, h(r) describes the system res­ ponse in the time domain, and H(p) describes the system response in the frequency domain. The frequency response function is now denoted by H(f). The frequency response function H(f) described earlier may be obtained by the Fourier transform of h(r). The formulation of the frequency response function is given in subsequent sec­ tion. 131

In a theoretical sense, the frequency response func­ tion of a structural system is unique for particular inputs such as wind loads or conductor loads and outputs such as the stresses experienced by a particular struc­ tural member. If the frequency response function of a transmission tower structural system is known, the re­ sponse of the structural system may be predicted if the time histories of the input or load are known. Similar­ ly, if the frequency response function of a transmission tower structural system is known, the input or load acting on the transmission tower structural system is known if the time histories of the response are known. In formulating the mathematical relationship to calculate the frequency response function of a transmission tower structural system, intermediate steps are involved. These steps are the calculation of power spectra of load and response time series and the cross spectra relating them. The following section deals with the power spectra of a time series.

5.3 Power Spectra of Time Series Any time histories are a measure of some physical quantities with respect to time. Any time series can be expressed as a spectrum having two components. These components of a spectrum as a function of frequency are 132 the amplitude and the phase. The spectrum for a random or non-periodic function can be determined by a Fourier integral transformation. In the analysis of spectrum, the phase information is frequently disregarded because it is dependent on the time origin, and in the analysis of random waveforms the time origin is usually arbitrary. In the case where phase information is disregarded, the most useful spectral property of a time function is its power spectrum. The units of the power spectrum are mean square value per cycle.

The flow chart for frequency domain analysis is shown in Figure 4.2. In frequency domain analysis, the power spectrum of a time history is usually computed first. The power spectrum of a time series represents the rate of change of mean square value with respect to frequency. Usually, the power spectrum is estimated by computing the mean square value in a narrow frequency band at various center frequencies, and then dividing by the frequency band. Spectral density functions can be defined and com­ puted in many equivalent ways. The information obtained from spectral density functions calculated using differ­ ent approaches and methods should be similar eventhough the final numerical values at a particular frequency are 133 different. The power spectrum reported herein is based on the Fourier transform of the autocovariance function of the stochastic process. Since the autocovariance function is an intermediate stage calculation in the time domain, it becomes pratical to derive the power spectral density function based on autocovariance function. The autocovariance function of a stochastic process, X , may be described in a continuous form as t

C (D = lim-r XX dt (5.3) XX T-CD' t t+r

Taking the Fourier transform of Equation 5.3 gives

C (De dr = e X X dt]dr (5.4) XX f T- t t+r

Multiplying the right hand side of Equation 5.4 by -ia)t iCjt e e and rearranging the terms gives nco -i6or -ico(t+r) C (T)e dr =Y X e dt X e dr . (5.5) XX t t+r -CO -CO ^--co The left hand side of Equation 5.5 represents the Fourier transform of the autocovariance function. Similarly, the Fourier transform of x is x e dt so that x e dt t t t is the complex conjugate of the Fourier transform of x . 134

Hence rcx5

Fid)) = X e dt (5.6) t '-CO where the asterisk indicates complex conjugate. The second integral on the right hand side of Equation 5.5 represents the Fourier transform of x Since t is a t+T constant and T is a variable, hence d(t+r)=dT However, X represents x itself with a shift in the time t+r t origin. Therefore, the second integral on the right hand side of Equation 5.5 is equal to the Fourier transform of X . Therefore, t POO -XJOT C (De dr = •F{U))F(OJ) XX T

FiCO) (5.7)

Hence, the power spectral density function of a stochas tic process x may be written as t -ifr (f) = C (De (5.8) 2TT dr XX XX ^-CD where f is used instead of CO to denote frequency. In Equation 5.8, S (f) is an even function, that is S (-f) XX XX 135 is equal to S (f). Therefore, only the positive values XX of S (f) need to be computed. In Equation 5.8, a factor XX of l/2Tf was introduced to preserve the Fourier trans­ form pairs between S (f) and C (T). If S (f) is XX XX XX known, then C (T) may be computed as XX C (D = roo XX ifr S (f)e df (5.9) ^-coX X Equations 5.8 and 5.9 are commonly known as Fourier transform pairs. Equation 5.6 provides the necessary mathematical relationship to calculate the power spectrum of a time series. Other mathematical considerations in calculating power spectrum include usage of spectral windows for smoothing purposes, and the maximum frequency content that will appear in the sampled data. In a time histories of N observations, it is possible to calculate at most N-l autocorrelations. Jenkins (1961) proved that, for finite samples, even if the autocorrela­ tions were exactly known, only a smudged averaige of power spectrum is obtained. Jenkins and Watts (1968) proved that the expected value of sample power spectrum corres­ ponds to a theoretical spectrum viewed through a spectral window. The expected value of the sample power spectrum estimator is written as: 136

CT -i27Tfu E[S (f)] = w(u)C (u)e du (5.10) XX XX '-T where w(u) is commonly known as the lag window. Equation 5.10 relates the power spectrum of a time series to the theoretical power spectrum of the saime time series. The theoretical power spectrum is a mathematical concept which represents the true power spectrum of a time series. In practice, the analyst only obtains the power spectrum of a time series. Therefore, the power spectrum of a time series obtained based on Equation 5.10 is now representative of the theoretical power spectrum. Table 5.1 summarizes four commonly used lag and spec­ tral windows with proper mathematical equations. Based on Table 5.1, the shapes of the lag and spectral windows are shown in Figures 5.2a and 5.2b, respectively. In Table 5.1 and in Figures 5.2a and 5.2b, M refers to the truncation point used in evaluating the autocorrelation functions of a time histories. The spectral window, W(f), can be obtained by taking the Fourier transform of the lag window, w(u). The inverse transform enables the lag window, w(u), to be calculated from the spectral window W(f). The measure which is normally used to characterize the shape of a window is its bandwidth. 13?

Table 5.1 Lag and Spectral Windows (Jenkins and Watts, 1968) Description Lag window Spectral window rectangular H,.C^,.2M('J^). -. ht

Bartlett fi-jjl. H-^(^r lo. |ir| > hi

Tukey sin InfM I iin2»fM(/+ jM) 2fr/A/ "*• 2 2nM{f+iM) lo, l«l > Af I1 sin2TrAf(/- ^M)! 2 2irM(/- IM) / -«(*-^^)(r.aW)' -<^< Parzen '-(^r-(S)- H M •(«) 138

IJ ''^^•^

^^^ ^^v

'^::^ ,•% \x\ ^«is. . ••. \ ^\ \ \\ Rccun

: r-::>:::^ 1 m IM 2M JM AM JJ# MH .IM AM 3M M •

Figure 5.2a Plot of Lag Windows From Table 5.1 (Jenkins and Watts, 1968)

ino

W^f) Recunguter ^df) BanleM I^H/) Tykey . W^f) Parzen

Figure 5. 2b Plot of Spectral Windows From Table 5.1 (Jenkins and Watts, 1968) 139

This bandwidth may be regarded as a filtering operation on the theoretical power spectrum to produce the sample power spectrum. Depending on the spectral window used in spectral analysis, the bandwidth maiy be written as

b =--r- (5.11) MA where b is the standardized bandwidth values given in 1 Table 5.2 when M=ZA=1. The minimum frequency resolution bandwidth available from the data is given by

I b =—T-T • (5.12) e NAt

Finally, the highest frequency that will appear in the saunple time histories data without significant loss of information is given by

f =_4— (5.13)

Equation 5.13 represents the cutoff or the Nyquist fre­ quency. To avoid the possibility of serious errors due to aliasing effects, it is important that the time series 140

Table 5.2 Properties of Spectral Windows (Jenkins and Watts, 1968)

Variance Degrees Standardized ratio of bandwidth Description Spectral window IjT freedom ^

rectangular IM .^ L OJ InfM M

Bartlett MI^^^^Y 0.667^ M \ »/A/ / '5

T-'i- *'('w"rnW) ""T ^«'s 1.333

iM /sin (w/Mmy 0.539 Y 3.71 ^ l.t6 Paraen \ •/M/2 / 141 data have no significant mean square value in the fre­ quency range above f . c Jenkins (1961) indicated that a compromise must be achieved between bias and variance in using a particular spectral window. This compromise may be summarized by using the following equation:

Bandwidth * Variance = constant . (5.14)

From Equation 5.14, small variances are associated with large bandwidths. Similarly, bias is reduced by making M large (Jenkins et al 1968), i.e. small bias is associated with small bandwidths. Jenkins and Watts (1968) sug­ gested using a Tukey spectral window because it is a compromise between Bartlett and Parzen spectral windows in terms of bias and variance. Tukey and Parzen spectral windows are superior over a Bartlett window because a Bartlett window produces large spurious ripples in the mean smoothed spectrum as proven by Jenkins and Watts (1968). Upon obtaining the power spectrum of a time series, it is necessary to calculate the cross spectra of a bivariate time series. A bivariate time series involves two entirely separate time series. The input time series 142 and the output time series constitute a bivariate time series. The formulation of cross spectra is now given in section 5.4.

5. 4 Cross Spectra of Bivariate Time Series This section deals with the frequency domain descrip­ tion of bivariate time series. In particular, the mathe­ matical relationships of the cross spectrum of a load time series, x (t), and a response time series, x (t), as 1 2 shown schematically in Figure 6.1 are discussed. The cross spectrum provides an indication of the regression existing in the frequency domain between two causally related time series. Results obtained from cross spec­ trum analysis of causally related time series provide the analyst with tower response information. The cross spec­ trum provides the necessary tools to formulate the fre­ quency response function of the transmission tower. In the statistical analysis of two causally related time series, the cross covariance function is an intermediate mathematical step in understanding the correlation be­ tween the load and the response time series. The cross covariance function enables the analyst to study the correlation between two causally related load and re­ sponse time series in the time domain. It will be shown in this section that the Fourier transform of the cross 143 covariance function represents the cross spectrum. The cross spectrum is a complex quantity which is comprised of the product of a real function and a complex function. The real quantity is known as the cross amplitude spec­ trum, whereas the complex quantity is known as the phase spectrum. The cross amplitude spectrum indicates how the mag­ nitude of the frequency components in the load time series are related with the amplitudes of the frequency components in the response time series at any particular frequency. The phase spectrum shows if the frequency components in the load time series lag or lead the compo­ nents at the saune frequency in the response time series. The development of cross spectrum is analogous to the development of the power spectrum given in section 5.3. The development of the cross spectrum begins with the cross covariance function. In Figure 5.1, the cross covariance function between load X (t) and response x (t) may be written as: 1 2 T c (r) = 1/T X (t)x (t+r ) dt (5. 15) 12 1 2 0 where T is the time lag. Equation 5.15 is the average of the product of x (t) at time t and x (t+D over an 1 2 144 averaging time T. Theoretically, T should approach infinity but in practice T is finite. The Fourier transform of Equation 5.15 yields the cross spectrum as

CO -i2Trfr S (f) = ' 12 2Tr c (T )e dr . (5. 16) 12 -Leo Equations 5. 15 and 5.16 constitute a Fourier transform pair. S (f) represents a complex quantity as a product 12 of an amplitude function and a phase function and may be written as:

iF,^ (f) S (f) = A (f)e '^ (5.17) 12 12 where A (f) represents the saimple cross amplitude func- 12 tion and F (f) represents the phase function. Evalu- 12 ation of Equation 5.17 requires expressing S (f) as a 12 sum of a real and an imaginary part, that is

S (f) = L (f) - iQ (f) (5.18) 12 12 12 where L (f) is an even function of frequency and Q (f) 12 12 is an odd function of frequency. L (f) is known as the 12 sample co-spectrum and Q (f) is known as the sample 12 quadrature spectrum. 145

The co-spectrum is evaluated as

n L (f) = 1 (r ) cos2Trfr dr (5.19) 12 12 ^-T and the quadrature spectrum is written as ^T Q (f) = q (T ) sin2rrfr dr (5.20) 12 12 where 1 (T) represents the even part of Equation 6.15 12 and q ( T" ) represents the odd part of Equation 6. 15. 12 Finally, the cross aunplitude spectrum may be written as

2 2 2 A (f) = L (f) + Q (f) (5.21) 12 12 12 and the phase spectrum may be written at

F (f) = arctan -[Q (f)/L (f)] (5.22) 12 12 12

The cross spectrum of a bivariate time series must be smoothed using a spectral window in order to reduce the statistical variance. The Tukey spectral window is used to smooth the cross spectrum. The mathematical develop­ ment of a cross spectrum given in this section is now 146 used to develop the frequency response function describe in the following section.

5. 5 Frequency Response Function of a Linear System The problem of estimating the frequency response function of a linear system is considered in this sec­ tion. In time domain analysis, the impulse response func­ tion is used to estimate the behavior of a structural system. An approach utilizing the impulse response func­ tion is more difficult because it involves estimation of too many parauneters. The statistical properties of these parauneters are inconsistent because neighboring estimates of the impulse response function are highly correlated (Jenkins and Watts, 1969). Although the Fourier trans­ form of the impulse response function gives the frequency response function given in Equation 5.2, cross spectral analysis is used to estimate the frequency response func­ tion. Jenkins and Watts (1968) suggest using cross spec­ tral analysis to estimate for the frequency response function because a better estimate is obtained. Consider the input as wind speed or conductor loads and the output as the strain readings from a strain gage mounted on a particular structural member. The trans­ mission tower structural system is then characterized by 147

H(f). The dynamic stochastic model characterizing the load and the response may be written as:

poo X (t)-yW.p h(u) [x (t-u) -/X,] du + Z(t) (5.23) 2 ^0 where h(u) is the impulse response function of the trans­ mission tower structural system and Z(t) is a noise term which is assumed to be uncorrelated with the input x (t). 1 If Z(t) is white noise, then

rOD c (u) = h(V ) c (u-i; )d'V . (5.24) 12 11 ^co The Fourier transform of Equation 6.24 gives

S (f) = H(f)S (f) (5.25) 12 11

where S (f) is the power spectrum of the load. Hence 11

H(f) = S (f)/S (f) (5.26) 12 11

Equation 5.26 is a complex function comprised of a real and an imaginary function. Rewriting Equation 5.26 gives

iF(f) iF:2(f) H(f) = G(f)e = [A (f)/S (f)]e '^ (S.27) 12 11 148 where G is the gain estimator. Equation 5.27 describes the frequency response function of a physically rtjaliza- ble system. The estimators of gain and phase are de­ scribed by Equations 5.21 and 5.22, respectively. Another useful result used to describe system response is the coherence function. The coherence function is a measure of the accuracy of the assumed linear load-response model. For a well defined single load-single response model, the ordinary coherence function will be unity for all frequencies if the structural system is linear and has constant parame­ ters and if there is no extraneous noise at the load source or the response source. The coherence function is given as

2 2 / (f) = {[A (f)]/[S (f)S (f)]>. (5.28) 12 12 11 22 2 where 0 ^ / (f) ^ 1 12

If the coherence function is zero, then the response is a pure white noise. If the coherence function is less than unity, there is a possibility that noise is present in the measurements or the structural system relating the load and the response is not linear and the response could result from other loads than the particular input 149 with which the response is correlated. The final con­ clusion regarding a system response can only be attained by studying the gain function and the coherence function together.

5.6 Illustrations and Applications of FrgqMgngy Rgspons^ FMnQtipn 5.6.1 Power Spectra Plots for Selected Time Histories In this section, power spectra plots for selected time histories are interpreted. In particular, records NOS and NOS are used for illustration purposes. Record NOS is recorded during an east wind and record NOS, during a west wind. Both wind speed records N05 and NOS act almost normal to the conductors and the transmission tower. In addition, records NOS and N08 are associated with high easterly and westerly wind speeds. The power spectra plots in the research presented herein are in the form of the product of spectral density with frequency. Spectral density is a normalized power spectrum which is defined as the ratio of the power spectrum to its variance. The power spectra of wind speed are now discussed. The power spectrum plot for wind speed shows the variation of the energy in the wind fluctuations as a 150 function of frequency. Very often, the gust fluctuations in the wind and the natural frequencies of some struc­ tural systems occur within the same micrometeorological range (Jan, 1982). Interpretation of the wind speed power spectrum plots consists of identifying the fre­ quency ranges over which noticeable peaks or energy occur, and comparing energy levels for different wind records. The power spectra of the wind speed at the 34.7 m height level for records NOS and NOS are shown in Figures S.Sa and 5.3b, respectively. Peaks in the power spectra are noticed between 0.01 and 0.4 Hz for both records. The frequencies where these peaks are noticed correspond to the energy level of the wind speed which are higher than usual. Therefore, sudden gusts may be expected at these frequencies. Most of the energy of the wind speed is concentrated below 1.0 Hz. In general, both plots indicate that the energy level of the wind speed is high at low frequency. The energy of the wind speed above 1 Hz is negligible for both records. The power spectra of wind speed at the 34.7 m height level for records NO? and N16 are shown in Figures D.la and D.lb, respectively, in Appendix D. Next, the power spectra of conductor loads are considered. 151 P»« SPECTWI OF ND5.«05 (TIKET SreCTWL WWOHl

FREQUENCY (HERTZ)

Figure 5.3a Power Spectrum of Wind Speed at 34.7 m for Record NOS

poicR spEcnni* or NDa.»605

I I I' 0.001 O.Ol FREQUENCY (HERTZ)

Figure S.Sb Power Spectrum of Wind Speed at 34.7 m for Record NOS 152

The power spectrum plots for conductor load values may be considered in three possible ways. These three ways are (i) the power spectrum plots for total load values, (ii) the power spectrum plots for transverse load values, and (iii) the power spectrum plots for longitudi­ nal load values. Among these three ways, only the fre­ quency contents of the power spectrum plots for trans­ verse load values showed any detailed frequency distribu­ tions. Appendix D ( Figures D.2a through D.ISa) gives the power spectra plots of total, transverse, and longi­ tudinal load values from the conductors not shown in this section. The power spectra for transverse load values from the west and the east conductors for record NOS are shown in Figures 5.4a and 5.4b, respectively. Peaks in the power spectra are observed in both conductors near 0.22 and in the vicinity of 2.5 to 3.0 Hz. In addition. Figure 5.4a indicates peak in the power spectrum near 0.45 Hz. These peaks in the power spectra indicate that the energy of the conductor loads are significant at the frequencies which correspond to these peaks. The power spectra for transverse load values from the west and the east conductors for record NOS are shown in Figures S.Sa and S.Sb, respectively. Peaks in the power 153 8 P»CR SPETreiH OF KB-LC03 nWMSVERSE 01RECT1O1

o o CO

a

I UJ 8 a ai >•

liJ O-

IIIII m II n PI lip •XJI 0.001 0.01 0.1 1.0 FREQUENCY (HERTZ)

Figure 5.4a Power Spectrum of Transverse Load From West Conductor for Record NOS

pact spcEimji OF ros.LaN TMNSYEXSE OIKCTION 8 a o § o >^ (O 8 a a o I 8 o UJ d 8 >• in § 8 8 8 {3 a. 8 8 - ""^^^"^^^^^^^ I I'l fi T '0.001 0.01 0.1 1.0 FREQUENCY (HERTZ)

Figure 5.4b Power Spectrum of Transverse Load From East Conductor for Record NOS 154 8 PO»€R SPeCTWJH OF ND8.LCQ3 TRHHSVERSE DIRECTION

o

V.

I UJ 3 ^ a

H- U UJ a.

FREQUENCY (HERTZ)

Figure S.Sa Power Spectrum of Transverse Lead From West Conductor for Record NOS

POICR SPCETlMf OF MM-LON TRRNSVEKSE OliiECTiaN

0.001 FREQUENCY (HERTZ)

Figure S.Sb Power Spectrum of Transverse Load From East Conductor for Record NOS 155 spectra are observed in both conductors near 0.02, 0.11, and 0.22 Hz. Peaks in the power spectra are also noticed in the vicinity of 2.5 to 3.0 Hz for both conductors. A spike in the power spectra is noticed at 1.0 Hz for both conductors. Spike in the power spectra indicates a sudden surge in the frequency content of the conductor loads at a particular frequency. The power spectra for both conductors compare closely with each other. Also, most of the energy of the conductor loads is concentrated below 1.0 Hz. The power spectra for transverse load values from the center conductors for records NOS and NOS are shown in Figures 5.6a and 5.6b, respectively. In Figure 5.6a, peaks in the power spectrum are noticed at 0.25, 0.45, and in the vicinity of 2.5 to 3.0 Hz. In Figure 5.6b, peaks in the power spectrum are noticed at 2.5 to 3.0 Hz. In both plots, the power spectra indicate that most of the energy for both conductors is concentrated at fre­ quencies below 1.0 Hz. The power spectra plots for total loads from the east, west, and center conductors are presented in Appen­ dix D (Figures D.2 through D.14). In general, the power spectrum plots for total load from the east, west. and center conductor indicate spikes near 1.0, 2.0, 3.0, 4.0, 156 8 POlO SPECTRIH OF fOS-LOB TRfiHSVERSE OIRECnCN

a .70 0 (T) o o 1—o 4 CO 8 Ns o

RL U a >• M o ai o Hoe-: 8• U o UJ 0- 8

Figure 5.6a Power Spectrum of Transverse Load From Center Conductor for Record NOS

piftc? spamnjH OF M]a.Lros TKRNSVEJSE DIREQION

0.001 FREQUENCY (HERTZ)

Figure 5.6b Power Spectrum of Transverse Load From Center Conductor for Record NOS 157 and 5.0 Hz for records NOS, NO?, and NOS. In all cases, these spikes are indicated by vertical lines in the power spectrum plots. The energy level associated with these discrete peaks is negligible since the area bounded by these vertical lines is zero. These discrete peaks are inconsistent with the dynamic phenomenon of the con­ ductors because continuity of the power spectra shapes is not preserved. A peak in power is observed at 0.45 Hz for total load values from east, west, and center conduc­ tor of record NOS. Also, a peak in power is noticed at 0.25 Hz for total load values from center conductor for records NOS and NOS. The power spectra plots of longitudinal loads from the east, west, and center conductors are presented in Appendix D (Figures D.2 through D.IS). In the case of longitudinal loads from the conductors, peaks in power are observed near 0.2, 2.3, and 4.0 Hz for longitudinal load values from east, west, and center conductor of record N16. The power spectra of strain gages are now

considered. Proper understanding of the power spectrum of strain gages can be made more clear by studying Figure 4.5. Strain gages mounted symmetrically and diagonally oppo­ site to one another, and on the corresponding oppositely 158 configured structural member are expected to produce opposing effects (see Kempner, et al 1977). If one structural member is observed to undergo tension, the similar and oppositely configured structural member should be expected to undergo compression of about the samie magnitude when subjected to dynamic load. The maximum frequency of the power spectra of the strain gages is 10.0 Hz if the time interval between two observations is 0.05 second for the time series of the strain gaiges. However, it is necessary to obtain similar time interval when cross correlating two separate time series. Since the cross correlation relating wind speed with strain gaiges, and relating conductor loads with strain gages are required in computing for the frequency response functions, the time interval between two obser­ vations is taken to be 0.1 second for the time series of the strain gages. This time interval corresponds to the time interval between two observations in the time series of the wind speed and the conductor loads. Figures 5. 7a and 5.7b show the power spectra of the strain gaiges mounted on main leg member located at SE corner and on main leg member located at NW corner for record NOS, respectively. Both plots are similar. Most energy is accounted for at frequencies below 1.0 Hz. 159 PCKR SPECnnil OF N0a.SC05 aiAH SPECTKH. HIMXM)

0.001 FREQUENCY (HERTZ)

Figure 5. 7a Power Spectrum of Main Strain Gaige Located at SE Corner for Record NOS

8 p^a spQnnjM OF f08.scii OIKET SfEaKRL HlfCONI

•^ SI 'is o (O m

UJ N ai

^ o (^ o

a.

0.001 FREQUENCY (HERTZ)

Figure 5.7b Power Spectrum of Main Strain Gage Located at NW Corner for Record NOS 160

Spikes are noticed at 1.0, 2.0, 3.0, 4.0, and 5.0 Hz for both plots. These spikes are noticed in almost all the power spectrum plots for strain gaiges of records NOS and N08 and are likely to be associated with noise. Also, the power spectra indicate some energy near 2.5 Hz for both plots. Figures S.Sa and S.Sb present the power spectra of the strain gages mounted on main leg members located at the SE corner and NW corner for record NOS, respectively. Both plots are similar. Most power is accounted for at frequencies below 1.0 Hz. Spikes noticed at 1.0, 2.0, 3.0, 4.0, and 5.0 Hz in both plots again are likely to be associated with noise and are insignificant. Peaks in energy are noticed at 0.45 and 2.5 Hz for both plots. Several observations are made based on power spectra analyses. Unless specified, the general observations made are for the selected records. These observations are: 1. The power spectra of the wind speed have high energy content at low frequency, that is, at fre­ quencies below 1.0 Hz. The energy beyond 1.0 Hz is negligible. 2. The power spectra of the total loads exhibit peak in energy at 0.45 Hz for record NOS. 161 3 fWCR SPECTWJM OF KK.SGOS (7l*ET SfECTIM. HIM}a4l

C3 „ S i

i 8

UJ ai 8 IM

c_> :: 'it ° CO

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Figure S.Sa Power Spectrum of Main Strain Gage Located at SE Corner for Record NOS

8 PO>CR SPCCTIilM OF M)S.SC11 i» (TIKET SPECTRflL HIWCHI a

o § . O (J ^^ SO O (D a m o u_ 8 i 3 o UJ 3 o

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Figure S.Sb Power Spectrum of Main Strain Gage Located at NW Corner for Record NOS 162

3. The power spectra of the transverse loads from the west conductor display noticeable energy at 0.22 and at 2.8 Hz. Record NOS displays additional energy at 0.45 Hz. High energy is observed at fre­ quencies below 1.0 Hz.

4. The power spectra of the transverse loads from east conductor display noticeable energy at 0.22 and at 2.8 Hz, except for record N16. High energy is observed at frequencies below 1.0 Hz. 5. The power spectra of the transverse loads from the center conductor display noticeable energy at 2.5 Hz. Record NOS displa^^s additional peaks in energy at 0.22 and at 0.45 Hz. 6. The power spectra of the longitudinal loads from the west conductor displaiy noticeable energy at 0.2, 2.3, and 4.0 Hz for record N16. 7. The power spectra of the longitudinal loads from the east conductor display noticeable energy at 0. 2, 2. 3, and 3.0 Hz. 8. The power spectra of the SE main strain gage 2 (SGOS) display noticeable energy at 2.3 Hz. Record NOS displays additonal peak in energy at 0.45 Hz. 163

9. The power spectra of the SE diagonal strain gage 3 (SG06) display noticeable energy at 0.2 and at 3.7 Hz. Record NOS displays noticeable energy at 0.45 Hz.

10. The power spectra of the NW main strain gage 2 (SGll) display noticeable energy at 2.3 Hz. Record NOS displays noticeable energy at 0.45 Hz. 11. The power spectra of the NW diagonal strain gage 3 (SG12) display noticeable energy at 3.7 Hz. Record NOS displays noticeable energy at 0.45 Hz. Record NIS displao^s noticeable energy at 0.2 Hz. The observations made in 1 through 11 are discussed in section 5.7. The following section discusses the fre­ quency response function of the transmission tower.

5.6.2 Frequency Response Function of Transmission Tower In this section, the frequency response function of the transmission tower structural system is investigated. The dynamic behavior of the transmission tower is de­ scribed in terms of the frequency response function. The frequency response function of a particular structural member of the transmission tower is unique for a particu­ lar load and response. For example, the load may be any 164 wind speed from the west, and the response may be the stresses experienced by a particular structural member. The frequency response function of the transmission tower mao^ be investigated and classified into two phases. These two phases are (1) the frequency response functions due to wind speed as the load and stresses experienced by structural member as the response, and (2) the frequency response functions due to conductor loads as the load and stresses experienced by structural member as the response. Again, it needs to be emphasized that final conclusions pertaining to the frequency response function cannot be made without observing the coherence function of the transmission tower. First, the frequency response function of the trans­ mission tower relating wind speed and stresses expe­ rienced by a structural member is considered. The study of the frequency response function enables the analyst to identify whether the effect of the wind speed acting on the tower directly is significant in explaining the responses of the transmission tower. Figures 5.9a and 5.9b present the effect of east wind speed on the diagonal leg members located at SE corner and NW corner for record NOS, respectively. Both plots 165 GfllN FUNCTION CF NOS.HSOS an HMO N0S,SG06

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5 2

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Figure 5.9a Frequency Response Function Relating Wind Speed and SE Diagonal Leg Strain Record for Record NOS

SflDt FUCTION OF NOS.HSOS 81 RnO N05.SC12

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Figure 5.9b Frequency Response Function Relating Wind Speed and NW Diagonal Leg Strain Record for Record NOS 166 are similar. Spikes are noticed at 1.0, 2.0, 3.0, 4.0, and 5.0 Hz for both plots. Comparisons of the effect of east and west wind speed on a main leg structural member located at SE corner for records NOS and NOS are shown, respectively, in Figures 5.10a and 5. 10b. The frequency response is intensified in the range of 2.0 to 3.0 Hz. If the frequency response function is increasing at certain frequencies, the response of the structural member is expected to be significant at that frequencies which correspond to the increase in the frequency response. Similar observation holds true for any plots of the frequency response func­ tion. In addition, the east wind effect causes a peak at 0.45 Hz as seen in Figure 5.10a. Figures 5.11a and 5.lib present the frequency re­ sponse function relating west wind speed to the strains in the diaigonal leg members located at NW corner and at SE corner for record NOS, respectively. Both plots are similar. In Figures 6.9a, 6.9b, 6.11a, and 6.11b, no peak frequency response is observed at low frequencies, that is at frequencies lower than 1.0 Hz. In general, the frequency response with wind ^3peed as input and strain gages as output shows spikes at fre­ quencies near 1.0, 2.0, 3.0, 4.0, and 5.0 Hz for the SniN FUCTIOM CF NOS.HSOS 167 RTO KD5.SG05

(O * (O

m u_

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Figure 5.10a Frequency Response Function Relating Wind Speed and SE Main Leg Strain Record for Record NOS

GAIN FUfCnCM OF roaL>£os 8 RNO »£8.SCC6 o

-9 -^"' est 8

u- 8 I a

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Figure S.lOb Frequency Response Function Relating* -Ur.a Speed and SE Main Leg Strain Record for Record N06 168 GAIN F=UMn'I(M OF rO8.>£05 an mo W8.SC06

CM (O o -1 9 (D

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Figure 5.11a Frequency Response Function Relating Wind Speed and SE Diagonal Leg Strain Record for Record NOS

GRIN FUCnON OF Mn.»6G6 ai (H) M)8.X12

en si

»— o H c_) f*

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I I I I I 111| ^^ ^ f>m 0.001 0.01 0.1 1.0 FREQUENCY (HERTZ)

Figure 5. lib Frequency Response Function Relating Wind Speed and NW Diagonal Leg Strain Record for Record NOS 169 selected records. These spikes were noticed even from the power spectra plots of the strain gaiges. These spikes are attributed to noise in the data recording system. In addition, a peak in frequency response is observed at 2.5 Hz for both records NOS and NOS. Also, a peak frequency response is observed at 0.45 Hz for record NOS only. Figures E.la through E.Sb in Appendix E give additional plots of the frequency response functions with wind speed as load and strain gaiges as response not presented in this section.

Next, the frequency response functions relating con­ ductor loads and stresses experienced by a structural member as the response is considered. Study of these frequency response functions enables the analyst to identify whether the conductor loads acting dynamically on the tower are significant in explaining the responses of the transmission tower. The dynamic loads from the conductors acting on the tower can be resolved into (1) total load, (2) transverse load, and (3) longitudinal load. Figures 5.12a and 5.12b show the frequency response functions relating total load from the east conductor and stresses on main leg members located at SE and NW eor- ners, respectively, for record NOS. Both plots are 170 8 GRIN RJNCnON OF M}5.UnN (TOrRLI RM) NOS.SGOS

0.001 FREQUENCY (HERTZ) Figure 5.12a Frequency Response Function Relating Total Load From East Conductor and SE Main Leg Strain Record for Record NOS

GRIN FUNCnm OF MS-LON (TomLi AM) NOS. sen

0.001 FREQUENCY (HERTZ)

Figure 5.12b Frequency Response Function Relating Total Load From East Conductor and NW Main Leg Strain Record for Record NOS 171 similar. Several peaks in frequency response are noticed for frequencies in the range between 0.01 and 0.1 Hz. Other peaks in frequency response are noticed at 0.4 and 2.5 Hz. The frequency response is relatively stronger at lower frequencies than at higher frequencies for both cases. The frequency response functions relating total load from the east conductor and stresses on diagonal leg members located at SE and NW corners are shown in Figures 5. 13a and 5. 13b, respectively. Several peadcs are noticed in the frequency range of 0.01 to 0.2 Hz. Figures 5.14a and 5.14b show the frequency response functions relating total load from the center conductor and stresses on main leg members located at SE and NW corners, respectively, for record NOS. Both plots are similar. Also, both of these plots are similar to the frequency response functions shown in Figures 5.12a and 5.12b. The frequency response is relatively stronger at frequencies below 1.0 Hz than at frequencies above 1.0 Hz. Peak in frequency response is also noticed at 2.5 Hz for both plots. Figures 5.15a and 5.ISb present the frequency re­ sponse functions relating total load from the west con­ ductor and stresses on main leg members located at SE and 172 8 GRIN FUNCTION OF NDS.irW 1T0TTU.J flW NOS. SGOS

0.1.. 1.0 10.0 FREQUENCY (HERTZ)

Figure 5.13a Frequency Response Function Relating Total Load From East Conductor and SE Diagonal Leg Strain Record for Record NOS

8 GRIN FUNcncN OF ros.LaN (TOTRLI RM) N06.SG12

I I I I I I I) '0.001 0.01 FREQUENCY (HERTZ)

Figure 5.13b Frequency Response Function Relating Total Load From East Conductor and NW Diagonal Leg Strain Record for Record NOS 173 8 GRIN FWCnol OF ICS.LCIB (TTmV.1 no N0S.SG05

0.001 FREQUENCY (HERTZ)

Figure 5. 14a Frequency Response Function Relating Total Load From Center Conductor and SE Main Leg Strain Record for Record NOS

GRIN FUMinCN OF t€JS.LnS (TOTRLI R»0 N05.SCI1

0.001 FREQUENCY (HERTZ)

Figure 5.14b Frequency Response Function Relating Total Load From Center Conductor and NW Main Leg Strain Record for Record NOS

1- - 174 GRIN FUNcnm OF rf}a.Lca3 (TOTRLJ FNO rCB.SCOS

0.001 0.1- 1.0 FREQUENCY (HERTZ)

Figure 5.ISa Frequency Response Function Relating Total Load From West Conductor and SE Main Leg Strain Record for Record NOS

GRIN Rjrcnm OF w)a.LnB 8 nOTFL] RNO N08.SC11

CM

m .00 0 v^ rt

CJ

§ I I I I I II n 10.0 '0.001 . 0.01 FREQUENCY (HERTZ)

Figure 5.15b Frequency Response Function Relating Total Load From West Conductor and NW Main Leg Strain Record for Record NOS 175

NW corners, respectively, for record NOS. Both plots are similar in comparison. Peaiks in frequency response are noticed in the frequency range of 0.01 to 0.2 Hz. Additional peak in frequency response is noticed at 2.5 Hz. The frequency response values are higher at low frequency than at high frequency for both plots.

The frequency response functions relating total load from the east conductor and stresses on main leg members located at SE and NW corners are shown in Figures 5. 16a and 5.16b, respectively. Both plots are similar. The frequency response are stronger at lower frequencies than at higher frequencies. Additional peak is noticed at 2.5 Hz for both plots. In general, the frequency response functions relating the total load from the east, west, and center conductors and stresses on main and diagonal leg members indicate a peak at 2.5 Hz. In addition, the frequency responses are relatively stronger at lower frequencies than at higher frequencies. Additional plots of the frequency response functions relating the total load from the conductors and stresses on main and diagonal leg members are given in Figures E.4a through E.10b in Appendix E. The effect of the transverse conductor loads on the stresses of a main or a diagonal leg member structural 176 8 GRIN FUM:T1« OF ND8.Lrw •« (Torn. J (W ND8.SGCS

• M^ CM cXn

0.001 FREQUENCY (HERTZ)

Figure 5.16a Frequency Response Function Relating Total Load From East Conductor and SE Main Leg Strain Record for Record NOS

8 GRIN FlMrnON OF NDa.LX:0M aorn.) fHO W8.scii

CM

10.0 FREQUENCY (HERTZ)

Figure 5.16b Frequency Response Function Relating Total Load From East Conductor and NW Main Leg Strain Record for Record NOS 177 member is now considered. In most of these plots, spikes in frequency response are observed at 1.0, 2.0, 3.0, 4.0, and 5.0 Hz. As discussed earlier, these frequencies are attributed to noise present in the data accumulation system. Figures 5. 17a and 5. 17b present the frequency re­ sponse functions relating the transverse load from the west conductor and stresses on main leg members located at SE and NW corners, respectively, for record NOS. A spike in frequency response is observed at 1. 0 Hz for both plots. The frequency response is similar. The fr«=i- quency response is relatively stronger at lower fre­ quencies than at higher frequencies for both plots. Figures 5.ISa and 5.ISb present the frequency re­ sponse functions relating transverse load from the east conductor and stresses on diagonal leg members located at SE and NW corners, respectively for record NOS. Both plots are similar. In addition, the frequency response tends to be more pronounced as frequency approches 1. 0 Hz. The frequency response for both plots are relatively stronger at lower frequencies than at higher frequencies. Figures 5.19a and 5.19b present the frequency re­ sponse functions relating transverse load from the center conductor and stresses on main leg members located at SE 178 GRIN FUfCnW OF «S.LDa 81 (TRFNS.) PHD N0S.SC06

CM cn

o -

0.001 0.01 0.1 1.0 10.0 FREQUENCY (HERTZ)

Figure 5.17a Frequency Response Function Relating Transverse Load From West Conductor and SE Main Leg Strain Record for Record NOS

GRIN FUCnON OF WS.LJCa3 81 ITRfttS.} RNO NOS.SGll

CM cn m cn a>^ M U- I o - o ot— u.

10.0 FREQUENCY (HERTZ)

Figure 5.17b Frequency Response Function Relating Transverse Load From West Conductor and NW Main Leg Strain Record for Record NOS 179 GRIN FUNCnCN BF NOS.LCm (TRms.) RNO N0S.SC06

FREQUENCY (HERTZ)

Figure 5.ISa Frequency Response Function Relating Transverse Load From East Conductor and SE Diagonal Leg Strain Record for Record NOS

GRIN FUCnCN OF N05.LaM ITRRIS.) RNO N05.SC12

CM cn cn . -

CD m u. I oz CJ

0.001 FREQUENCY (HERTZ)

Figure 5.ISb Frequency Response Function Relating Transverse Load From East Conductor and NW Diagonal Leg Strain Record for Record NOS 180

8 GRIN FlMrnON OF «S,LaB (TTtmS.) RNO N0S.SC06

FREQUENCY (HERTZ)

Figure 5.19a Frequency Response Function Relating Transverse Load From Center Conductor and SE Main Leg Strain Record for Record NOS

GRIN FUMTHON OF M)5.La5 (TRmS.I RNO ^CS.SCI1

10.0 FREQUENCY (HERTZ)

Figure 5.19b Frequency Response Function Relatir.is Transverse Load From Center Conductor and NW Diagonal Leg Strain Record for Record NOS 181 and NW corners, respectively, for record NOS. Both plots show similar shape for all frequencies above 0.01 Hz. The frequency response for both plots are relatively stronger at lower frequencies than at higher frequencies.

In the case of record NOS, Figures 5.20a and 5.20b present the frequency response functions relating trans­ verse load from the west conductor and stresses on main leg members located at SE and NW corners, respectively. Both plots are similar. High frequency response is ob­ served at low frequencies for both cases. Concentration of frequency response is observed to occur near 1.0 Hz for both plots. Figures 6.21a and 6.21b present the frequency re­ sponse functions relating transverse load from the west conductor and stresses on diagonal leg members located at SE and NW corners, respectively, for record NOS. Both plots are also similar. Figures 5.22a and 5.22b present the frequency re­ sponse functions relating transverse load from the east conductor and stresses on main leg members located at SE and NW corners for record NOS, respectively. Both plots are similar. The frequency response functions are high at frequency below 1.0 Hz. Additional plots of the frequency response functions relating transverse load 182 GRIN Furcnw OF fcaicoa (TRRNS.) RM) NOB.SGOS

0.1 1.0 FREQUENCY (HERTZ)

Figure 5.20a Frequency Response Function Relating Transverse Load From West Conductor and SE Main Leg Strain Record for Record NOS

8 GRIN FUNCntM OF lOLLCQa (TRRNS.) RM) NOS.SCI 1

0.001 FREQUENCY (HERTZ)

Figure 5.20b Frequency Response Function Relating Transverse Load From West Conductor and NW Main Leg Strain Record for Record NOS 183 GRIN FUfCnON OF NDOLLOB (TRRNS.) RU) NOe.SGQS 81

CM cn m

m

CJ

FREQUENCY (HERTZ)

Figure 5.21a Frequency Response Function Relating Transverse Load From West Conductor and SE Diagonal Leg Strain Record for Record NOS

GRIN FUNCnCN tF NOS.LOB (TRRNS.) RM) N08.SC12

CM

0.1 • 1-0 FREQUENCY (HERTZ)

rf Figure 5.21b Frequency Response Function Relatin Transverse Load From West Conductor and NW Diagonal Leg Strain Record for Record NOS 184 GRIN FUCnON OF «a.LaB aRRNS.) RM) NOe.SGOS

cCMn M cn

O m u. I CJ

FREQUENCY (HERTZ)

Figure 5.22a Frequency Response Function Relating Transverse Load From East Conductor and SE Main Leg Strain Record for Record NOS

GRIN FWCnCM OF N08.L£aa (TRRNS.) RM) N08.SC12

0.001 0.1 1.0 FREQUENCY (HERTZ)

Figure 5.22b Frequency Response Function Relating Transverse Load From East Conductor and NW Main Leg Strain Record for Record NOS 185 from the conductors and stresses on main or diagonal leg members are shown in Appendix E (Figures E. 11a through E.17b). The effect of longitudinal conductor loads on the stresses experienced by structural members is considered here. In general, most of the frequency response func­ tions relating transverse load from the conductors and stresses on main or diaigonal leg members indicate dis­ crete peaks at 1.0, 2.0, 3.0, 4.0, and 5.0 Hz. These peaks are attributed to the presence of noise in the data accumulation system. This noise is likely to be from the data accumulation system of the response. Figures 5. 23a and 5.23b present the frequency re­ sponse function relating longitudinal load from west con­ ductor and stresses on main leg members located at SE and NW corners, respectively, for record NOS. Higher fre­ quency response is observed at lower frequencies than at higher frequencies. In addition, Figure 5.23a indicates a peak at 0.4SHz. Figures 5.24a and 5.24b present the frequency re­ sponse functions relating longitudinal load from the east and center conductors and stresses on main leg members located at NW corner,respectively, for record NOS. Both plots are similar. Higher frequency response is observed 186 GRIN FUCnOI OF NOS.LDB (U>C1 RM) NOS.SGOS

FREQUENCY (HERTZ)

Figure 5.23a Frequency Response Function Relating Transverse Load From West Conductor and SE Main Leg Strain Record for Record NOS

GRIN FUCntM OF N05.LI3S 81 (LOMk) RM) NOS.SGH

CD M U. zI o - o

I—I

CJ

0.001 1.0 10.3 FREQUENCY (HERTZ)

Figure 5.23b Frequency Response Function Relating Transverse Load From West Conductor and NW Main Leg Strain Record for Record NOS 187 8 GRIN FWCnCN OF N0S.LCOI (LONG.) RM) NOS.SGH

CM cn m

CD m u. 1

CJ

U-

0.001 10.0 FREQUENCY (HERH)

Figure 5.24a Frequency Response Function Relating Longitudinal Load From East Conductor and NW Main Leg Strain Record for Record NOS

GRIN RJMrnON OF NOS.LCaS ILONO.) RM) NOS.sell

10.0 FREQUENCY (HERTZ)

Figure 5.24b Frequency Response Function Relating Longitudinal Load From Center Conductor and NW Main Leg Strain Record for Record NOS 188 in both plots at lower frequencies than at higher fre­ quencies. Figures 5.2Sa and 5.25 present the frequency response functions relating longitudinal load from the west con­ ductor and stresses on main leg members located at SE and NW corners, respectively, for record NOS. Both plots are similar. The frequency response is higher at frequencies below 1.0 Hz for both plots than at frequencies above 1.0 Hz. Figures 5.26a and 5.26b present the frequency re­ sponse functions relating longitudinal load from the east and center conductors and stresses on the main leg member located at SE corner, respectively, for record NOS. Both plots are similar. High frequency response is obtained at lower frequencies for both plots. Frequencies in the range of 0.1 to 1.0 Hz also has high frequency response. In general, comparison between east and west wind records indicates no similarity in the frequency response for similar load and response. Additional plots of the fre­ quency response functions relating longitudinal loads from the conductors and stresses on main or diagonal leg members are given in Figures E.ISa through E.23b not presented in this section. 189 GRIN FlffCnCN OF WSLina (LOIC.) (HO M}8.SC0S

O.QOl FREQUENCY (HERTZ)

Figure 5.2Sa Frequency Response Function Relating Transverse Load From West Conductor and SE Main Leg Strain Record for Record NOS

GRIN ntcum OF M)a.LaQ n "" a.O«C.) RM) f08.SCll

a —^ CM cn m 8 IS I \ Mo CD m u_

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0.001 10.0 FREQUENCY (HERTZ)

Figure 5.25b Frequency Response F'-.:nc"^ I'T; ^P"'-^i"^ ^ n'l Transverse Load From West Conductor and NW Main Leg Strain Record for Record NOS 190 8 GRIN FUNCnON OF rca.LOM (L04G.) RNO M)8.SC0S

CM cn 8 ^•m^ •1 5 O U- 8 z - tairf 5 o 8 0.001 10.0 FREQUENCY (HERTZ)

Figure 5.26a Frequency Response Function Relating Transverse Load From East Conductor and SE Main Leg Strain Record for Record NOS

GRIN RJMrnON OF M)8.LOB a.aNC) RNO M)8.SC0S

'0.001 FREQUENCY (HERTZ)

Figure 5.26b Frequency Response Function Relating Transverse Load From Center Conductor ina SE Main Leg Strain Record for Record NOS 191

In the following section, the coherence function relating the loads and the responses is obtained. Since the results obtained in this section are dependent on the results obtained in the following section, further dis­ cussion of this section is made in the following section.

5.6.3 Coherence Function of Transmission Tower In this section, the coherence function relating the loads and the responses is considered. The coherence function can be used to measure if the transmission tower structural system relating the load and response is linear. Also, the coherence function can be used to detect the presence of noise in the measurements. Figures 5.27a and 5.2?b present the coherence func­ tions for record NOS relating wind speed at 34.7 m height and stresses on diaigonal leg members located at SE and NW corners, respectively. The values of the coherence func­ tions are small for frequency below 1.0 Hz in both plots. Since the power spectra of wind speed have high energy for frequency below 1.0 Hz, and the frequency response functions shown in Figures 5.9a and 5.9b indicate no peak frequency response at low frequency, it is expected that wind speeds do not affect the diagonal leg members. In both plots, the coherence function flutters. 192 8 (SeSNCE FUNCTION CF WS.MS05 RNO »OS.SC06

a o ^^ oa t— CJ a 9 u. o UJ a 8 UyJ a Q^ a ^ o 8 u o a a a ^ a a 8 1.0 FREQUENCY (HERTZ)

Figure 5.27a Coherence Function Relating Wind Speed and SE Diagonal Leg Strain Record for Record NOS

(3CRENCE FUNCTION OF NOS.HSOS FNO N05.SC12

FREQUENCY (HERTZ)

Figure 5.27b Coherence Function Relating Wind Speed and NW Diagonal Leg Strain Record for Record NOS 193

Since the power spectra of wind speed have high energy for frequency below 1.0 Hz, and the frequency response functions shown in Figures 5.9a and 5.9b indicate no peak frequency response at low frequency, it is expected that wind speeds do not affect the diaigonal leg members. In both plots, the coherence function flutters.

The coherence functions for records NOS and NOS relating wind speed and stresses on the main leg member located at SE corner are shown in Figures 5.2Sa and S.2Sb, respectively. The coherence functions are higher at most frequencies for both of these plots in comparison to the coherence functions shown in Figures 5.27a and 5.27b. In particular, the coherence functions are large at frequencies below 0.1 Hz. This indicates that wind speed is relatively more significant on the main leg members than on the diagonal leg members. In general, the coherence functions relating wind speed and stresses on main leg members at frequency below 0.1 Hz are high. Also, the coherence functions relating wind speed and stresses on main leg members are rela­ tively higher at frequencies below 0.1 Hz than those relating wind speed and stresses on diagonal leg members. In all the selected records, the values of the coherence functions are relatively small at frequencies between 0.1 194 CaCRBCE FUNCTION r N05.HS0S no M)S.SC06

0.001 10.0 FREQUENCY (HERTZ)

Figure S.2Sa Coherence Function Relating Wind Speed and SE Main Leg Strain Record for Record NOS

(»CRENCE FUNCTION OF N0B.HS05 RNO M08.SC05

0.001 10.0 FREQUENCY (HERTZ)

Figure 5.28b Coherence Function Relating Wind Speed and SE Main Leg Strain Record for Record NOS 195 and 1.0 Hz. The frequency response functions relating wind speed and stresses on leg members, and the power spectra of the member leg strains indicated spikes at 1.0, 2.0, 3.0, 4.0, and 5.0 Hz. However, these spikes are not noticed in the coherence functions relating wind speed and stresses on leg members. This indicates that wind speed is not contributing to the responses of the leg members at 1.0, 2.0, 3.0, 4.0, and 5.0 Hz. Instead, this suggests the presence of noise in the data accumula­ tion system of the responses at these frequencies. Additional plots of coherence functions relating wind speed and stresses on main or diaigonal leg members which are not presented in this section are presented in Figures F.la through F.Sb in Appendix F. Next, the coherence functions relating conductor loads and stresses on main or diaigonal leg members as output are considered. Figures 5.29a and 5.29b present the coherence func­ tions relating total load from the west conductor and stresses on main and diagonal leg members located at SE corner, respectively, for record NOS. Less fluttering is noticed near 0.2 Hz. Spikes in coherence are noticed at 1.0, 2.0, 3.0, 4.0, and 5.0 Hz. These spikes are also noticed in the power spectra of the total load from the west conductor, and in the power spectra of the SE main 196 8 CWERENCE FUCTIW OF o N0B.LC03 RNO M)8.SC06

0.001 FREQUENCY (HERTZ)

Figure 5.29a Coherence Function Relating Total Load From West Conductor and SE Main Leg Strain Record for Record NOS

CattERBKE FUNCTION OF NOB.UZia RNO IO8.SG06

o CJ

o CJ

FREQUENCY (HERTZ)

Figure 5.29b Coherence Function Relating Total Lo.^a From West Conductor and SE Diagonal Leg Strain Record for Record NOS 197 and diagonal leg strains. However, these spikes are not noticed in the frequency response functions relating total load from west conductor and stresses on main and diagonal leg members located at SE corner. This suggests the presence of noise in the data accumulation system.

Figures 5.30a and 5.30b present the coherence func­ tions relating total load from the east conductor and stresses on main leg members located at SE and NW corners as output, respectively, for record NOS. Both plots are similar. The values of the coherence functions are high at frequencies below 0.3 Hz for both plots. Figures F.4a through F.7b in Appendix F present the coherence func­ tions tions with total load from conductors as load and stresses on main or diaigonal leg members as response not discussed in this section. Figures 5. 31a and 5.31b present the coherence func­ tions relating transverse loads from the west conductor and stresses on main and diagonal leg members located at SE corner, respectively, for record NOS. Relatively, the values of the coherence functions relating transverse conductor loads to main leg stresses are higher than those relating transverse conductor loads to diagonal leg stresses. In both plots, a high peak in coherence i^3 observed near 0.45 Hz. In addition, Figure 5.31a shows a 198 3 CaeSNCE FUNCTION OF o N0B.L(2)>1 RNO M)8.SC0S

FREQUENCY (HERTZ)

Figure 5.30a Coherence Function Relating Total Load From East Conductor and SE Main Leg Strain Record for Record NOS

COCREMZ FUNCTION OF NOB.LCm RNO U}8.Xn m* O 9 _ d • o a _ 2 ti "

o g• ^ t—^^ a CJ a

U5- a in _ UJ d ^ . UJ (ki. n ^ 8. - o T U a_ . »> .

av« ri • d °0. 001 0.01 FREQUENCY (HERTZ)

Figure S.SOb Coherence Function Relating Total Load From East Conductor and NW Main Leg Strain Record for Record NOS 199 8 COCRENCE RJCTION OF a mS.L(213 FNO M0S.SC06

O »— o

'±UJ UJ o u

0.001 FREQUENCY (HERTZ)

Figure 5.31a Coherence Function Relating Transverse Load From West Conductor and SE Main Leg Strain Record for Record NOS

CSOeCE FUCTION OF Na5.L(2}3 PNO >IIS.SG06

0.1 1.0 10.0 FREQUENCY (HERTZ) Figure 5.31b Coherence Function Relating Transverse Load From West Conductor and SE Diagonal Leg Strain Record for Record NOS 200 high peak in the coherence function near 2.5 Hz. In both plots, the coherence functions flutter and the values are small at low frequencies. Figures 5.32a and 5.32b present the coherence func­ tions relating transverse loauis from the west conductor and stresses on main end diagonal leg members located at NW corner, respectively, for record NOS. The coherence functions flutter. The peadc value in coherence function is observed to occur near 0.45 Hz in both cases. In addition. Figure 5. 32a displao^s a peadc near 2.5 Hz. Figures 5.33a and 5.33b present the coherence func­ tions relating transverse loads from the west conductor and stresses on main and diagonal leg members located at SE corner, respectively, for record N08. Relatively, the coherence function relating transverse load from the west conductor and SE main leg member is higher over a wider range of frequencies than the coherence function relating similar loads with stresses in the SE diaigonal member. The peak value in coherence is observed in Figure 5.33a near 2.5 Hz. Additional peak in coherence is observed near 0.2 Hz for both plots. These peaks observed at 2.5 and 0.2 Hz are also noticed in the frequency response functions relating transverse load from west conductor and stresses on main and diagonal leg member located at 201 8 CCHERENCE FUCTIOM CF a N05.L(2J3 flNO M05.SCI1

O o u. UJ C_)

UJ UJ 3: uo

10.0 FREQUENCY (HERTZ)

Figure 5.32a Coherence Function Relating Transverse Load From West Conductor and NW Main Leg Strain Record for Record NOS

COCReCE FUCTIOM OF ME.LCSa RNO M05.SC12

o O

UJ

UJ

uo

FREQUENCY (HERTZ)

Figure 5.32b Coherence Function Relating Transverse Load From West Conductor and NW Diagonal Leg Strain Record for Record NOS 202 COIBtSCE FUNCTION OP NOB.LC03 RNO U08.SC06.

'0.001 10.0 FREQUENCY (HERTZ)

Figure 5.33a Coherence Function Relating Transverse Load From West Conductor and SE Main Leg Strain Record for Record NOS

CmB»CE FUNCTION OF § NOB.LCOa RNO M)8.SC06,

o

CzJ liJ

o o

'0.001 FREQUENCY (HERTZ)

Figure 5.33b Coherence Function Relating Transverse Load From West Conductor and SE Diagonal Leg Strain Record for Record NOS 203

SE corner. Therefore, transverse load from west con­ ductor is contributing to the response of the leg mem­ bers. Figures 5.34a and 5.34b present the coherence func­ tions relating transverse loads from the west conductor and stresses in the main and diaigonal leg members located at NW corner, respectively, for record NOS. Relatively, values of coherence function with transverse load from west conductor acting as input on NW main leg member are higher over a wider range of frequencies than the coher­ ence function with similar input acting on NW diaigonal leg member. Figure 5.34a indicates a peak in the coher­ ence function near 2.5 Hz. Figures 5.SSa and S.SSb present the coherence func­ tions relating transverse loads from the east conductor and stresses on main and diagonal leg members located at the SE corner, respectively for record NOS. Values of the coherence function relating transverse load from the east conductor to main leg member stresses is relatively higher than the values of the coherence function relating transverse load from the east conductor to diagonal leg member stresses. A peak value in the coherence function 204 8 COCKOCZ FUNCTION OP a N0B.LC03 RNO lt08.SCn

3 a cJ o

O to

a d a 9 8 uo d 8 d a d 3. 0.001 d, 10.0 FREQUENCY (HERTZ)

Figure 5.34a Coherence Function Relating Transverse Load From West Conductor and NW Main Leg Strain Record for Record N08

COfiteCE FUNCTION CF NaB.L(2)3 FMO M08.SC12

a.Q FREQUENCY (HERTZ)

Figure 5.34b Coherence Function Relating Transverse Load From West Conductor and NW Diagonal Leg Strain Record for Record NOS 205 CtWERENCE FUNCTION CP Na8.L(ZM RNO U)8.SC0S

0.001 FREQUENCY (HERTZ)

Figure 5.SSa Coherence Function Relating Transverse Load From East Conductor and SE Main Leg Strain Record for Record NOS

CatFBKE FUNCTION OF NOB.LCOM RNO M)8.SG06

0.001 0.1 •• 1.0 FREQUENCY (HERTZ)

Figure 5.SSb Coherence Function Relating Transverse Load From East Conductor and SE Diagonal Leg Strain Record for Record NOS 206 is observed near 0.25 Hz for both plots. Figure 5.SSa indicates a peak value in the coherence function near 2.5 Hz. In general, the high coherence relating transverse load from the conductors and stresses in main leg members peak near 0.2 and 2.5 Hz is noticed. Figures F.Sa through F.9b in Appendix F present the coherence func­ tions relating transverse load from the conductors and stresses in main or diagonal leg members not presented in this section. Finally the effect of longitudinal load from the conductors on the leg members are discussed. Figures 5.SSa and 5.36b present the coherence func­ tions relating longitudinal load from west conductor and stresses in main and diaigonal leg members located at SE corner, respectively, for record NOS. Peak values in coherence are noticed near 0.2, 0.45, and 2.5 Hz. In the case of west wind record NOS, Figures 5.37a and 5.37b present the coherence functions relating longi­ tudinal load from the east conductor and stresses on the main and diagonal leg members located at SE corner, respectively, for record NOS. The values of the coher­ ence functions are generally lower relating longitudinal conductor loads than relating transverse conductor loads and the stresses in structural members. 207 CaOBCE FUCTION OF NOS.LCSS RW> U05.SC06

o I—• •— CJ u. UJ CJ z UJ ^ 8. uo

0.001 0.01 0.1 1.0 10.0 FREQUENCY (HERTZ)

Figure 5.36a Coherence Function Relating Longitudinal Load From West Conductor and SE Main Leg Strain Record for Record NOS

COOBCE FUNCTION OF NOB.USa RM) M)S.SC06

0.001 0.1 1.0 FREQUENCY (HERTZ)

Figure 5.36b Coherence Function Relating Longitudinal Load From West Conductor and SE Diagonal Leg Strain Record for Record NOS 208 COHERENCE FUNCTION OF N0B.L(a4 RNO M08.SG06

0.001 1.0 10.0 FREQUENCY (HERTZ)

Figure 5.37a Coherence Function Relating Longitudinal Load From East Conductor and SE Main Leg Strain Record for Record NOS

cwaeotcz FUNCTION tr ma.Lznn RNO UO8.SCO6

0.001 0.1 1.0 FREQUENCY (HERTZ)

Figure 5.37b Coherence Function Relating Longitudinal Load From East Conductor and SE Diagonal Leg Strain Record for Record NOS 209

Figures S.3Sa and S.3Sb present the coherence func­ tions relating longitudinal loads from the east conductor and stresses on main and diagonal leg members located at NW corner, respectively, for record NOS. A peak in coher­ ence function is observed for both plots near 2.5 Hz. Additional plots of the coherence functions relating longitudinal loads from the conductors and stresses on main or diaigonal leg members are given in Appendix F (Figures F.10a through F.12b). The observations made from the frequency response function and coherence function analyses are now dis­ cussed. Unless specified otherwise, the observations made in subsequent paragraphs are valid for all the selected records. The frequency response functions and the coherence functions relating wind speed and member leg strain are now considered. The frequency response functions and coherence functions peadc near 2.8 Hz when main leg member stresses are considered as the response. Also, the frequency response functions peak near 3.1 Hz when diagonal strain gaiges are considered as the res­ ponse. The frequency response functions relating conductor loads and strain gages are considered and discussed in three phases. First, coherence functions relating total 10 CWaENCE FUCTION OF 8 NOB.LCOil RNO M)8.SCn o

FREQUENCY (HERTZ)

Figure 5.SSa Coherence Function Relating Longitudinal Load From East Conductor and NW Main Leg Strain Record for Record NOS

COdBCC fUCTION OP NOB.LOyi RNO )J0e.SG12,

0.001 1.0 10.0 FREQUENCY (HERTZ)

Figure 5.SSb Coherence Function Relating Longitudinal Load From East Conductor and NW Diagonal Leg Strain Record for Record NOS 211 conductor loads and leg member strains are considered. Second, coherence functions relating transverse conductor loads leg member stresses are considered. Finally, cohe­ rence functions relating longitudinal conductor load and leg member stresses are considered. In the case of the coherence functions relating total conductor loads and strain gages, the frequency response functions and the coherence functions peak sharply at a frequency near 0.2 Hz. The values of the coherence functions are small at low frequencies. Also, the values of the frequency response functions are high for record NOS relating west conductor and strain gages. The values of the frequency response functions are high for west wind records relating east and center conductor loads with leg member stresses. In most cases, the frequency response functions and the coherence functions peak near 2.5 Hz. The coherence functions relating transverse conductor loads and strain gaiges are now considered. The coherence functions relating west wind records to leg member stresses are relatively higher than the coherence func­ tions for record NOS. The coherence functions peak with a value which is almost unity near 2.5 Hz. The coherence function has a peak value which is almost unity near 0.45 212

Hz even though the frequency response function does not show any peak near 0.45 Hz for record N05. Finally, the coherence functions relating longitudi­ nal conductor loads and strain gages are considered. The values of the coherence function at low frequencies are relatively smaller than the values of the coherence func­ tion at higher frequencies. The frequency response func­ tion at lower frequencies is generally higher than the frequency response function at higher frequencies. The magnitudes of the coherence functions and the maignitudes of frequency response functions near 3.0 Hz are relative­ ly small compared to the magnitudes of coherence and frequency response functions at other frequencies. The discussion of results and conclusions are now given below.

5.7 Conclusions and discussion of RegMlta The conclusions made in this section are based on the results obtained in sections 5.6.1 through 5.6.3. In particular, results obtained from power spectra analyses, frequency response function analyses, and coherence func­ tion analyses of the transmission tower are used as the basis for conclusions made in the frequency domain. The dynamic behavior of the transmission tower was analyzed using MSC/NASTRAN version 63 software. The 213 dynamic analysis of the transmission tower showed that the fundamental frequencies of the tower due to trans­ verse, longitudinal, and torsional responses are observed to occur at 2.87, 3.01, and 4.92 Hz, respectively. Higher frequency modes are not discussed because the frequencies of higher mode responses are greater than the Nyquist frequency of the tower response. The power spectra of the wind speed do not have significant energy content at higher frequency to corre- spend with the natural frequency of the transmission tower. Almost all the energy of the wind speed is accounted for at frequencies below 1.0 Hz. The power spectra of the transverse load values from west, east, and center conductors displayed significant energy near 0.2 and 2.8 Hz. These frequencies are associated with the fundamental frequency of the con­ ductor oscillations and the fundamental frequency of the transverse tower response. The power spectra of the longitudinal load values from west, east, and center conductor displayed signifi­ cant energy near 0.2 Hz, corresponding to the fundamental frequency of the conductor oscillation. In addition, significant energy is displayed near 2.3 and 3.7 Hz for outer conductors. Center conductor displayed additional 214 energy near 2.3 Hz only. The energy observed near 2.3 Hz is believed to be due to the non-vertical position of the outside conductor insulator strings (Kempner and Laursen, 1977). The energy seen near 3.7 Hz is attributed to subconductor oscillations (Kempner and Laursen, 1979) present only in the outer conductors. The fundaunental frequency of longitudinal tower response is not excited by the longitudinal load values. The presence of noise in the data acquisition system is seen near 1.0 Hz.

The power spectra of the strain gages are now con­ sidered. In all cases, noise or electronic interferences are observed at 1.0, 2.0, 3.0, 4.0, and 5.0 Hz. The SE main strain gaige 2 (SGOS) and the NW main strain gage 2 (SGll) displayed noticeable power near 2.3 Hz. The SE diagonal strain gage 3 (SGOS) and NW diagonal strain gage 3 (SG12) displao^ed noticeable power near 3.7 Hz. In all cases considered above, only record NOS displayed addi­ tional energy near 0.45 Hz. Record NOS indicated a general trend that wind speed is relatively stronger correlated with the main strain gaiges than with the diagonal strain gages. However, re­ cord NOS indicated a general trend that wind speed is somewhat strongly correlated with both the main strain 215 gages and the diagonal strain gages. The following con­ clusions may be stated: 1. The responses of the main leg members are signifi­ cant at the transverse natural frequency of the tower. 2. For smooth terrain, the wind speed affects main leg members more than the diagonal leg members. On the other hand, for rough terrain, the wind speed affects equally both main leg members and diagonal leg members 3. Wind speed affects the tower response at low fre­ quencies. Since the natural frequency of the tower is at a higher frequency, wind speed may be treated as a quasi-static loading. 4. The direct effect of wind speed is not the major contributing factor to the response at frequencies close to the natural frequency of the conductor oscillation. In considering the total conductor load values as inputs and strain gages as outputs, the following conclu­ sions are obtained: 1. Conductor loads contribute predominantly to the tower response at frequencies near 0.2 and 2.8 He. 216

2. The effects of conductor loads on the tower re­ sponse are more significant for west winds than for east winds. For frequency response functions relating transverse loads and leg member stresses, the following conclusions mao'^ be stated: 1. The transverse conductor loads contribute more significantly to the transmission tower response for west wind records. 2. Transverse conductor loads are the predominant contributing factor affecting tower response near 2.8 Hz. 3. The transverse conductor loads have more pro­ nounced effects on the main leg members than on diagonal leg members. For frequency response functions relating longitudi­ nal conductor load values and strain gages, the following conclusions mao^ be stated: 1. The longitudinal conductor loads dominate trans­ mission tower response at higher frequencies. 2. The longitudinal conductor loads effect more signi­ ficantly the diagonal leg member responses than the transverse conductor loads. 21?

In the case of the coherence functions, the magni­ tudes of the coherence at any frequency range from zero to almost unity. Since the transmission tower is a real physical system, a value of unity in the coherence func­ tion is not realizable. The following conclusions and observations may be stated for coherence functions which are less than unity at a particular frequency: 1. Noise is present in the system at that frequency. 2. The response is due to the load considered as well as to other loads not tadcen into consideration. These loads can act individually or together at the frequency in which the coherence functions are less than unity. 3. Nonlinearities may exist in the transmission line tower system. Statements 1 through 3 may be confirmed by performing the frequency response functions of the transmission tower structural system subjected to multiple loadings. In the following chapter, relationship between multiple loadings and a single response are considered. CHAPTER 6 FREQUENCY RESPONSE FUNCTION OF MULTIPLE INPUTS AND A SINGLE OUTPUT

6.1 Introduction In this chapter, the methods of Chapter 5 are generalized to deal with the frequency response function of a structural system relating several loadings and one response. Chapter 5 dealt with the frequency response function of a transmission tower structural system rela­ ting one load and one response. In general, the response of a transmission tower structural system resulting from a particular loading maiy be classified into two cases. First, the response of the transmission tower structural system may be entirely the result of the loading consid­ ered. Second, the response of the transmission tower structural system maiy result partially from the loading considered. The discussions for the two cases mentioned above are now considered. It is possible in theory to obtain the response of a structural system entirely as a result of a particular loading. Such phenomenon rarely occurs in a real struc­ tural system. The response of a structural system may be attributed to various loadings acting on the structural system. In the case of a transmission tower structural

218 219 system, the response of a particular structural member may be attributed to three possible loadings. First, the response of a particular structural member may result purely from the wind loads acting on the transmission tower. Second, the response of a particular structural member may result purely from the conductor loads acting on the transmission tower. Finally, the response of a particular structural member mao^ result from a combina­ tion of wind loads and conductor loads acting on the transmission tower. Results obtained in Chapter 5 indi­ cate that the effects of multiple loading on transmission tower structural system should be investigated to achieve a complete analysis of the response of the transmission tower. The dynamic response of the transmission tower due to multiple loadings is achieved through multivariate frequency response functions which are discussed in sub­ sequent section. In calculating the frequency response functions of the transmission tower due to multiple loadings, the assumption is made that the loading effect from the overhead ground wires negligible since the loads from the overhead ground wire are very small comparison with the loads from the outer and central conductors. In the 220 following section, the general requirements of multiple loads-single response are given in the following section.

6.2 General Requirements Material contained in Chapter 5 is now extended to multiple loadings problems. In particular, multiple loadings and a single response models are discussed. In addition, partial and multiple coherence functions are defined for these models and discussed in subsequent sections. Figure 6.1 presents a schematic diagraon for a struc­ tural system excited by multiple loadings and producing a single response. There are q clearly defined measurable loadings denoted by x (t) where i=l,2,...,q and one mea- i sured response denoted by y(t). Relating the q mea­ surable loadings to the one mesured response are the frequency response functions of the assumed constant- parameter linear systems denoted by H (f) where i i=l,2,....,q. The loadings may or may not be mutually uncorrelated. The response noise term N(t) accounts for all deviations from the ideal model. Deviations results from unmeasured inputs, nonlinearity of the structural system, non-stationary effects, and instrument noise. 221

y (t) 1 X (t) N(t) 1 y2(-t) X2(t)

y3(t) X3(t) .^(t)

y (t) i X (t) -HH (f)f i i

y (t) q X (t) ^H (f)f q q

Figure 6.1 Schematic Diagram for Multiple Inputs and Single Output System 222

Referring to Figure 6.1, four general conditions are required for the model to be well defined. These four conditions are:

1. The ordinary coherence functions between any pair of loading records should be less than unity. If the coherence functions between a pair loading records is unity, these loading records contain redundant information and one of the loading rec­ ords should be omitted from the model. 2. The ordinary coherence functions between any loading and the response should be less than unity. If this is not the case, model should be considered as a single load-single response model. 3. The multiple coherence function between any loading and other loadings, without considering a particular load, should be less than unity. If this is not the case, the effect of that parti­ cular loading is not providing any extra informa­ tion to the response. Therefore, redundancy occurs and that particular loading should be omitted from the model, 4. The multiple coherence function between the re­ sponse and the given loadings, in a practical sit­ uation, should be sufficiently high for the 223

theoretical assumptions to be reasonable. If the multiple coherence function is low, important loadings most probably are being overlooked or non­ linear effects on the structural system are signi­ ficant in determining the response. The schematic diagram shown in Figure 6.1 assumes that simultaneous measurements of the loadings and the response time histories in the model are possible. The final step involves estimating the frequency response functions of the system. The mathematical formulations of the frequency response functions are extensions from the mathematical formulation of the frequency response function for single loading-single response system pre­ sented in Chapter 5. Consideration is now given to a dynaonic system subjected to two loadings and one response.

6. 3 Frequency Response Function Relating luQ L£2adiQgs Qns. Rossons-S. In this section, the mathematical requirements in estimating the frequency response functions relating two loadings and one response for a structural system are discussed. Figure 6.2 is a schematic diagram for a system of this type. The loadings are represented by time series number 1 and time series number 2, respectively. 224

Time Series No. 1 Structural Time Series No. 3 Time Series No. 2 System

Figure 6.2 Schematic Representation of Two Loadings and One Response 225

The response is represented by time series number 3. As indicated previously, two frequency response functions must be estimated for a system subjected to two loadings and producing one response. Since frequency response functions are derived from impulse response functions, mathematical derivation begins with impulse response functions.

The impulse response functions are obtained by solving Wiener-Hopf equations simultaneously. For a dynaunic system subjected to two loadings and one re­ sponse, the impulse response functions h (u) relating 31 time series number 3 and 1, and h (u) relating time 32 series number 3 and 2 may be written in the form of convolution integral as

CO rOD c (u) h (v)c (u-v)dv + h (v)c (u-v)dv (6.1) 13 31 11 32 12

and •^co nOD c (u) = h (v)c (u-v)dv + h (v)c (u-v)dv (6.2) 23 31 21 32 22 u-CO where c = autocovariance function when i-j

i j • I. • 1 • = cross covariance function when ifj , 226

The time domain equations represented by Equations 6.1 and 6.2 may be converted to the frequency domain equa­ tions by taking the Fourier transforms of Equations 6.1 and 6.2, respectively. The frequency domain equations may be written respectively as:

S (f) = H (f)S (f) + H (f)S (f) (6.3) 13 31 11 32 12

end

S (f) = H (f)S (f) + H (f)S (f). (6.4) 32 31 21 32 22

Referring to Figure 6.2, S , S , S , and S are the 13 12 32 21 cross spectra relating the two subscripts; S and S 11 22 are the power spectra; H and H are the frequency 31 32 response functions relating the two subscripts. Solving for H (f) and H (f) gives the following expressions for 31 32 the frequency response functions, in terms of the power

and cross spectra:

H (f) = (S (f)S (f) - S (f)S (f))/D (6.5) 31 13 22 23 12 227 and

H (f) = (S (f)S (f) - S (f)S (f))/D (6.6) 32 23 11 13 21 2 where D = S (f)S (F) - S (f) 11 22 12

Equations 6.5 and 6.6 are complex expressions involving real and imaiginary quantities. Equations 6.5 and 6.6 can only be solved in terms of gains and phases as discussed in Chapter 5. The gains, G (f) and G (f), used to 31 32 estimate H (f) and H (f), respectively, are written together with the phases q) (f) and CD (f) as: ^31 32 2 2 G (f) = VA (f) + B (f) 31 31 31 2 2 G (f) = VA (f) + B (f) 32 32 32

d) (f) = arctanC -B (f)/A (f)] 31 31 31

(h (f) = arctanC -B (f)/A (f)] (6.7) '32 32 32 where A (f), i=l,2 represents the real quantities and Si B (f), i=l,2 represents the complex quantities. A (f), 3i ^^ 228

A (f), B (f), and B (f) are as follow: 32 31 32

A (f) = [L (f)S (f)+Q (f)Q (f) 31 13 22 23 12 L (f)L (f)]/D 23 12

A (f) = [L (f)S (f)-L (f)L (f)+ 32 23 11 13 21 Q (f)Q (f)]/D 13 21

B (f) = [Q (f)S (f)-Q (f)L (f) 31 13 22 23 12 L (f)Q (f)]/D 23 12

B (f) = [Q (f)S (f)-L (f)Q (f)- 32 23 11 13 21 L (f)Q (f)]/D. (^-9) 21 13

The squared multiple coherency spectrum is derived

from the residual or noise spectrum. The residual spec­

trum is written as:

S (f)= S -H S - nn (q+i)(q+i) (q+i)i (q+i>^ H S ^^-^^ (q+l)q (q+l)q 229 where q is the number of input processes. Equation 6.9 may be rewritten as

S (f)=S (f)[l- r^ ] (6.10) nn (q+l)(q+l) (q+l)12...q

where:

/^ = H S + + (q+l)12. . .q (q+l)l (q + l)l H S (q+l)q (q+l)q

= squared multiple coherency spectrum of the output process and q input processes.

The multiple coherency spectrum is used to measure the proportion of the response spectrum which can be pre­ dicted from the loadings. The terms described within the parenthesis of Equation 6.10 represent the remaining proportion of the response spectrum resulting from noise. The squared multiple coherency spectrum is obtained by substituting Equation 6.10 into Equation 6.9 and is written as:

/^ = 1 - |[S ]| /SS (6.11) (q+l)12...q (q+l)(q+l) 230

where |[»]( = determinant of spectral matrices

SS = S |[S ]| . (q+l)(q+l) qq

In the case of a system subjected to two loadings (q=2) and producing one response, the squared multiple coherency spectrum may be written as:

S S S 11 12 13 S S S 21 22 23 s s s (6.12) ^312 31 32 33 S S 11 12 33 S S 21 22

Expanding Equation 6.12 gives

2 . ,2 s Is I + s Is I - 22 31 11 32 2Re[S S S ]/S D (6.13) 12 23 31 33

where Re[«] = real terms of the product of the cross spectra. 231

Equation 6.13 is expressed in terms of the cross spec­ trum, power spectrum, co-spectrum, and quadrature spec­ trum of the three time series.

Two partial coherencies spectra may be estimated from Equation 6.13 and from Chapter 5. These two partial coherencies spectra are given as

X 2^1 (6.14a)

^3/a =1- 1-4 (6.14b)

2 For example, the partial coherency X,, measures the squared covariance at a particular frequency f between the processes x (t) and x (t) when allowance is made for 3 1 the influence of x (t). The idea developed in this 2 section can now be extended to numerical exaunples shown in the following section.

6.4 Numerical Examples of Transmission Tower Subjected to Two Loadings and One Response In the numerical examples presented herein, the transmission tower structural system is subjected to two 232 loads and one response. In particular, record NOS is used for numerical examples. In addition, combinations of two loadings selected are from LCOS, LC04, and LCOS, and they represent the transverse load values from the conductors. The responses are selected from SGOS, SGOS, and SGll. First, the frequency response functions of the trans­ mission tower structural system relating two loadings and one response are studied. Two plots for the frequency response functions may be obtained as described by Equations 6.5 and 6.6. Equation 6.5 describes the fre­ quency response function of the first loading with the response, and Equation 6.6 describes the frequency res­ ponse function of the second loading with the response (see Figure 6.2). Examples with proper observations are first given. Figures 6.3a and 6.3b present the frequency response functions relating wind speed as the first loading and transverse load from the west conductor as the second loading with the SE main strain gage record, respective­ ly, for record NOS. The plots are not similar in magni­ tude. Since the magnitudes of the frequency response function are relatively larger in Figures S.Sb than 6.3a, it is expected that the response of the leg members is affected more by conductor loads than by wind speed. 233 3 FRF OF HSOS RNO SGOS Oi urmrsHsos RM) LCO3) d o s '^m i (Ti d3 cn 3 a d u_ o I 8 z d o o a d 3 3 o •^ 3

O 2 d o 3 I I III) fi-^^WWI'L 0.0001 111 iiff 0.001 0.01 0.1 1.0 10.0 FREQUENCT (HERTZ)

Figure 6.3a Frequency Response Function Relating WSOS ^^H t^?.l ^'^^ "^^^ ^^ LCOS as Loadings and SGOS as Response for Record NOS

FRF CF LC03 PNO SCCS 81 ([Nnjr>HS05 RM) LCQ3)

m V)

C3

I z o - o

I

mrr tH- I I » T TTT» 0.0001 0.001 0.01 0.1 1.0 10.0 FREQUENCT (HERTZ)

Figure 6.3b Frequency Response Function Relating LC03 and SGOS With WSOS and LC03 as Loadings and SGOS as Response for Record NOS 234

Further, the frequency response functions are observed in both plots to occur between 0.1 and 1.0 Hz only. Also, the frequency response functions are most prominent in the range of frequencies between 0.2 and 0.5 Hz.

Figures 6.4a and 6.4b present the frequency response functions relating wind speed as the first loading and transverse load from the west conductor as the second loading with the SE diaigonal strain gaige record as re­ sponse, respectively, for record NOS. Again, both plots indicate that the non-zero values of the frequency re­ sponse functions occur between 0.1 and 1.0 Hz only. Values of the frequency response functions shown in Figure 6.4b are significantly larger than the values of the frequency response functions shown in Figure 6.4a indicating that the conductor loads affect the diagonal leg members more significantly. In Figures 6.3a through 6.4b, no noticeable spikes occur at 1.0, 2.0, 3.0, 4.0, and 5.0 Hz. This confirms the conclusion made in Chapter 5 regarding the presence of noise in the data accumulation system at these fre­ quencies . Figures 6.Sa and 6.Sb present the frequency response functions relating tranverse load from the west conductor as the first loading and transverse load from the east 3 FRF (F HSOS RhO SGOB 235 o o (IMPUTiKSOS RM) LC03) o R rvj o (D o M 3

Figure 6.4a «^H*^Qrn«^La?SPS5S? Function Relating WSOS ^ cSS^ ^^^^ ^^^^ ^^ LCOS as Loadings and SG06 as Response for Record NOS

FRF (F LC03 PNO SGOS ai (INPUT I HSOS RM) LC03)

rvj

cn a - m

a

CJ

g 2

I 111 iif I r I I • I III M- 0.0001 O.OOt 0.01 0.1 1.0 to.o FREQUENCY (HERTZ 1

Figure 6.4b Frequency Response Function Relating LC03 and SG06 With WSOS and LC03 as Loadings and SG06 as Response for Record NOS 8 FRF CF 10)3 PNO SGOS 236 (IMPUTiLCOa RM) LCO*l)

o o cc " O o 3 I I I I I lUj .A_ 0.0001 rrrr— 4l 0.001 0.01 0.1 1.0 10.0 FREQUENCT (HERTZ)

Figure 6.Sa Frequency Response Function Relating LCOS and SGOS With LCOS and LC04 as Loadings and SGOS as Response for Record NOS

8 FRF (F La)% RNO SGOS a lINPUTiLCOO RM) LCO«l) o

eg SO O cn o * ^^ cn 3 \ ^ a a Um- 3 1 n oz o ^-< CJ 3 ri« 3z o u. z 8 ^•^ CT . — C3 o a 3 I I I 1111A V TTTT f T T T f Iff^" 0.0001 0.001 0.01 0.1 1.0 lo.a FREQUENCY (HERTZ)

Figure 6.Sb Frequency Response Function Relating LC04 and SGOS With LCOS and LC04 as Loadings and SGOS as Response for Record NOS 237 conductor as the second loading with SE main strain gage record, respectively, for record N08. In both plots, non­ zero values of the frequency response functions are ob­ served to occur between 0.01 and 0.03, and between 2.5 and 3.0 Hz. It is expected that the response of the main leg members is significant at these non-zero values of the frequency response functions. The plots are similar to each other. This indicates that the outer conductors affect the response of the main leg members almost identically.

Figures 6.6a and 6.6b present the frequency response functions relating transverse load from the west con­ ductor as the first loading and transverse load from the east conductor as the second loading with SE diagonal strain gage record as response, respectively, for record NOS. The plots are similar to one another. This indi­ cates that the outer conductors affect the diagonal leg members almost identically. The values of the frequency response functions are observed to occur between 0.01 and 0.03, and between 2.5 and 3.5 Hz. Therefore, the re­ sponse of the diagonal leg members are significant at these frequencies when the transmission tower structural system is subjected to two outer conductor loads. 238 3 FRF CF LCD3 PNO SGOS a (INPUT I LCOS RM) L(3)4) o o

os CNJ (D 3 m r» ^^ O cn 3 \

2 10 0 o a

3 I I I • flllf ^-AI" " I I I I nn I 1 ri 1II n o.ooot 0.001 O.Ol 0.1 1.0 to.o FREQUENCY (HERTZ)

Figure 6.6a Frequency Response Function Relating LC03 and SGOS With LCOS and LC04 as Loadings and SGOS as Response for Record NOS

PRF CF \.ca\ rm SGOB

eo o (IMPUriLC03 RMJ L(3)*) 1 o o ^ ^_ (St a~ (Q o * 3 cn d ^^ C":D: 8in _ M o U- , 3 1 J Z d" o •—• a »C-J a ^~ •z. ° u^- s8 _ Z o" ^- o

g o= - o 1 3 °0. 0001 0.001 O.Ol 0.1 1-0 FREQUENCY (HERTZ1

Figure 6.6b Frequency Response Function Relating LC04 and SG06 With LCOS and LC04 as Loadings and SG06 as Response for Record NOS 239

Figures 6.7a and 6.7b present the frequency response functions relating transverse load from the west con­ ductor as the first loading and transverse load from the east conductor as the second loading with NW main strain gage record as response, respectively, for record NOS. The plots are similar to one another. In addition, the non-zero values of the frequency response functions occur between 0.01 and 0.03 Hz, and between 2.5 and 3.0 Hz. Figures S.Sa and S.Sb present the frequency response functions relating transverse load from the west con­ ductor as the first loading and tranverse load from the center conductor as the second loading with SE Main strain gage record as response, respectively, for record NOS. In both plots, the non-zero values of the frequency response functions occur between 0.01 and 0.03 Hz, and between 2.5 and 3.5 Hz. The maignitudes of the frequency respnse functions are higher at frequencies between 0.01 and 0.03 Hz than at frequencies between 2.5 and 3.5 Hz. Therefore, the response of the main leg members is more significant at frequencies between 0.01 and 0.03 Hz when an outer conductor and a center conductor are considered as the loads to the transmission tower structural system. Next, the partial coherence functions describing the 3 FRF CF [.033 RNO SGll 240 in o (irWT'LCOa RM) LOJiH ^ (\J U") 8:t m d c^n^ ^M^ ci) 3 « n U- o 1 o 3 «—t—• r« CJ a 3z : U. o z o

Figure 6.?a Frequency Response Function Relating LCOS and SGll With LCOS and LC04 as Loadings and SGll as Response for Record NOS

3 FRF CF Lix« mo sen lO (INPUr'LCOS RM) L(2}

E. 8

o 3 • III illl '•t I I I III 0.0001 0.001 O.Ol 0.1 1.0 10.0 FREQUENCY (HERTZ)

Figure 6.7b Frequency Response Function Relating LC04 and SGll With LC03 and LC04 as Loadings and SGll as Response for Record NOS 3 PRF CF L(3)3 RNO SGOS 241 OI (tNPUriLC03 RM) LCOS)

CNJ cn m v4 cn

CD m li. 3 zI o (— CJ

a 3 I I I llll I I I I III 'III nil" 0.0001 ^ iM'i—I- *i*i 1111?^ 0.001 0.01 0.1 1.0 10.3 FREQUENCY (HERTZ)

Figure 6.Sa Frequency Response Function Relating LC03 and SGOS With LCOS and LCOS as Loadings and SGOS as Response for Record NOS

3 FRF OF LCOS RNO SGCS (INPUT < LCOS RM) LCOS)

(NJ cn cn CJ

3 I o t— CJ

cr o

o \J •^J*L, 3 I IIIII ^ ^ -f^rV^ ,-rrrp TTI^ 0.0001 0.001 0.01 0.1 1.0 10.0 FREQUENCY (HERTZ)

Figure 6.Sb Frequency Response Function Relating LCOS and SGOS With LCOS and LCOS as Loadings and SGOS as Response for Record NOS 242 process in which the transmission tower structural system is subjected to two loadings are considered. Equations 6.14a and 6.14b are used to obtain the partial coherence functions which are discussed below. For a structural system subjected to two loadings, two partial coherence functions maiy be obtained. First, the partial coherence function relating the first loading and the response given that allowance has been made for the influence of the second loading is obtained. Second, the partial coherence function relating the second loading and response given that allowance has been made for the influence of the first loading is next obtained. These partial coherence functions are now considered. Figure 6.9a presents the partial coherence functions relating transverse load from the west conductor and SE diagonal strain gage record given that allowance has been made for the influence of the transverse load from east conductor. Similarly, Figure 6.9b presents the partial coherence functions relating transverse load from east conductor and SE diagonal strain gage given that allow­ ance has been made for the influence of the transverse load from the west conductor. In both plots, the values of the partial coherence functions are generally high. The plots are similar to one another. This is expected 3 COH. OF LC03 AND SG06 243 GIVEN LC04 S »— H CJ S 3z R u_ R UJ CJ § 2 lO UJ § UJ in z an CoJ :# R d 8 t—4 1— § Q£. OI CC a. § 8 3 O.OOOi 0.001 FREQUENCY (HERTZ1

Figure 6.9a Partial Coherence Function Relating LCOS and SG06 Given LC04 for Record NOS

3 con. OF LC04 and SG06 GIVEN LCD3

0.0001 0.001 0.01 0.1 1.0 lO.O FREQUENCY (HERTZ)

Figure 6.9b Partial Coherence Function Relating LC04 and SG06 Given LCOS for Record NOS 244 since the effect from the outer conductors on the diago­ nal leg members is almost identical to one another. Figure 6.10a presents the partial coherence functions relating tranverse load from the west conductor and SE main strain gage given that allowance has been made for the influence of transverse load from east conductor. Similarly, Figure 6.10b presents the partial coherence functions relating transverse load from the east con­ ductor and SE main strain gage given that allowance has been made for the influence of transverse load from west conductor. In both plots, the values of the partial coherence functions are generally high. This indicates that the effect from both outer conductors on main leg member is significant. Less fluttering is seen in Fig­ ures 6.10a and 6.10b than in Figures 5.SSa and 5.SSa. Also, the values of the partial coherence functions are relatively higher when two outer conductors are consid­ ered as the loads to the transmission tower structural system than values of the coherence functions when a single outer conductor is considered as the load to the transmission tower structural system. Therefore, two loads acting on the transmission tower structural system are better representation of the actual response of the transmission tower structural system. In addition, less 245 3 cm. OF LC03 RNO SGOS GIVEM LC04

0.0001 0.001 0.01 ( 10.0 FREQUENCY (HERTZ)

Figure 6.10a Partial Coherence Function Relating LCOS and SGOS Given LC04 for Record NOS

3 Ct». (F LCDI PNO SGOS GIVEN LCOS

z a o 01 H- R CJ S) ^ • U_ Ra UJ

CJ 0(D . lO

z (D O UJ UJ in n R o 3 CJ R cr 8

t— OO Q (k£ OI CC mn i 0- a 3 I llll iin I I I 111 m I llll iiip I' 111 til 0001 0.001 0.01 0.1 1.0 10.0 FREQUENCY (HERTZ)

Figure 6.10b Partial Coherence Function Relating LC04 and SGOS Given LCOS for Record NOS 246 fluttering is noticed between 2.5 and 3.0 Hz and the values of the partial coherence functions are high at these frequencies. Also, very little fluttering is noticed at low frequencies. The plots are similar.

Figure 6.11a presents the partial coherence functions relating transverse load from the west conductor and NW main strain gage records given that allowance has been made for the influence of the transverse load from east conductor. Figure 6.lib presents the partial coherence functions relating the transverse load from the east conductor and NW main strain gage record given that allowance has been made for the influence of transverse load from west conductor. The plots are similar to one another. Fluttering is less prominent between 2.5 and 3.0 Hz and at lower frequencies. The values of the partial coherence functions are generally large at most frequencies. In the following section, a discussion of results obtained in this section is given.

6^5 Discussion of Results In Chapter 5, the transmission tower structural system is subjected to a single loading and a single response is measured. In Chapter 6, an extension of the work of Chapter 6 is made by subjecting the transmis^3ion tower structural system to two loadings. The purpose of 247 3 COH. OF LC03 RNO sen GIVEM LC04

T^ I llll m; 0.0001 O.OOt 0.01 0.1 FREQUENCY (HERTZ)

Figure 6.11a Partial Coherence Function Relating LCOS and SGll Given LC04 for Record NOS

can. (F LCD* PNO SGll GIVEN LCDS

to.o 0.0001 FREQUENCY (HERTZl

Figure 6.lib Partial Coherence Function Relating LC04 and SGll Given LC03 for Record NOS 248

Chapter 6 is to provide evidence, if any, that the behav­ ior of the transmission tower structural system cannot be satisfactorily explained by considering only a single loading. Several conclusions can be made from the exam­ ples presented. In considering wind speed as the load to the trans­ mission tower structural system, it is noticed from the frequency response functions that the direct effect of wind speed is not significant on the transmission tower structural system (Figures 6.4a and 6.4b). Instead, the effects from the conductor loads are more significant to the response of the transmission tower structural system. This conclusion supports a similar observation made in Chapter 5. Since the direct effect of wind speed is not significant on the response of the transmission tower structural system, it becomes increasingly important to study the effect of conductor loads on the response of the transmission tower structural system. In general, when conductor loads are considered, non­ zero values of the frequency response functions are ob­ served to occur between 0.01 and 0.03 Hz. Also, non-zero values of the frequency response functions are observed to occur between 2.5 and 3.0 Hz which correspond to the 249 fundamental frequency of the transmission tower in the transverse direction.

The effects of the west and east conductor loads on the response of the transmission tower structural system are similar to one another. This inference is based on the similarity in shape of the frequency response func­ tions relating the east and west conductors loads and a strain gage record. If main leg member strain gage records are used as the response, values of the frequency response functions are significant between 2.5 and 3.0 Hz. However, if the diagonal leg strain gage record is used as the response, significant values of the frequency response functions occur between 2.5 and 3.5 Hz and near 4.5 Hz. This indicates that the response of the trans­ mission tower in the longitudinal direction has an effect on the diagonal members of the transmission tower. The values of the frequency response functions are significant in the frequency range between 0.01 and 0.03 Hz when the outer and the center conductor loads are considered. Also, values of the frequency response func­ tions are significant near 3.0 Hz which correspond to the fundamental frequency of the transmission tower in the transverse direction. 250

The partial coherence functions indicate that the effects of conductor loads on the diagonal leg strain gage records are less significant than their effect on the main leg strain gage records. The partial coher­ ence functions flutter very little at low frequencies. Also, very little fluttering of the partial coherence functions is observed near 3.0 Hz. In general, the large maignitudes of the partial coherence functions indicate that the response of the transmission tower is more accurately represented by considering two loadings as opposed to a single loading. Fluttering of the partial coherence functions may be attributed to two factors. First, the presence of noise may contribute to such behavior. Second, at the fre­ quencies in which the partial coherence functions flutter, some other input which is not considered in calculating the partial coherence functions is affecting the response transmission tower structural system. The possibility of non-linear behavior of the transmission tower at this point cannot be ruled out, although the large maignitude of the partial coherence function tends to suggest that the response of the transmission tower is mainly linear. Further study of the transmission tower structural system subjected to multiple inputs and 251 can provide a definite answer as to the type of response the transmission tower is experiencing. In the following chapter, modeling of time series is given. CHAPTER 7 TIME SERIES ANALYSIS AND MODELING

7. 1 Introduction This chapter deals primarily with modeling of time series. In particular, the methodology advanced by Box and Jenkins (1976) is used to model the time series of wind speeds. The definition of a time series is given in section 7.2. The concept in time series modeling is given in section 7.3. The mathematical models for sta­ tionary and non-stationary time series are described in section 7.4. The power spectrum of the time series model is given in section 7.5. Numerical examples of time series modeling are given in section 7.6 with a dis­ cussion of results given in section 7.7. The definition of a time series is first discussed.

7^2 Definition of a Time Series A time series is a set of observations generated sequentially in time. In particular, a time series may be classified as continuous time series or discrete time series. If the set of observations is recorded con­ tinuously with respect to time, a continuous time series is obtained. A discrete time series is obtained when the set of observations is recorded discretely with respect

252 253 to time. A time series may be recorded electronically or mechanically utilizing an analog device. An analog device records a time series continuously in the form of electrical signals. For analysis purposes, a discrete time series is preferred over a continuous time series because the former is more tractable numerically. A discrete time series may be obtained from an analog device using an analog to digital aid converter which converts a continuous time series into a discrete time series using a selected time interval. In the research reported herein, only discrete time series are analyzed. In general, most discrete physical time series are random in nature. The time series of the wind speeds are random in nature and cannot be duplicated. A random time series can only be described in terms of probability distributions. A random time series is called a stochastic process since it evolves in time according to probabilistic laws. In general, a time series usually provides an immense source of statistical information pertaining to the physical phenomena under­ lying the time series. A time series is usually obtained from data collected over a period of time only. It is feasible to collect data continuously over an unlimited period of time but such a data collection 254 process is usually inefficient. The data making up a time series is comprised of a sequence of observations. These observations can be thought of as a realization of jointly distributed random variables which can only be described in terms of probability distributions. These joint distributions maiy be used in forecasting the future values of a time series. More specifically, from the knowledge of the observed values of x , x , . . . . , x , a 12 t conditional distribution function for the future observa­ tion X maiy be obtained. This constitutes the basic t+1 feature in time series modeling. In time series modeling, a specific joint distribu­ tion function is never used to describe a particular physical time series. It is simpler to deal directly with the mechanism of the stochastic process generating the observations and to derive from the stochastic pro­ cess a conditional distribution of future realizations. In time series modeling, an attempt must be made to infer from the recorded data the mechanism which is generating the data. In a broad sense, this mechanism represents the statistical properties of the time series. The con­ cept in time series modeling is now given. 255

1. 3 Concept in Time Series Modeling Time series data are often used and examined in an attempt to discover any significant historical pattern that may be exploited in forecasting future behavior of the series. It is convenient to think of a time series as consisting of several statistical components. The statistical components of a time series are trend, cycle, seasonal variations, and irregular fluctuations. Trend refers to the upward or downward movement that characterizes a time series over a period of time. Trend usually indicates the growth or decline in a time series. The presence of a cycle in a time series represents the recurring up and down movements around the trend or around a constant mean, if no trend is present. A cycle tends to have a regular frequency and varying amplitude. Seasonal variations are periodic patterns in a time series that usually repeat themselves within a certain period in time. Irregular fluctuations are erratic move­ ments in a time series that possess no recognizable or regular pattern. Such fluctuations are considered in time series modeling after trend, cycle, and seasonal variations have been thoroughly considered in the mathe­ matical model and the model is insufficient statistically to represents the actual time series. Many irregular 256 fluctuations in a time series are caused by unusual events that cannot be forecast. The components of a time series discussed above do not always occur alone. The components mao^ occur either singly in any combination. For this reason, no single forecasting technique is superior over any other fore­ casting techniques. The most important problem to be considered in forecasting is to try to match the appro­ priate forecasting technique to the pattern of the available time series data. Upon selecting the proper technique, the methodology usually involves analyzing the time series data in such a manner that the different components present can be estimated by the technique. In the research reported herein, the Box-Jenkins methodology is used to model and to forecast a time series.

The Box-Jenkins methodology consists of a three-step iterative procedure. Figure 7.1 summarizes the steps involved in using the methodology advanced by Box and

Jenkins (1976). The first step in the Box-Jenkins methodology is called identification. In this step, a tentative model is obtained through preliminary analysis of the time histories. Upon obtaining a tentative model, the second step is executed. The second step is called estimation. 257

Postulate General Class of Models

Identify Model Tentatively

Estimate Unknown Parameters of the Tentative Model

Use Model to Forecast or control

y. End

Figure 7.1 Stages in Time Series Modeling Using Box-Jenkins Methodology 258

In this step, the unknown parameters representing the tentative model are estimated statistically from the record or time history of the time series. The third step is called diagnostic checking. In this step, the tentative model is checked statistically for adequacy to represent the actual time series. If the tentative model is statistically inadequate, the entire process is repeated. However, once a time series model has been developed, a fourth step, called forecasting, generates predictions of future values of the time series. The advantage of using Box-Jenkins methodology lies in its capability to consider the four components dis­ cussed earlier which may occur in a time series. Fur­ ther, the methodology is systematic and is capable of handling non-stationary data in the modeling process. Section 7.4 provides an in-depth discussion on Box- Jenkins Methodology.

7.4 Models for StatJonanx and Nonstationary Time Series. A time series Z where t=l,2,....,N of N successive t observations may be regarded as a sample realization that was generated by a stochastic process. Further, a sto­ chastic process may be thought of as being generated by a series of independent random shocks a (Yule, 1927). 259

These random shocks are usually assumed to be normally distributed having mean zero and variance CTn" From an engineering standpoint, this sequence of random variables a , a , a ,.... is called a white noise. The white t t-1 t-2 noise process a is transformed to the process Z by a t t linear filter as shown in Figure 7.2. In Figure 7.2, \J/(B) is an operator describing the dynamics of the sto­ chastic process, in that, it shows the relationship of Z 's and a 's. This relationship mao^ be written as: t t

Z =Lt-fa + >i/a + \[/a + t t ^1 t-1 2 t-2 = /X+ vj/(B)a (7.1)

where LL and \1/ are fixed parauneters and

2 >vi/(B)=l+^j/B-f\j/B + (7.2)

m where B a = a t t-m m = any integer.

\1/(B) transforms a intb Z and is called the transfer t t °° function of the filter. If E^ is finite and con- i»0 ' vergent, then the filter is stable and the process Z is C" 260

^(B)

White Noise, a. Linear Filter

Figure 7.2 Generation of Time Series From White Noise Through a Linear Filter 261

is stationary. If Z is stationary, then from Equation 7.1,

E (Z ) = E{/Ji) + E{\i/(B)}E(a ) t t ^ P- ' (7.3)

The variance of the process Z may be written as t 2 Var(Z ) = E [Z - E(Z )] t t t , 2 = E[a +\J/a + ] t I t-1 2 2 2 = E[a +^a + ] t / t-1 + E [cross product terms]

00 = ^n^E^ (7.4) 2 where OI, - variance of white noise.

Equation 7.4 is only meaningful if jJ. exists and the sum CD 2 2J ^ converges. Equations 7.1 through 7.4 form the 1=0 '• basis for time series modeling. The first stochastic model which is useful to model certain time series is the autoregressive (AR) model. In AR model, the current value of the process, Z , is t expressed in terms of the previous values of the process 262

^'^'' ^^-_/ ^ o' ' ^^^ ^ random shock a . This t 1 t—^ ^ AR model may be obtained by rearranging Equation 7.1 as follows:

a - Z - LL - \l/a - \]/a t t ^ M t-1 ^2 t-2 a - Z -jJ, - \J/ a - \i/ a t-1 t-1 ^1 t-2 2 t-3

a -Z -/^-\f/a -\^a -.... (7.5) t-2 t-2 'I t-3 2 t-4

Substituting Equation 7.5 into Equation 7.1 and re­ arranging gives

z = c^z + cbz + + (b Z t I t-1 2 t-2 p t-p + (5" + a (7.6) t where the weights cb placed on past observations are I functions of the \I/. weights and Q is a constant, which is also a function of ^ and the \|/ weights. Rewriting Equation 7.6 by letting Z,Z ,Z , t t-l_ t-2 be the deviation from U ; for example, Z - Z - U , ' t t then 263

z =(bz -fi^z 4-.... + (bz t I t-1 2 t-2 ^p t-p

^ \ (7.7) where O is assumed to be negligible. Equation 7.7 is called an autoregressive (AR) process of order p or AR(p). The final form of Equation 7.7 may be written in shorter notation as

cb(B)Z = a (7.8) t t where Cp(B) = autoregressive operator 2 p (JD(B)=1-4)B-4)B - - 9B

Equation 7.8 is essentially a regression equation because Z is related to its own past values instead of to a set t of independent variables. Equation 7.8 contains p+2 2 unknown parameters jJi , &) , (^ , • . • , (^ ' ^n ^ which "2 "^P have to be estimated from the data. The AR operator can be expressed in terms of \//(B) from Equation 7.1 as

v|/(B) =

The weights ^1/ > ^^ » ^ > , v|y in \|/(B) - (f) (B) should form a convergent series for the process in Equation 7.8 to be stationary. The AR process can be thought of as the output Z from a linear filter when the t -1 input is white noise a with transfer function 0) (B). t ' Equivalently as in Equation 7.1, an AR process may be used to express Z as an infinite weighted sum of a 's. t _ t Such an expression of Z in terms of the finite random t shocks is called moving average (MA) process.

A MA process of order q or MA(q) may be written by making Z linearly dependent on a finite number q of t previous random shocks a 's as: . t

Z :r a - 0a - fia - - fta . (7.10) t t 't-1 2 t-2 ^ t-q q Any MA process is stationary since ZJO; is always finite because there are a finite number of terms in the sum. If the MA operator of order q is defined as

BtB) = 1 - g^B - e^B^ -.... - ey c^-ii) then the MA model may be written as

Z - e(B)a (7.12) t t 265

In Equation 7.12, there are q+2 unknown parameters to be estimated from the data. These unknown parameters are

LL> Q, > • • • • ' Oq 2ind Gi. . Equation 7. 12 represents the MA process, Z , as the output from a linear filter t with transfer function y(B), when the input is random shock or white noise a . In time series modeling, it is t also possible to obtain another class of model which is a combination of both the AR and the MA model. This combi­ nation of AR and MA model is called the autoregressive- moving averaige model or ARMA model. An ARMA model of order p for the autoregressive components and order q for the moving average components or ARMA(p,q) may be written in mathematical form as:

Z=(|DZ +.... +(^Z +a t I t-1 P t-p t - Pa -....- Qa . (7.13) I t-1 ^ t-q

Rewriting Equation 7.13 in the form of the autoregressive and moving averaige operators yields

(b(B)Z = e(B)a ('7-14) t t

There are p+q+2 unknown parameters to be estimated from the data in Eqiaation 8.14. These unknown parameters are 266

f^' H^i ' ' ^p ' 9,^ ..... 9q; and CT^ . Equation 7. 14 may be used to express Z in terms of the transfer func- t tion and white noise a . Rewriting Equation 7.14 yields t

6(B) a. 2 = "T • (7. 15) C})(B)

Therefore, an ARMA process can be thought as the output

Z from a linear filter whose transfer function is t 0(B)/ (p(B) , when the input is white noise, a . ARMA t processes are more complicated than either AR and MA processes because more unknown parameters must be esti­ mated from the data. However, an ARMA process must be used if the analysis of a time series indicates that both autoregressive and moving average components are present. The final class of models to be dealt with describe non-stationary time series. Many time series exhibit non-stationary behavior and do not in general vary about a fixed level or a fixed mean. Although a time series may be non-stationary, occasionally it exhibits homogeneity in the sense that some parts of the time series have similar statistical properties in comparison with one another. Such homogeneous, non-stationary time series can be modeled by proper differencing of the time series to 267 produce a stationary time series. These models are called autoregressive integrated moving average (ARIMA) processes. An ARIMA(p,d,q) represents a process which is auto­ regressive of order p, moving averaige of order q, with a d th degree of differencing. An ARIMA(p,d,q) process may be written as:

•d CJ:)(B)(1-B) Z = Q(B)a (7. 16)

Equation 7.16 maiy be rewritten as

CJ)(B)V Z = 9(B)a (7.1?)

where \/ - (1-B) is a backward difference operator. In general, d is usually 0, 1, or at most 2. Equation 7.17 can be used to model both stationary and non-stationary time series. Equations 7.1 through 7.17 do not consider seasonal components of a time series. A seasonal time series may also be non-stationary. Transformation by differencing the time series once or twice in many cases may produce stationary time series. 268

Transformation by first or second differencing is de­ scribed in Equation 7.1S(a) and Equation 7.1S(b) respec­ tively as:

Z =\7 X = X - X (7. 18(a)) t t t t-1 2 Z -\/ X = X - 2x + X . (7.18(b)) t t t t-1 t-2

Frequently, seasonal differencing is required to produce a stationary time series. If L is the number of seasons in a time series, then the seasonal operator V may be L written as

„ L V = (1 - B ) . (7.19) L

In general, if D is the degree of seasonal differencing required to produce stationary time series values, then

D L D V Z - (1 ~ B ) Z . (7.20) L t t

If the variability of the time histories of a seasonal time series is constant with respect to time, then the seasonal time series possesses additive seasonal varia­ tion. If the variability of the time histories of a 269 seasonal time series is increasing or decreasing with respect to time, then the seasonal time series possesses multiplicative seasonal variation. A general transforma­ tion that will usually produce stationary time series may be written as

D d L D d V V Z = (1 - B ) (1 - B) Z . (7.21) L t t

Equation 7.21 maiy be used to describe an even more general form for a time series regardless of its varia­ bility. A seasonal time series may be AR, MA, or even a combination of both AR and MA. An extension of Equation 7. 17 to incorporate seasonal time series may be written as

, , L D d L Cp(B)cb(B )V y Z = Q(B)9(B )a . (7.22) L t t

Equation 7.22 is the final form of complete time series modeling for seasonal and nonseasonal time series. The invertibility conditions for a time series should also be checked for to ensure mathematical stability. The mathematical requirements for invertibility of a time series are discussed in detail in Box and Jenkins (1976). Upon obtaining and identifying the general class of model 270 for a time series, the next step would be to estimate the necessary parameters involved in a particular model. Identifying the behavior and characteristic of a time series as AR(p) and MA(q) or both is achieved through an analysis of the autocorrelation function and partial autocorrelation function. The autocorrelation function is given in Equation 4.4. The partial autocorrelation function may be written discretely as

/ r ; k=l 1 k- I - 5] r r / k j_| k—1,J k—J r =^ ; k=2,3,.... (7.23) kk k-l 1 - E r \ ij = l k-l,j j where r = r - r r for j = l,2, ,k-l. kj k-l,j kk k-l,k-j Equation 7.23 is also known as Yule-Walker equation. Equation 7.23 describes the relationship between the autocorrelation at time lag k to previous autocorrela­ tions. Table 7.1 provides a summary for the behavior of the general models discussed. Table 7.1 describes the gener­ al behavior and tendency of the theoretical partial autocorrelation function and theoretical autocorrelation function for AR(p), MA(q), and ARMA(p,q) processes. 271

Table 7.1 General Models

Model Theoretical Partial Theoretical Autocor­ Autocorrelation relation Function Function

MA(q) Dies down Cuts off after lag q AR(p) Cuts off after lag p Dies down

ARMA(p,q) Dies down Dies down 272

After a tentative model has been fitted to the data, a diagnostic check is performed to test the adequacy of the model. First, it is useful to study the adequacy of the model by examining the autocorrelation function of the residuals. The difference between the model and the actual time series at any point in time is referred to as the residual at that point in time. A graphical analysis of the residuals is most effective in detecting possible deficiencies in the model. In addition, a lack of fit test proposed by Box and Pierce (1970) using the Q sta­ tistic is appropriate to test the adequacy of the model. The Q statistic, commonly termed the Box-Pierce Chi- Square statistic, is computed through the analysis of the residuals. The Q statistics is given as:

k 2 Q = (N - d) E r, (^) ^'^•24) 1=1 ^

where N = number of observations in the original time series d = degree of differencing

2 .^ , r (€) = the sample autocorrelation of the residuals ^ at lag 1.

If the model is adequate, the residuals should be inde­ pendent and the autocorrelation of the residuals should 273 be small. Therefore, Q should also be small. A large value of Q indicates that the model is inadequate. The model is accepted if

Q ^ Xa^K - n ) (7.25) ^ P 2 in which ^ (K-n ) defines a point in chi-square dis- ^ P tribution having K-n degrees of freedom at the 95% P confidence level, and n denotes the number of parame- P ters that must be estimated in the model under considera­ tion. K denotes the number of autocorrelation terms of the residuals used in calculation of Q. Box and Jenkins (1976) suggested a minimum of 12 to be used as the value of K. Once the final model is established, the power spectrum of the model may be obtained by transformation of Equation 7.1. This transformation of Equation 7.1 into the frequency domain is given in the next section.

7.5 Power Spectrum of a Linear Process The power spectral density function of a linear process represents the rate of change of mean square value with frequency. The total area under the power spectral density function over all frequencies is equal to the total mean square value of the process. 274

Similarly, the partial area of a power spectral density function from frequency f to frequency f represents 1 2 the mean square value of the record associated with that frequency range. Power spectral density is useful in determining the system properties from input data and output data, in prediction of output data from input data based on system properties and vice-versa, in identifying noise sources, and in optimizing linear prediction and filtering. Although the power spectrum developed from an identified model is theoretical in nature, it provides a mean to predict the behavior of a system under simulated conditions. The general methodology in developing a theoretical spectrum from a model is based on the auto­ covariance function for Equation 7.1.

The autocovariance of a linear process described in

Equation 7.1 may be obtained as:

C = E [Z Z ] k t t+k 00 oc

j=o h=o J " t-j t+k-h

i=o J j+k 275

If the autocovariance generating function is defined as

C(B) = 2_/ C B . (7 27) k=-oo k

Substituting Equation 7.26 into Equation 7.27 and letting j+k=h such that k=h-j, then

2 ^ 00 . . h-j C(B) - ^ E S ^ ^B ^ j = o h=o j h

Cg^E vkB E ^B ^ ^^-.r^ H • ^ 2 = Cr^ Vj/(B) \j/ (F) (7.28) -1 where F = B = Forward shift operator.

The power spectrum of a linear process may be obtained -i2TTf from Equation 7.28 by substituting B=e , where i is the square root of -1, into Equation 7.28 to obtain one half of the power spectrum. Hence the power spectrum of a linear process may be written as

P -i2TTf i2Trf P(f) - 2Cr^\|/(e )VJ/(e )/\ —12 f 2 = 2A^4'(e ) , 0 ^ f ^ 1/2 A (7.29) 276

Equation 7.29 relates the power spectrum of the output from a linear system to the uniform power spectrum of a white noise input. The power spectrum of AR, MA, or a combination of both AR and MA processes may be obtained utilizing the AR or the MA operators.

In the case of an AR process of order p, the spectrum of the AR process may be written as

2cx?A P(f) = (7.30) -i2r7f -i2npf '- 4^ e -. . . - Cp e where 0 ^ f ^ 1/2^ ^^^ the denominator is derived from the AR operator, Cp(B). The spectrum of a MA process of order q may be written as:

-12 f -12 qf P(f) =2cr^^A 1 - 9,e 9*^ (7.31) where 0 ^ f ^ l/2/\. Similarly, the spectrum of a mixed AR and MA process can be written as

-i2rTf 1 - Q P(f) ^ !A (7.32 ^ '-^4- -i2TTf -i2n"pf, 2 (pe Cbe T»

The development of the power spectra given in Equations 7.30 through 7.32 were based on the transfer function 277 developed earlier by assuming a process to be generated by sequence of random shocks or white noise. Box and Jenkins (1976) discussed in detail some transfer function models. Numerical examples are presented in the next sectior

7j_6 Numericai Exampies of Time Series Modeiing 7.6.1 Time Series Models In this section, time series modemit; is discussed. The purpose of this section is to investigate and to show the possibility of modeling any physical time series if there are no restrictions. Restrictions in time series modeling occur usually as the results of time and eco­ nomy. The selected time series are modeled using Statis­ tical Analysis System (SAS - Version 5.16). The proce­ dures to model a time series are iterative in nature as described previously. The entire process of modeling a time series is tedious and time consuming. Also, numer­ ical computations involved in estimating the unknown parameters of autoregressive and moving average processes of a particular time series are lengthy even with the aid of SAS. Therefore, only a few selected time series are modeled and discussed. In this section, the time histo­ ries of WSOS for records NOS, N07, and NOS are modeled. 278

The time history of WSOS for record N16 was not modeled because the mean wind speed associated with this record has the smallest magnitude in comparison with other west wind records.

Table 7.2 summarizes the selected time series models. The models indicate that large number of moving average parameters are needed to model the time series of the wind speeds. The numerical values of the moving average parauneters and the statistics of the modeled time series are given in Appendix G. The adequacy of the models are based on Box-Pierce Chi-Square statistic indicated by Equation 7.24. The models are considered adequate if Equation 7.25 is satisfied. In Table 7.2, all the selected time series are non- stationary. One degree of differencing is required in all cases to obtain stationary time series plus noise components. In all cases, except NOS.WSOS, the number of parameters required to model the time series are large. The goodness of fit statistics of the modeled time series are given in Table 7.3. Table 7.3 presents the chi-square values of the auto­ correlations of the residuals. A minimum of 30 lags are used in evaluating the chi-square values of the auto­ correlation of the residuals to ensure a high degree of 279

Table 7.2 Identification of Time Series Model:

Series Degree Nature of time Identification of series for differencing Z t

NOS.WSOS 6th. order MA (0,1,6) NO?.WSOS 16th. order MA (0, 1, 16) NOS.WSOS 17th. order MA (0,1,17)

Table 7.3 Chi-Square Statistics of the Autocorrelation of the Residuals

Series Degrees Number Box-Pierce Chi-Square of of Chi-Square Values Freedom Lags Statistics

NOS.WSOS 23 SO 32.67 35. 17 NO?.WSOS 13 30 22.01 22.36 NOS.WSOS 12 30 14.85 21.03 280 accuracy. The chi-square values of the autocorrelation of the residuals are then compared with the standard chi- square values. In this case, a 95 % confidence level is used. It was found that the models adequately fit the time series. Upon obtaining the models for the selected time series, power spectra may be generated based on the models.

7.6.2 Power Spectra of Modeled Time Series In this section, the power spectrum of a selected modeled time series is generated. In particular, the power spectrum of modeled time series of wind speed for record NOS is presented as numerical examples. The var­ iance associated with the actual time series of the wind 2 2 speed is 9.30 m /s . Similarly, the variance associated with the modeled time series of the wind speed is 8.47 2 2 m /s . The power spectrum of the selected modeled time series is then compared with the estimated power spectrum of the time series used originally before it was modeled. Discussions regarding the estimated power spectra of any time series are given in Chapter 5. The numerical values of the MA parameters represented by G, , 9^ , , 9,7 of NOS. WSOS are given in Appendix G. The power spectrum plot is then overlayed with the power spectrum plot of the actual time series. 281

Two legends are used to identify the difference between the power spectra of modeled and actual time series. Solid lines are used to represent the estimated power spectrum of a time series, and broken lines are used to represent the power spectrum of a modeled time series. Figure 7.3 presents the comparison of estimated and modeled power spectra of NOS.WSOS. Both power spectra indicate little or no energy beyond 1.0 Hz. The term "energy" is discussed in the Chapter 5. The estimated power spectrum of NOS.WSOS exhibits peaks near 0.007, 0.03, and 0.06 Hz. Additional peaks are observed in the frequency range of 0.1 to 1.0 Hz. The power spectrum of the model indicates a peadc in the vicinity of 0.015 Hz. Discussion of results are now given in the following section.

7j_7 Discus.sion of Results The results obtained in section 7.6.1 indicate that any physical time series may be modeled using a suffi­ cient number of parameters. As observed from section 8.6.2, the power spectrum generated from the modeled time series are generally representative of the actual power spectrum. Furthermore, the model aids in checking t:he estimated power spectrum of the actual time series. 282

PO>CR SPECTWJH OF ND8.H505

Actual

a ^' I I I I I I I I I > •! 10.0 8 0.01 'O.OOl FREQUENCY (HERTZ)

Figure 7.3 Estimated and Modeled Power Spectra ^ of WSOS for Record NOS CHAPTER 8 CONCLUSION

The purpose of this research can be divided into two stages. First, the wind and associated transmission tower response data collected by the BPA at a full-scale test site in Oregon are analyzed. Second, these wind and transmission tower response data are used to develop the autocorrelation functions, cross correlation functions, frequency response functions, and coherence functions. In particular, four records were selected as representa­ tive of the twenty three available records for the purpose of this research. The selection criteria are summarized in Chapter 4. Also, earlier research to verify the time histories of the records indicated that the four records selected for the purpose of this research are valid (Norville, Mehta, and Farwagi, 1985; and Levitan, 1988). The research presented herein in­ corporates four major areas. These areas are now dis­ cussed briefly. First, the time histories of the records are plotted. Basic statistical properties of the time histories are summarized. Autocorrelation and cross correlation func­ tions of the time histories are next obtained.

283 284

Second, the response characteristics of the trans­ mission tower structural system under the action of a single loading is studied. The response characteristics of the transmission tower structural system is studied in the frequency domain. Power spectra, cross spectra, frequency response functions, and coherence functions are calculated and plotted.

Third, the response characteristics of the trans­ mission tower structural system under the action of two loadings is studied in the frequency domain. Frequency response functions, and partial coherence functions are calculated and plotted. Finally, modeling of the selected wind speed time histories using the methodology advanced by Box and Jenkins (1976) is performed. After the models are ob­ tained, the power spectrum of the modeled wind speed for record NOS is plotted for illustrative purposes. Several observations and conclusions have been compiled throughout the course of this research. These observations and conclusions are valid for the selected records. 285

1. The time histories of the wind speeds, conductor loads, and strain gaiges are found to be non- stationary based upon a study of the autocorrela­ tion functions. 2. The power spectra of the wind speed do not have significant energy content beyond 1.0 Hz. 3. The power spectra of the transverse conductor loads display noticeable energy near the frequencies of 0.2 and 2.8 Hz which correspond to the fundamental frequencies of the conductors and transmission tower, respectively. Also, the power spectra of the longitudinal conductor loads display signifi­ cant energy near 0.2, 2.3, and 3.7 Hz. The energy observed near 2.3 Hz is attributed to the non- vertical position of the outside conductor insula­ tor strings (Kempner and Laursen, 1977). Also, the energy observed near 3.7 Hz is attributed to sub- conductor oscillations (Kempner and Laursen, 1979). Again, high energy is concentrated at low fre­ quencies for the power spectra of the longitudinal conductor loads. 4. The power spectra of the main leg strain gages display significant energy near 2.3 Hz. In record NOS, main leg strain gages also display significant 286

energy near 0.45 Hz. Similarly, the power spectra of the diagonal leg strain gages display noticeable power near 0.2 and 3.7 Hz. Again, high energy is concentrated at low frequencies for the power spec­ tra of the main leg and diagonal leg strain gages. 5. The presence of peaks at 1.0. 2.0, 3.0, 4.0, and 5.0 Hz can be attributed to noise in the data acquisition system. 6. In the case of the response characteristics of the transmission tower structural system under the action of a single loading, the following observa­ tions are discussed. The responses of the main leg members are significant near the transverse natural frequency of the tower. On the contrary, the re­ sponses of the diaigonal leg members are significant near the longitudinal natural frequency of the tower. Therefore, the transverse conductor loads have a more pronounced effect on the responses of the main leg members than on the responses of the diagonal leg members. Similarly, the longitudinal conductor loads have a more pronounced effect on the responses of diagonal leg members than on the responses of the main leg member. The observations 287

made here are valid only for the selected strain gaiges considered.

7. In the case of the response characteristics of the transmission line tower under the action of two loadings, the following observations are made. The effect of conductor loads are much more significant on the response of the transmission tower struc­ tural system than the direct effect of wind speed acting on the transmission tower. Similar re­ sponses of the transmission tower structural system are found if the east and/or the west conductors are considered as loadings to the transmission tower structural system. Overall, the effects of conductor loads are more pronounced on the main leg members than on the diagonal leg members. The response characteristics of the transmission tower is explained much more satisfactorily by con­ sidering two loadings acting together on the trans­ mission line tower than one load acting alone. 8. A large number of parameters are needed to accu­ rately model the time histories of the wind speed records. In general, the power spectra generated by the models of the wind speed conform to the 288

general shapes of the power spectra estimated directly from the data. The pertinent conclusions made in 1 through 8 are expressed here because they represent more significant observations made from the examples presented in Chapters 4, 5, 6, and 7. Other less significant observations were made in Chapters 4, 5, 6, and 7 where discussions of results are given. The response characteristics of the transmission tower improved significantly as discussed in Chapter 6 by considering two loadings instead of one loading. The results obtained in Chapter 6 clearly indicate that current design method for transmission tower structural systems which utilizes superposition of all conductor loads makes a good design approach. Also, the trans­ mission tower structural system behaves mainly linearly. Therefore, the assumptions that the transmission tower structural system is a linear system in current design standard is also valid. The direction of future research parallel to the objectives outlined in the research presented herein should incorporate an in-depth analysis of the response characteristics of the transmission tower under the 289 action multiple loadings i.e., by considering more than two loads acting together on the transmission tower. LIST OF REFERENCES

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65. Texter, P. A., and Ord, J. K. 1985: "Forecasting Using an Automatic Intervention Detection System: A Comparative Analysis," Fifth International Symposium on Forecasting, June, Montreal. 66. Tuan, C. Y., Potter, M. T., and Jackman, D. E. 1985: A Field Study of Wind-Induced Conductor Loads," Proceedings of the Structural Division,ASCE, August, Kansas City, Missouri. APPENDICES

A. TIME HISTORIES PLOTS B. AUTOCORRELATION FUNCTIONS C. CROSS CORRELATION FUNCTIONS D. POWER SPECTRA E. FREQUENCY RESPONSE FUNCTION F. COHERENCE FUNCTION G. MOVING AVERAGE PARAMETERS

297 APPENDIX A TIME HISTORIES PLOTS

NQ5. LCOS u/«/ti ia.ta.3 uon czLL «. 9 j>« i%rt msr \ nOT one oa/iw? : > a.a n TOC > o.an Mil •CM - a.(B n INT. M 3 29.0 Kit TIK 1.1117 inr 3T1 KV 3 Q.2t DOT. MM • 2B.9I (M «.7S7 IWT STD CXV • 0.17 INT. NIN • 2B.eB I. IBS ... MM PTS/(I(T • to Tire HISTORT PBR 1.000 XDK) (NTCm. nVEIO&ES

s-klMli II * 9 " ". W "/"i'"f™i''Pi'IFP'pii, II

i.Jl.lt;ujiiili:r^il^ 11-9 m- 'T| 11 1 j-M' '1 MM f||i a I'l'lip'" '" HrtFH cr

• ' 1 • 1 • 1 I 1 ' I li 1 2 • 1« 12 TIME (MINUTES) Figure A.la Time History of Load From West Conductor for Record NOS

N07.LC03 U/l B/B a. OB. II. Loc OBJ. m. 9 JKS \an ICST caoumK nor OIK QK/iwr uoT. MR - a.a IN mc - j.ta an mm v.m KM INT. «« ' a.aB (M TDC ' 11.193 DIN IBT sn OEV : a.3i KM Iter. MM - 2».7j W mc • i.sa KIN INT STU CEV • o.a at INT. HIN • 27. a (M TDC - S.SQI NIN MM m/m • 10 rnc NisTocr PS 1.000 SECaO IMTEinRL RtflQEES

n- % LiiliiU.l.iJlilli \lU, k a 'iL ^[iinimiwMiwmmiimmimM N-l cr o in(T|iiT \'\mv I

-I ' 1 ' r 10 12 « • • TIME (MINUTES) Figure A.lb Time History of Load From West Conductor for Record N07 2)8 299 NOB.LCOS rnnun •I. 1. 9 j)-» isn rtiir ane mnwr UOT. MS > a. 0.31 n nm. MN - Z7.0B IN TDC • ICoa UN iiT STO act • 0.2 n INT. HIN • 37.71 IN TDC - 3.801 NIN MH PTVin • 10 TIM NISTOn POt 1.000 (ITEinn. (NEHEES

.IkilJl)^ al.. ...mJil.j n iiiLit'.'K.-vr-ii .'iti.iBkf••vjkA:'dL^i«b*Mt4u;"r Mmuu N- S IMHII f\ II T a (E

T T r —I • a I la 12 TIME (MINUTES)

Figure A.2a Time History of Load From West Conductor for Record NOS

N16.LC03 .11.] I. 9 jy II mnwwt tioT. MS - a.a n II.aa Ha INT. mi a 2&.21 W TDC a 0.000 in I0T 3T1 KV « o.a OI TDC • 0.219 nm IHT STD CeV • INBT. WH > aB.M IN 0.07 OI TDC • 7.017 NIN MM PTVir • INT. HIN • a.a IN 10 TIM NISTOer PK i.aoD (HTBm. (MI0EE9

Z -i i ti.ii. I I . N* 9 N II il'iillUU. i.i'lll MMIii'JMikMII ll.'Ul.iri'tii. MTri'.aL'Ifel.U.'liMIIU-UII N- 9 '^'i I "1 -y*- " I a »M 11 ao:

—T ' 1 ' I 1^ 1 U « a • TIME (MINUTES)

Figure A.2b Time History of Load From West Conductor for Record N16 300

NOB. LCOU ,a/, .10.3 uam ou. m. % jy ia/« OBT nor one - mns/m IM9T. MR - a.37 IN TDC • l.flOi NIN «A« > a.a ot IMT. m 3 aB.« KM TDC = l.aOl IIN INST STV OeV : 0.01 OI INBT. WN - 29.9 KM TDC - S.tBS IIN INT STD OEV • 0.07 IN INT. NIN • a.07 KN TDC - J1.7B7 NIN nm PTVIRT • to niC HISTORT FOR 1.000 XCOO tNTOWL fWHOCES

N* 9 Z

II - i a cr o

TIME (MINUTES)

Figure A.3a Time History of Load From East Conductor for Record NOS

N07.LCOU «/ .SI. Bi. «. « jy lun OBT cm rujr one m/iwT IIOT. •«• - TT.m IN n>c - i.tn NIM ICM a.aB KM INT. mm > 27.(B IM TDC 3 S.I81 NIN IBT STl OEV : 0.S CN INST, rtn • 71.99 IN TDC " 2.8a NIN INT STD CZV • o.a KN INT. HIN - a.«i KN TDC • I.S17 NIN Mil PTVIRT • 10 Tue HiSTonr pat i.ooo SEcam INTDPIR. BWIMBES

«• 9 I.II.JI. ..I.ILIHHMIIIIM IliUllllij .J.lll .Mkk\ [jJiiiT.Viiiii'^;virt.iTi,iiniii*iiLiru. y 11/iri^M UMiil[ B- 9 o jTI ]\fl\] II|[|'i| Ml 1(1 [|i' ^^ cr

T T -1 T 10 t a i 12 TIME (MINUTES)

Figure A.3b Time History of Load From East Conductor for Record NO? 301

NOS. L(Xm oi/mym •i.ii •• « JI-* ivn am rur OIK OB/IW . MM • a.a m i-OOi NIN INT. mi a 27.8S IN TDe a %.aaa NIN inT STl KV 3 0.31 EM INBT. r«N - a.a w Tire" I.971 NIN IHT STD tZV • 0.a KM INT. NIN • 21.00 IN TDT • L9a NIN MM PTVIITT • ta TIK nSTSKT PK I.COO O IhTBHR. RVEMZS

\]i^.i.L,i]}i..Mu!it\it,^ a* 9 •III jBi.'iii'.ij. u/ik'i iir.'.'.iiMiyiMuakMiJc/kiiniii.?: i>;.*fii' N- 9 'JT

a oCE

-T ' 1 ' r -T tat ta U TIME (MINUTES)

Figure A. 4a Time History of Load From East Conductor for Record NOS

N16.LC011 tafwta a. 11.] I. « Jhm II m/wmr ifBt. mt ~ 2B.n IN TOC • II.BV NIN • 1B.S9 KM INT. mm a a.a4 IN TDC a ]|.917 NIN tar STl OEV a 0.11 KN INBT. r«N - 2B.S1 IN TDC • 2.3a NIN INT STD IZV • O.a (N INT. nm - a.st IN TDC - 7.799 NIN MM PTVIRT • 10 TIIC MISTOer FOR l.OOO (KTonn. menus ^1

H« 9 t^.Ji'jilh.iJ.tiaMitJI'^ LMI N uii iMuiMViii l•ukl'lllJ•.w1ml.^J'.v.^ltLWfllr^.'iy N- S T-.| • 4- v "" 1 ^T a cr o -1 B

-I • r -T I 10 12 « a TIME (MINUTES)

Figure A.4b Time History of Load From East Conductor for Record N16 302 NG5.LCOS u/ La» cm. m. i jymian cmmt nor one aB/lS/«7 M T1»C - 0.117 NIN INT. laV 3 2B.V IM a.a Oi Tnc 3 i.aoi UN IHT STl OEV I INST. WN - 27.n IN 0.01 a TDC - I.3SI NIN INT STD OCV • INT. NIN - a. 01 KM o.a KM TDC " 11.017 UN nm PTVIRT . to TIW MISTORf POR .000 XCSO (NTHnPL HVEIBEES

a cr o

•^ 1 ^ ~T ' 1 ' r -. 1 r- 2 I « a • 10 12 TIME (MINUTES)

Figure A.5a Time History of Load From Center Conductor for Record NOS

N07.LC05 01/ .It. k 9 l»n nor oNK oKA&v? Ml • a.9 m TOC • S.V71 NIN ICRi > 77.a KM INT. mi a a.a IM TDC a s.aa IIN inr sn KV t a. 31 KM IMT. nn - a.2i IN TDC • i.Ta RIN INT STD OCV • 0.a CN INT. NIN - a.si IM TI7C • }.an NIN MM PTVIRT • 10 TIK HISTTKT POt 1.000 XON) INTOm. nVEMGES

a ocr

T -• r 10 12 « TIME (MINUTES)

Figure A.Sb Time History of Load From Center Conductor for Record NO? 303 r 108. LCOS ai/xyu It.! ax w. 9 Ji-a la/N icMia cBnuncK njor ane ai/iv«7 tm. MM - 2a.a IN TOC • 1.017 NIN mm a. 17 KM INT. mc 3 29.(M IN TDC 3 1.058 NIN IBT STl OEV 3 0.31 CM INST. MN - 27.13 IN Tin - 2.8a NIN INT STD OEV • o.a KM INT. IIN • 77.S0 IM TDC - 3.117 NIN MM rrviiT • 10 TIK IISTORT PCM 1.000 5EC90 INILKNl RVEIQUES

z

N- S Q cr o

•• r 1 ' r —r 12 2 a a 10 TIME (MINUTES)

Figure A.6a Time History of Load From Center Conductor for Record NOS

NIB.LCOS njoi one m/ia/wt I cax M. 9 J>m iwN camR • a.ns NiH mm - a.ia a INST, mt « a^9 IN TDC a 12.000 NIN IBT STl KV « 0.U KN INT. IM a 2B.S1 IM TDC - 9.119 NIN INT STD orv • a.11 KM IMBT. WN - Z7.a IN TOC - S-"T IIN MM PTVIRT • 10 INT. NW - a7.a IN (VTEinPL RVCMZS TIK NHTBRT BK l.OOO

a (oX

T T T a • • 10 12 TIME (MINUTES)

Figure A.6b Time History of Load From Center Conductor for Record N16 304 NOS.SflOS ia,«« M.10.2^ »iBo loau m. 9 jD-9 i%/% ICST caai. •« oit. PUT line oi/i2/mr IN9T. MV - l.M OBB TI>C - O-OPIS NIN ICPR (Laa ocB INT. IM s 1.07 DEC TDCs 1.833 NIN IIOT STB OEV 0.11 [SB INST. MIN - 0.29 DEC TI« - I.3S7 HIN IMT STD OCV 0.09 ZO INT. NIN « 0.72 OEB TDC i.asn NIN 10 ^ TIK NISTWr RK l.OOO SGQK) IKTHnBi RVEmEES

TIME (MINUTES) Figure A.?a Time History for West Conductor Longitudinal Swing for Record NOS

37.Sfi05 ot/M/a m.m.n. trntmoLgm, sJO-9 IM/* ICST cao. -41 on. nor ome oi/ia^vT liST. WH > 3.S KB TDC > LSia RIN KPN -.01 OBB mr. Nn s 0.W KB TDC 3 n.oos RIN nsr sn KV 3 1.12 (ZC INST, nn - -«.31 lEB TDC > 9.>ta9 NIN IRT STOOrV • 0.91 tro INT. NIN - -l.SI OEC TDC • o-tas NIN hm PTVIRT • 10 TIM HISTORT P(K 1.000 SECOKI (ITCXTFL flVERMGES

UJ l!fV^'f\ F'nf rj' CC

-T ' 1 ' T « i I 10 12 TIME (MINUTES)

Figure A.7b Time History for West Conductor Longitudinal Swing for Record NO? 305 NOa.SflOS auu^ ...3^,^ alias max n. s .»« ii/i icsr can. •« oia. oar ome 0I/L2««7 [•«.*I- 2.31 OtB TOC. 1.307 .IN -.21 OBB «;^-' 0.39 OEC TDC= 2.H7 NIN iNsr STU DEV 0.62 ZC S^'-^ *'•" "=* "«-•.•« NIN IHT STO OCV a22 oes JJi!" " -•* <«> TDC- 7.1S7 NIN UM PTS/INT 10 TIK HISTORT RK I.OOO SEDIO IHTDftH. RVCnCES

a a

TIME (MINUTES)

Figure A.8a Time History for West Conductor Longitudinal Swing for Record NOS

N16.Sfl05 oi.ci« «..,.«r aiias maLC NO. S JD-O la/i ICTT caai. -m ou. nxM oi/iavr INST. MV - 0.11 OBB TT»C - 7.339 HIN mm m 0.19 OS IMT. HPK a 0.«| DEC TDC s 7.039 NIN lasr STO OEV > 0.00 IZC IWT. MN - -.02 OEG TDC - I.2Z7 NIN Iir STD ccv • o.a (Es IMT. HIN • 0.02 DEC TDC -J. 139 NIN MM PTVIRT • 10 TIK NisTonr POR 1.000 xnio (NTERVRI RVC«Z3

« • I TIME (MINUTES)

Figure A.Sb Time History for West Conductor Longitudinal Swing for Record N16 306 NOS.SflOS ia/]8/ai 11.10.20. ^im (Uk£ m. a jy i^ vit cwti •T OIR. RJST ONK Ol/l^W INSR.HWs -7.38 OCB riK a u.ZO ua -a.9 Its IMBT STO ORV : o.a so INST, nn - A.ia an nm - a.oa HOI INT aro (TV . 0.19 les UMPTVOUT i U) TtK HCSTWT F« i.ooO SECOK INTBtVW. flVBtffia TIME (MINUTES)

Figure A.9a Time History for West Conductor Transverse Swing for Record NOS

N07. SP)06 ot/ta/a a. 01.91 3MIM max IB. B JD-O !•/« ICST CaO. tt OIR. not one n/t.3fwf INBT. MM • t2.a KB TOC - t.79 •IH KPN 3.02 as INT. mi = S.i« OEB TOC a 2.907 IIN INST yn KV a 1.8« OEB INST. MIN - -1.79 DEC TDC • 1.827 IIN IHT STD CZV • l.n OEB INT. NIN • -1.17 OEB TDC - 1.831 IIN MM PTVIIT • 10 TIK HISTORT PK 1.000 (RTDrm. fWCKHQES

o z Z (D

—I 1 1 1 [- 1^ a a I 10 12 TIME (MINUTES)

Figure A.9b Time History for West Conductor Transverse Swing for Record NO? 307 NG8.SPI06 01/31/B .,.a.jx atiio max HO. a JO-B i»/\ »cn CBMI. •»» OIR. rujr ome mm/vj IIOT. MM 12.92 •B TOC - l.oa HIN 7.07 lEB INT. mi 11.49 OEB TDC a l.SOa IIN INST STl KV 1.51 ZC INST. MIN 9.n OEB TT7C • 10.089 NIN IRT STD OCV l.

CD UJ !S- a

UJ N • 3

z cc H- 9 o z I—t ' cn

—r 10 12 TIME (MINUTES)

Figure A.10a Time History for West Conductor Transverse Swing for Record NOS

N16.Sfl06 avi2/a2 19.031. 9IIIM- PMLC m. a j»-a ia/« KST CMS. *T OIR. lUT ONV ai/i2^w IlOr. NM a ^37 OEB TDC a ll.SOS MM mm a -I.S QB INT. NM = -.at 0B» mc = 0.000 MM INBT STB ORV : a.a oo iMV. mm m -i.oa OEB TDC - 7.3» MIN INT STD KT - a.a KB INT. RIN 3 -1.90 CEB TIK a 7.517 N0« NLMPTVOfT a 10 TtK RISTKT FK 1.000 9BC0K INIBTNC mSRCES TIME (MINUTES) 0 2 a B B 10 12 1 . 1 . 1 • 1 1 1 a

c^ A 1 • . ft 1.. ^ B iWAji/V.^AALr i^irr^y^ tin. ,J\j. T > ^. \\^jhAr'/iMrV ,.I , UJ

cr

CO

Figure A.10b Time History for West Conductor Transverse Swing for Record N16 308 N05.SR07 la/a/a a.io.a. aiias i«ax m. i jo-s la^ am CBM. -HI OIR. na ore 0l/l2i^B7 INSI. MM • 2.a OBB TOC • 1.209 NIN mm m 1.9 ITB INT. NPR a 1.82 DEB TDC a |.817 NIN INST STl KV a 0. IS OEB IWT. MIN - 0.99 ORB TDC • I.SIQ NIH IRT STD ORV . 0.07 IZB INT. NIN • 1.37 OB; TDC - 2.717 NIN MM PTVIRT • 10 TIK HISTORT FOR 1.000 KCOKJ (NTDPM. RVEHCES

UJ ^ a

J. .wiji..—:atnL d:- i.'.iipjLiur.T,. I "iiu '' H'" I """niT c5 z "--^ cn

1 ' r 10 12 2 a TIME (MINUTES)

Figure A.11a Time History for East Conductor Longitudinal Swing for Record NOS

NG7. SR07 ot/«« a. 01.91. atiao mar HB. 7 JD-O la^ OVT CBML -m on. rur one 01/12IV7 ncn. MM > a.a KB n>C • LOTI NIM ICM I.a KB INT. HFR a 2.20 KB TDC a 11.150 IIN t»T STl OEV a 0.a OEB INSI. WN - -S.7<1 ORB TTK • •••Ml HIN INT STD err • 0.39 (0 INT. NIN • O.IIS OEB TDC • 2-aB7 IIN MM PTVIRT • 10 TIK HISTORT PK 1.000 SECOM) (RTEim. flVEtfCES

aUJ „-

UJ

cc C3

czn

a a I TIME (MINUTES)

Figure A.lib Time History for East Conductor Longitudinal Swing for Record NO? 309 NGS.SflO? auj,m ,i.M.a. mnm tmmx mu. r JD-» i»n am ram. *€ oil. puir one 0I/12««7 INSI. i«R • a.OT OBB TOC - i.i«n nm KRH l.Sa OBB INT. IfC 3 2.81 OEB TDC a J.iw UN lei sn OEV a X7i ZB IWT. niH - -1.17 OBB TDC • l.2n NIN IRT STD ORV • 0.9 ZD INT. NIN - a.lS OGB TDC - I. IBS NIN MM PTVIRT • 10 TIK HISTORT PK 1.000 SCON) tNTOrMl nVEHGES

H» 9

a a I TIME (MINUTES)

Figure A.12a Time History for East Conductor Longitudinal Swing for Record NOS

NlS.SfiO? ovta/n s. 19.901 MIHOIWILe NB. 7 l-O la^ OVT CDW. -HI Olf. PUTT one 01/12^97 IN9T. MM • 2.IB ORB TDC ' 7.079 NIN I.a OEB INT. IFR a 1.9N OEB TDC a 7.0B9 IIN IBT sn KV a 0.11 lEB INST. MIN - O.Sa ORB TI rC • 0.B7Z NIN IRT STD CRV • 0.19 OEB INT. NIN • 1.01 OEB TDC - 11.700 NIN MM PTVIRT • 10 TIK HISTKT FOR C SCON} (RTEim. Rvcnvzs

C5 UJ a

UJ g .0 OJ cc C!) z z en

T T -r 12 a a I 10 TIME (MINUTES)

Time History for East Conductor Figure A.12b Longitudinal Swing for Record N16 310 NOS.SflOS 12/is/ai ii.io.20. 9IIIS fMU MB. 0 J0-« IS/a ERST CWtL *T OIR. PLOT OMIS - 01/12^*7 INBT. MB= -1.27 tXB riK a 11.757 NOl mm a -2.02 OCB INT. NKI = -1.83 CE» riK = 1I.307 nCN IfQT STO OEV = O.a OO INST. MIN - -I.a OCB rilC • 1.07 NIN IMT STD trr - 0. IS UCS IWT. NIN = -2.43 OEB riK a 2.133 MM lUIPTVtMT a 10 TIK HISTKT FK 1.000 secora iNTBtvia. mstpoa TIME (MINUTES)

Figure A.13a Time History for East Conductor Transverse Swing for Record NOS

NG7. Sfl08 oi/Na/ B ]a,ai.si aiRB nar NO. B JO-S la/a oar am. «r oii. rur one at/i»v7 INST. MM - 10.07 DEB TT»C • i.aa NIN mm a.as KB INT. «« a 15.113 OEB TDC a 2.989 NtN INST STO OEV a 1.89 (ZB INSI. MIN - «.n DEB TDC • S.7a NIN IRT STD CRV " l.M (KD INT. HIN - S.a OEB TDC - 1.89 NIN MM PTVIRT • 10 HK HISTORT PK 1.000 XQN) (HTOtm. nVERMGES

a a I TIME (MINUTES)

Figure A.13b Time History for East Conductor Transverse Swing for Record NO? 311 NOS.SflOS oi,3,;B „.a,.,i ano Max m. a jo-» i»f% am cam. ••» oo. nor one 0IA2^«7 INSI. mi m |«.2i TI>C - 1.019 NtN 19.a BB INT. mm a |8.(]g OEB TOC a 1.050 UN INST, nm m f.77 INST 3T1 OEV 1.57 ZB KG TOC - 10. UB HIN IRT STD OEV INT. IIN - 10.0» I'll m OEB TDC - 10. la NIN MM PTVIRT to TIK HISTORT PK SEcao (NTEmn. RVEBHZS

TIME (MINUTES)

Figure A.14a Time History for East Conductor Transverse Swing for Record N08

N16.Sfl08 dvtsuia IS.19.9a ane WMLC m. a a-« la^ amT cao. *f oil. rur one aw\.2/m INST. MM • a.

a a I TIME (MINUTES)

Figure A.14b Time History for East Conductor Transverse Swing for Record N16 312 NQ5. SflG9 13/a/n a. 10.a. atiio MOLC m, 9 jo-B 11/1 coTT cao. «• oil. nor tMie 0I/12/V7 INST. MM - 9.M OEB TOC- J. 179 NIN mm m 2.85 CZB INT. »« a 3.12 OEC roe a 1.817 NIN INST STO OEV a 0.17 OEC IIOT. MIN - 2.37 OEB TOC " 1.3a NtN INT STO OEV • 0.09 oro INT. HIN - 3.9 OEB TDC • J.OM NIN MM PTVIRT • to TIK HISTORT PK 1.000 SEOSO (NTEinn. nVEHCES

UJ

H • S UJ Tipv 'iwiniriiriri'.iii/.Hi'ifiTfiii.i x."ii 'LiiAiuiiii'.'i'iiipt"! N r >^rr|Jyy,vJl;|'••:^i'|||••ll•l.r,|1Ji4J.|^,,,••yi^J-K..l m N- S g m ii ]]W ' 1 '"vwi cr

z CO -r a 0 0 to 12 TIME (MINUTES)

Figure A.15a Time History for Center Conductor Longitudinal Swing for Record NOS

N07, Sfl09 ou a, 01.91. 4« OIR. aiRO maz NO. a jym la/a can nor arc oi/ia^«7 mi. MM > ia.a OEB TDC • i.'rn HIN KPR - I.a (^ INT. l«« > 2.97 OEB TDC a 30.217 NtN INST Sn OEV a 1.39 OEB INST. rON - -S.8Z OEB Tire > 7.971 NIN INT STD CEV • 0.37 OCB OfT. NIN - 0.91 OEB TDC - 1.339 NIN MM PTVIRT • to TIK HISTORT PK 1.000 (RTERtn. HVEDCCS

^ ^ ^--1

UJ

JLiJIkJiiL Ai. >1 • 9 z N i.ll.'i.'il I 'ir.VII.'. f'"!.! 'T.MllJliJi.U'. 't* I .Miii—HMumjg H- S i» CO ur ™r 'HI

I —r 12 10 TIME (MINUTES)

Figure A.15b Time History for Center Conductor ** Longitudinal Swing for Record NO? 313 Noa.sflog o,^« ,,.3,.^ aiio n«r m. 9 jo-e i»/% can COMI. -HI OM. rur CMTE 0IAa>V7 INST. MM > 7.U OBB TT>C - 1.389 in INT. vat 3 2.2 (ZB 3.a8 OEB TOC a 2.581 RIN IBT STB OEV a INST. r«N - O.a ZB -i.ta oco Tire - 2.331 HIN IRT STD DEV • INT. IIN • 0.31 CEO I.S DEB Ti>c - i-aa NIN HM PTVIHT • 10 TIK IISTIKT FOR l.OOO SEOX) tRTQWa. BVCWGES

N * S

TIME (MINUTES)

Figure A.16a Time History for Center Conductor Longitudinal Swing for Record NOS

NlG.SflOg -s/oaa s.ii.n. aiBO roHU m. 9 JD-O iva CDTT can. -t aiu njot one n/12/vr INST. MM • 2.a OBB TOC • 7.a«9 IIN mm m 2.91 OS INT. MM a 2.01 OEB TT7C a 7.a5r NIN lar sn OEX a 0.111 IXB INST. MIN • 1.09 OEB Tire • 3.029 NtN IRT STD CEV • 0.19 IZB INT. NIN • I.a OEB TDC - «.a33 UN MM PTVIRT • 10 TIK HISTORT FK 1.000 XCOMI IRTEXTRl HVERMGES

cc

z CO

1^ to 12 TIME (MINUTES)

Figure A.16b Time History for Center Conductor Longitudinal Swing for Record N16 314 NQS.SfllO la^n^i iB.1a.20. Slia IMU 10.10 JD-B IV% SXT CMRL «r OIR. njm ome oi/i^w INST, fais -«.8a OEB riK a 11.718 NO* icn a -6.31 aa INT. NPB = -«.a OEB TIIC : 11.791 NIN IWT STD OEV = O.a aa iRsr. MIN - -«. 10 OEB riic > i.aa Mot INT 3TD CEV - 0.17 DEB INT. NIN 3 -5.80 OEB TIK a l.SEI NOl MMPTVOTT a 10 TIK HISTKT FK 1.000 SECOM INIBtvn. PUBOVES TIME (MINUTES) to 12 _J

UJ o iiliiii.. ,.,i.jiykii„kn.il^iJM

^i.a7':nin;u.''j:;yiT'iHkiikiii;yui/,iii M - 9

Figure A.17a Time History for Center Conductor Transverse Swing for Record NOS

N(}7.SfllO 01/ a a. SI. , -tV OUL rur iMTE ai/t»v7 ana MMLR ia.io J0-« ia/« COT INST. MM - a.« OEB TOC - 1.070 HIN 8.50 OEB INT. HFR 3 12.80 OEB TDC a 2.951 IIH INST sn KV a 2. IS OEB tNBT. MN • -.a OBB TDC - 7. on NIN IRT STO OEV • I.a OEB INT. NIN - a. as DEB TDC • 1-73 NIN MM PTVIRT > 10 TIK HISTORT PK l.OOO SEDSO (NlfcXTW. flVlWGES

a

i''..>^,^u^Cl^\^.,..^^y^/liy^^.^^>,./. « • 3 N-l

-I ' r "' T T 12 -" r I 10 2 a a TIME (MINUTES)

Figure A.17b Time History for Center Conductor Transverse Swing for Record N07 315

NOS.SfllO oi/siye Bi.a.3X aiNO WMJE HO. 10 JM» IB^ CBIT (981. *T OIR. rUM ORTE 0I/12^W7 IMSl. MM > I7.a ORB TOC • l.oai HIN mm It.W CRB INT. mm a ts.32 OEG TDC a I.SB1 NIN INST STB OEV a I.SO KG INST. MIN • B.OI OCO TDC • }0.ira HIN IRT STD OEV - i.

N* S

N- 9

cr

T 10 12 TIME (MINUTES)

Figure A.ISa Time History for Center Conductor Transverse Swing for Record NOS

NlS.SfllO aviaaa aLia.sa I8MLC HB. IB JD-O IV\ COIT OMI. •** OIR. rur ONTC ouii/mr ICPR l.flS OEB INST. MM - 2.a tB» TOC • 11.as im INST STO KV a 0.29 OEB INT. mm a 2.7a OEB TOC a 12.000 IIN INT STD CEV • O.a SB INBT. Mm • 1.12 OEB TOC • 7.081 NIN MM PTVINT • 10 INT. NIN • i.at KG TOC • T.S81 IIN TIK HISTORT PK 1.000 xi3*o (Nmm. HVEinCEs

a • • 10 TIMErzmmJTE. )

Figure A.18b Time History for Center Conductor Transverse Swing for Record N16 316 NU5.5(}05 \2/is/tj 11.10.28, ITWIN GWE «. S JD-B U/H SC 2 MIIN inxiR) PtOT OBTE OlATt/m IWT. mx - -5.90 NPR riK = 5.1*73 HCN -7.03 «»» INT. NNI = -1.15 nPN ritiE : S.UW nCN IMST »T0 067 : 0.2t ••H IM3T. HIN • -7 a HTN riNC « a. tm HCN INT aro OEV • Q.2J nm IMT. niH 3 -7.73 mi riK = a 117 NtN NUN PTS/INT = JO TtK HISTKT PK 1.000 SECOril INTBWR flVBWGES TIME (MINUTES)

10 12

cr a.

T-

Figure A. 19a Time History for Stress in Southeast Main Leg for Record NOS

NG7. SGQ5 oi/a/Ba ia.a.si STMDH OBZ m. 9 JD-O 18^ X 2 Mim CFMIM.! rur ONTE 01.i7/«7 INST. MM - l«.a ITN TOC • I.OMI NIN mm LOB vn INT. mm a 19.27 ITN TIK a 1.700 NIN IHSr STl KV a 2.S2 rm INST. MIN • -I.a ITN Tire • I.M] NIN INT STO OCV > 2.>i9 tm INT. NIN • -1.113 m* TDC - •.asa NIN MM PTVINT • a TIK HISTORT PK 1.000 SECOK) INTOnRL flVERKZS an

cr ^^^^^fc=:: CD

1^ —I 10 12 TIME (MINUTES)

Figure A.19b Time History for Stress in Southeast Main Leg for Record NO? 317 N08. SCOS oi/9t/R3 II.a. 11 sTiaa OBZ m. s JD-B W\ ae 2 WIN cf«tf«j rur one 01/W/B7 INST. MM - 21. a im TOC • 1.007 NIN la.os M« INT. NPR a 20.19 irn TOC a 1.050 NIN INST STO OEV 2.21 MH INBT. r«N - 7.82 ITN Tire • i.asT NIN IRT STD CEV 2. IB rrm INT. HIN - a.S3 if>n TDC • l.aB7 NIN MM PTVIRT a TIK HISTORT PK 1.000 SECSO INTEJnPl flVOOCES in

OC

H*i i y^KvL^^AAi^in/ W H- 3

T "1 10 12 TIME (MINUTES)

Figure A.20a Time History for Stress in Southeast Main Leg for Record NOS

N16.SG05 aa/a/n S. 19.90. snna oMe m. s JD-» iv^ a 2 MHH OMIM.! rur ant II1/D7/V7 INST. MM • 2.a ir« TOC • i.ia NIN mm l.ua INT. NMI a 2.«7 im TOC a 1.331 IIN IWSf STl KV a 0.37 >m irer. MIN • 0.37 (TN TOC • I.3ZZ NtN IRT STD CEV " o.a rrm INT. NIN • o-iB im TOC - i.sa NIN MM PTVINT > a SECOK) (HTEmPl flVEHCES

CC

CO cn UJ Q£ I— cn

a a I TIME (MINUTES)

Figure A.20b Time History for Stress in Southeast Main Leg for Record NIS 318

NOS.SCJOB 12/18/Ot a.10.30. STNNBN GHZ lO. B JO-6 IV^ SC 9 mO IRUNLI rur ome Ol/tr/87 INST. MM • 0.70 im TOC - 0.031 NIN mm O.SI M^ INT. mm a 0.72 wn TOC a 1.733 NIN INST STO KV 0.07 iro INST. MIN > 0.27 im TOC • 0.819 NIN INT STO OEV O.ON M^ INT. IM > a.>ic im TOC • 1.083 NIN MM PTVINT a TIK HISTORT PK 1.000 SECOK) INTElWfa. flVEBRES

CO "•

I— CO "!-

—r 12 10 TIME (MINUTES)

Figure A. 21a Time History for Stress in Southeast Diagonal Leg for Record NOS

NG7. SG06 ai/io/B3 ta.iM.si. STirniH GHce a. s jo-c i%/% z 3 IRXOft.) nor OBTC 01/07/87 INST MM • I.a TOC • 1.091 NIN mm -.Hi M^ IMT. NPR a 0.73 NPf) TIfC a s.asa IIN IHSr STO OEV a 0.M ITA INST MIN • -2.II7 Ttre • z.am NtN IIT 3T0 oev • 0.«9 NPN INT. HIN • -I.7J HP« Tcrc • 1.987 UN NUM PTVINT • a TIK HISTORT FK t.OOO SECOH} (NTERtn. RVEKilGES

CO

ft T T T I a a I 10 12 TIME (MINUTES)

Figure A.21b Time History for Stress in Southeast Diagonal Leg for Record NO? 319

NG8. SGOB o./3.« II.a. IX STODN ORK m. B jo-m la/^ SE 9 OIN inaii.1 PUT DRTC 01/07/D7 INST. MM - 1.89 im Tt>C - 1.3M NtN mm 0.51 tm INT. m a 1.23 ITB TI>C a J. 950 NIN INST STO OEV a 0.38 mt INBT. rRN - -.00 irw TOC - 1.131 NIN IRT STD OEV - 0.23 trm INT. NIN - -.08 m TOC - 0.817 NIN MM PTVIRT • 20 TIK HISTKT FK 1.000 KCOK) INTDJWL flVEBBES

cn

TIME (MINUTES)

Figure A. 22a Time History for Stress in Southeast Diagonal Leg for Record NOS

N16.SGQ6 oa/ia/Ba is.i9.sa smm OCR NB. a JD-O W% X 9 OIN incoi.) rur ONTE 0I/D7/87 INST. MM • 2.a icn TOC • LOB? NIN mm t.a m INT. mm a 2. IS im TOE a 1.700 NIH INST STO OEV a O.Oa PTN IIBT. NIN • i.n m Ttrc • 1.1102 NtN IRT STD OEV • a.oB WW INT. NIN • 1.7S im TOC • •.SOD NIN MM PTVIRT • a TIK HISTORT PK t.OOO SECOK) (RTCRWa. RVCRffiES

cn --

T T T 1^ a a I 10 12 TIME (MINUTES)

Figure A.22b Time History for Stress in Southeast Diagonal Leg for Record N16 320

NG5. SGI 1 ia/i«Ai a. 10.3a NEE m. 11 JO-6 ISft m 2 MIIN laiMJ ruT ome 01/O7/W7 INST. MM a. a TOC • 002 HIN 8.85 M^ INT. mm 9.52 tm TOC a 117 NIN INST STO OEV 0.31 M>« tMST. MIN 7. a Tire • •Ml NtN IRT STO CEV 0.27 »WI INT. HIN 7 TOC - vol NIN MM PTVIRT a SEC90 (NTEXWL RVERICES

cr

cn (n UJ

cn -

a a I 12 TIME (MINUTES)

Figure A.23a Time History for Stress in Northwest Main Leg for Record NOS

NG7.SGI 1 ai/M/n ia.aLSi. 11 JD-O mrt m 2 WIN imiiaj rur one 0t/D7/B7 INST. MM - 3.37 WW TOC • i.Ml NW ICPO - -I.a tm INT. IBM a H.M WH TOC a 9.850 NIN IIOT STO KV a 2.S3 tm INST. MIN - -12.87 ITW TOC - 2,913 NIN IHT STO CCV - 2-79 M^ INT. NIN - -11.90 ITN TDC- J.M9 NIN MM PTVIRT - a TIK HISTORT FK 1.000 SECOK) (NICXWI. RTEWtZS '^Vy-Wy^^' cn

cn B-

T T T —T -1 a • * 10 12 TIME (MINUTES)

in Northwest Figure A.23b Time History for Stress Main Leg for Record NO? 321 N08.SG11 Ot^/R 01.38.32. STRRIN GMZ ML II JXi is/a Ml 2 aiH (laiiiL) lui ORIS - oiAn/m tIBT. KK 3 -1.00 »a riK a 1.85] NOl mm a -iii.7i mi INT. NM = -B.aa tm roc = I.8B7 HOI INST STD CRV 3 2.11 tm IWT. MN- -ZS.SS MTI rite- 1.037 HOI INT STD OEV - 2.n Mm INT. NIH 3 -2U58 KN riK a I.OSD NOl MJNPTS/0(T a 20 TIK HISTKT FK l.OOO 3a2HI INTERTPL RWBWCE3 TIME (MINUTES)

Time History for Stress Northwest Main Leg for Record NOS

N16.SG11 09/0/09 s.i9.sa sraoM OBR a. ii jB-e m/% a 2 MIIN imiMJ rur tMIB 0I/D7/V7 INST. MB - I.a im TOC • t.32t NIH KPB a.«l M^ INT. MM a 1.58 im TOC = 1.531 NtN INST 3T0 KV a o.«9 tm INST. MIN - -.80 I^K TOC • •.IM NIN IHT STO OEV • o.a M^ INT. NIN - -.70 tn TOC • 1.339 NIN MM PTVIRT • a TIK HISTORT PK 1.000 SECOK) (HTOTRa. flVOOIZS

GC

M • 3

M- 9 cn V\/'\^ (n UJ

cn

-• r r 2 12 10 TIME (MINUTES)

Figure A.24b Time History for Stress in Northwest Main Leg for Record N16 322

NOS.SGI2 12/iaai a. 10.20. 12 JO-C B/a Ml 9 OIN CTMin.1 nor ORTC 01/TX7/B7 INST. MM • o.a icA TOC • i.aoi NIN KM 0.51 M^ INT. mm 0.81 iro TOC a 1.917 NIN IRSr STO OEV a o.oa t^^^ INST. MIN • 0.37 tm TOC - 0.145 NtN INT STD OEV « 0.09 *N INT. N]N • 0.>tO im TDC - 7.9B7 NIN MM PTVIHT • 20 TIK HISTORT FK l.OOO SECOM) (HTEmPL nVERMZS

cr

cn " cn UJ t— cn *-|

1^ I a a I 10 12 TIME (MINUTES)

Figure A.2Sa Time History for Stress in Northwest Diagonal Leg for Record NOS

N07.SG12 ai/a/B3 aoLsi. a jo-B ia/*i a 9 OIN OMiia.i rur one tn/ry/BT INST. Ml • 0.07 tm TOC • 7.373 NIN -1.10 M^ INT. MM a 0.10 ITN TOC - 2.381 NIN INST STB OEV a INBT. rRI • -3.a m TOC • 2.712 NIN IRT STD OEV • 0.59 tm INT. H)N - -2.S9 NPN TOC • 1.717 NIN MM PTVIHT • SECOK) (HTOnn. flVEKNGES a

8 I 13 TIME (MINUTES)

Figure A.25b Time History for Stress in Northwest Diagonal Leg for Record N07 323 NOS.SGI2 oi/ii/n a.38.32. STRMN GRGE lO. 12 JO-6 IB^ Ml 3 OIN lAKIR.) Rjn ONIB oi/rn/a liBT. Kl 3 aa? KB TIK = J.922 NOl KM -.a tm INT. NM = -.« im TIIM r 1.887 NOt INBT rrn oev o.u trt IWT. WN - -J.00 tm Titm. • 0.324 NM INT STO KV o.a M^ INT. HIH 3 -l.m mt riK a 0.333 NOI MM PTVOTT 20 TIK HISTKT FK l.OOO SECONI INIBnia. RVB3CE3 TIME (MINUTES)

a: Q-

cn cn UJ I— cn

Figure A.26a Time History for Stress in Northwest Diagonal Leg for Record NOS

NI6.SG12 aa/xajmi s.ia.ia 1 OMR a. 12 JD-O m/% a 9 om (TMOtJ PUT one m/VF/VT INST. MM - a.NfT trm Ttrc - 1.9B HIN MPR 0.21 M^ INT. HFR a a.a7 iro TOC a 9.117 IIN IHSr STO KV a 0.12 WN HOT. r«N • -.22 trm TOC " 1.312 NIH IRT STO ORV • 0.11 tm INT. NIN • -.13 im TDC " 1.517 NIN MM PTVIRT > a TIK HISTKT PK 1.000 SECOM) (NTEXtn. nvCMCES

a a TTMF (MINUTES)

Figure A.26b Time History for Stress in Northwest Diagonal Leg for Record N16 APPENDIX B AUTOCORRELATION FUNCTIONS

AUTOCORBEUnorf YAUTIS Of NOT.WSOO OMiODiALAimFasT oargggms soRigsroR roo uca SAiMtJMORAIg - tOSPB

•.«

*.» ly^^v'v

Figure B.la Autocorrelation Functions of Original €ind First Differenced Series of WSOS for Record N07

AUTOCORSBLATIOrf VALOKS OF N16.WSM ORiaouLA/m rasr Dovwuritcg sw/ugsrog too ucs SAMrUMCMAIgm IOSPS

Figure B.lb Autocorrelation Functions of Original and First Differenced Series of WSOS for Record N16 324 325 iUTOCOBSZU'nON VALUES or N07.LC03 OMIOMALSgaigSrOlttaOLdGS URSTDiFrgRgjngsgiugsng taouea SAMniMCXAam tOSFS

Figure B.2a Autocorrelation Functions of Original and First Differenced Series of LCOS for Record N07

AUTOCOBRIXAnON VALUES OT N07.LC04 oanmAtsgRosroRtaoucs raSTD/FTggggcgsgiugsroM taoues SAMFtUrCMAJg - fOSPB

Figure B.2b Autocorrelation Functions of Original and First Differenced Series of LC04 for Record N07 326 AUTOCORRELAnON VALUES OF NOT.LCOft - ^ojtfcP^t sggnrsFOR tao uca fnnTDirrgKgtrcg sgiugs /or laouea SAimjMCJUlgm tOSPB ^^

Figure B.3a Fir^?T?i^^'°'' !'^"^^i°^s °f Original and J-irst Differenced Series of LCOS for Record N07

AUTOCOBBZLA'nON VALUES Or Nl 9.10)3 QgiODfAL sggas mt tao LACS nRSTOimgMM\j sgngg FOR taouea SAMFUMOHAn' lO. t-*i

^^^l^lt^^

Figure B.Sb Autocorrelation Functions of Original and First Differenced Series of LC03 for Record N16 327 AUTOCORSEUnON VALUES OF N1«.LC04 OajODIALSgROaFOR taoUGS fjRSTOiFrgggjrcgsggigsnm taouea SAMrUMCRAJg^ IOSPS *^i

Figure B.4a Autocorrelation Functions of Original and First Differenced Series of LC04 for Record N16

AvrocoBBnAnoN VALUES or Ni«.LCOft oamNAL smtagaroH tao ucs nafTDurgRgiK*ssmasnm taoues SjOtFUMOMAIg ^ IOSPS

*.•

-"i • II I

Figure B.4b Autocorrelation Functions of Original and First Differenced Series of LCOS for Record N16 328 AUTDCORRBIATION VALUES OP PfOT.SGM OMIOOUL AND FIRST DOrgggHCg SgROB FOg ISO UCS SAMPtme 2A7g m AO SPS

Figure B.Sa Autocorrelation Functions of Original and First Differenced Series of SGOS for Record N07

AirrOCOSBBLAnON VALUES or NVT.SGI 1 OaiODiAL Aim FIRST DOTggginS SRIUgS FOR ISO LAGS SAMFtlMe RATg •ao SPS

Figure B.Sb Autocorrelation Functions of Original and First Differenced Series of SGll for Record N07 329 AUTOOOBBELATION VALUES OP N07.SGO« SMMOIAL AND FIRST OargMgUOiSgRaSFIUI t SO UCS SAMruMcaAigmaospe

Figure B.6a Autocorrelation Functions of Original and First Differenced Series of SG06 for Record N07

AUTOCOBBBLATION VALUES OP n97.SG12 ORiaoiAL AND FIRST Dorgagya sgRiia FOR tsoLAca SAMFUMORLrg^MSPS

Figure B.6b Autocorrelation Functions of Original and First Differenced Series of SG12 for Record N07 330 AUTOCOBBBLATION VALUES OP m«.SG06 OMIOOUL AND FIRST Dorgggya sgargg FOR ISO UCS SAUniMO RATg ' Mt SPS

k.*'

.«.a

-4.*

— > »••' Mi in

Figure B.7a Autocorrelation Functions of Original and First Differenced Series of SGOS for Record N16

AUTOCOBBELATION VALUES OP I7M.SG11 OMIGOULAND riRST MrmgHcg sRima roR tso ucs SAUrUNG RAJg m ao SPS

4.* •W^W^VV'^^^^^^''^

Figure B.7b Autocorrelation Functions of Original and First Differenced Series of SGll for Record N16 331 AUTOCOSBBLAnON VALUES OF N18.SG06 OMIOOUL AND FIRST DOrgggiKg SgRfgS TOR ISO UCS SAMHJMGRAJg - AO SPS

Figure B.Sa Autocorrelation Functions of Original and First Differenced Series of SGOS for Record N16

AUTOOORBBLATIDN VALUES OP rfl«.SG12 ORlOaULAND FIRST tXFTgggtra SSRIXSFOR tSO UCS SAMFUMO RAJg • M SPS

Figure B.Sb Autocorrelation Functions of Original and First Differenced Series of SG12 for Record NIS APPENDIX C CROSS CORRELATION FUNCTIONS

a?OSS CORREUTION SETATEN NOS.WSOS .\ND NOS.SGH

Figure C.la Cross Correlation Function of WSOS and SGll for Record NOS

CROSS CORREUnON BBTWEBX IRH.irSOOAND ttOO.SCIM gAMPUNORATgm to SPS

Figure C.lb Cross Correlation Function of WSOS and SG12 for Record NOS

332 333 CROSS CORRSUTION BRTEEIf MOf.WSOS AND MOV.SGOS SAMHJIMJUTE' tO SPS

\m-

a

Figure C.2a Cross Correlation Function of WSOS and SGOS for Record N07

CROSS CORREUTION BBTTESN tan. wsao M*D ROV-SGI I aAMPUMORATt'tOSPg

Figure C.2b Cross Correlation Function of WSOS and SGll for Record N07 334 CROSS CORRSUTION BCTinN M»T. trsooAND ttof^seoo SAMfWtaRATES tOSPS Kl

'I I' 11

Figure C.3a Cross Correlation Function of WSOS and SGOS for Record N07

CSOSS CORSSUnON BETVEBrr mrf.trsooANO iwt.se*s aAMPUMCJUTM m to SPS

•,1

At

Figure C.3b Cross Correlation Function of WSOS and SG12 for Record N07 335 CROSS CORRSUTION BmnsN int.waooAND ino.seoo SAitnafORATE' to SP9

Figure C.4a Cross Correlation Function of WSOS and SGCS for Record N16

C3tOSS CORRSUTION BBTWESN no.waeoANDgio.seom aAMFURORATE ' tO SPS

kia kM ita i»»

Figure C.4b Cross Correlation Function of WSOS and SG06 for Record N16 336 CftOSS CORRSUTION BKTIESN ROSJ^OOfrOULiAMB Ros.sei 1 aAMPUHORATE'tOSPS

%i

AM

A.f

Figure C.Sa Cross Correlation Function of Total Load Values From West Conductor and SGll for Record NOS

CROSS CORRSUnON BETWEEN MOM.ie0¥T0r.a}AMD )IO0.SG*X SAMPUNORAfS' tOSPS

Figure C.Sb Cross Correlation Function of Total Load Values From West Conductor and SGI2 for Record NOS CROSS CORBSUnON BRWESN 337 MOOJXOAfTOnL) \AMD ROO.SG* 1 SAMPUNORATEs tOSPS

•.37

|a.M kiL. • •""

xm

'T*.P««»T«.««'V«««»T.'««v<'T.^.««TV«>«T««>*

Figure C.6a Cross Correlation Function of Total Load Values From East Conductor and SGll for Record NOS

CROSS CORBSUnON BETVESN gO0.UC04fT0tAL) AMD ROO.SGtX aAMPURORATE' tOSPS

*.at

e %m

%m ca am

'r • •

Figure C.6b Cross Correlation Function of Total Load Values From East Conductor and SO 12 for Record NOS 338 CROSS CORBSUnON BBTWESN iMcxcssnezu; ARB Roo.sGt i SAMPUMRAIE ' tO SPS

Figure C.7a Cross Correlation Function of Total Load Values From Center Conductor and SGll for Record NOS

CROSS CORRSUTION BRWESN iLcoorrotu) AND Hoojxtx SAMnOMRATE' tOSPS

Figure C.7b Cross Correlation Function of Total Load Values From Center Conductor and SG12 for Record NOS 339 (aoSS CORRSUTION BBTWESN RgTJ£Oa(TOnL) AMD ROf.SGOO EAMPUMORATE - tO SPS

e '* t

! 1-

A9

Figure C.Sa Cross Correlation Function of Total Load Values From West Conductor and SGOS for Record N07

CltOSS CORRSUTION BBTWESN '.leoarronLiAMD mv.setx SAMPURORATE ' tO SPS

ct

T»»"»T"" 11 III '^.^rmrm^rm

Figure C.Sb Cross Correlation Function of Total Load Values From West Conductor emd SG12 for Record N07 340 CaOSS CORRSUTION BBTWESN M0ir.La4ftOtkL)AMD HOf.SOOO EAMnatORATE 'IOSPS

Figure C.9a Cross Correlation Function of Total Load Values From East Conductor and SGOS for Record N07

CROSS CORBSUnON BBTWESN Ror.Laa(Totu,) AMD umr.sooo aAMPUHORATE ' to SP9

I

IA*

Figure C.9b Cross Correlation Function of Total Load Values From Center Conductor and SGOS for Record N07 341 CROSS CORRSUTION BBTWESN gl0.W00fTOtAL) AMD R1t.SCag SAMPUMORATE > tO SPS

Figure C.10a Cross Correlation Function of Total Load Values From West Conductor and SGOS for Record N16

CROSS CORRSUTION BBTWESN gto.Leoonrtnx.) AMD 0to.set i SAMPtOfO RATE'IOSPS

Figure C.lOb Cross Correlation Function of Total Load Values From West Conductor and SGll for Record N16 342 OttSS CORRSUnON BBTWESN jrf*££iMr»£t£; AMD t/to^seoo SAMPIBURATE 'IOSPS

it "»•

e •"• i CM ' ca k &.n I *• I ^*

Figure C.11a Cross Correlation Function of Total Load Values From Center Conductor and SGOS for Record N16

CROSS 00RRSUT30N BBTWESN MIOJCOAfJOttLi AMD M10.i aAMPUNaRATE'tOSPg

a.m &a &i7 &a am CM &a &a

ca

Figure C.lib Cross Correlation Function of Total Load Values From East Conductor and SGOS for Record N16 343 CROSS CORRSUTION BBTWESN nog tcmtaoNK.)jMBMosjeoo aAMnOMRATE'tO^S

Figure C.12a Cross Correlation Function of Longitudinal Load Values From West Conductor and SGOS for Record NOS

CBOSS CORRSUTION BETWEEN ma,icotaaNe,)ARa )mo.3eoo SAMPiaCRATE ' 10 SPS

u

I

Figure C.12b Cross Correlation Function of Longitudinal Load Values From East Conductor and SGOS for Record NOS 344 CROSS CORRSUTION BBTWON m7j£040MNG.)AMM Mor.3eoo SAUPUMRATE'IOSPS

Figure C.13a Cress Correlation Function of Longitudinal Load Values From East Conductor and SGOS for Record N07

ObOSS CORRSUTION BBTWESN M0rrJ£O0(L0NG.) AMD MOT.SeOO OLMnOfORAtE ' lO SPS

Figure C.13b Cross Correlation Function of Longitudinal Load Values From West Conductor and SGOS for Record N07 345 CROSS CORRSUTION BBTWESN M07J£OO(LONG.) AMD MWr.SGOO SAMnaWRATE 'IOSPS

Figure C.14a Cross Correlation Function of Longitudinal Load Values From West Conductor and SG06 for Record N07

CBOSS CORRSUTION BBTWESN jiRRT JO»«ffawR j AMD Mrr.seoo aAMPUNORATE 'IOSPS xa

&a

&a

Aa

Figure C.14b Cross Correlation Function of Longitudinal Load Values From East Conductor and SG06 for Record N07 346 CROSS CORRSUTION BBTWON mTJ£OO(L0Na) AMD MOTJSGIX aAMPUHORATE 'IOSPS

Figure C.15a Cross Correlation Function of Longitudinal Load Values From West Conductor and SGI2 for Record N07

CROSS CORRSUTION BBTWESN Mafrj£O4fL0Ne.) AND )for.seix SAMPUNORATE 'IOSPS t,a a.Ni

AV -AM

Figure C.ISb Cross Correlation Function of Longitudinal Load Values From East Conductor and SG12 for Record N07 347 CROSS CORRSUTION BBTWESN WOO LCOOfTMAMS h)AMD RtS-JKOO SAMPUtaRATE' IOSPS xs XM %m

t,9

} J*

' 0.0 I- &a I n,m S xa XB xm

Figure C.16a Cross Correlation Function of Trainsverse Load Values From Center Conductor and SGOS for Record NOS

CROSS COflSSUTlON BETWEEN RooJcoofTRAMarpAia ttoo.sei t SAMPIOMRATE ' lO SPS

Atm

-«kU Ata A» -*a \Am i-ca ' Ata -•.a I

Figure C.16b Cross Correlation Function of Transverse Load Values From Center Conductor and S^JII for Record NOS 348 CROSS CORRSUnON BBTWESN I'^'J'CO^fnUMS.iAMO NOOJX11 SAMHOORATE • to SPS

Ll

Figure C.17a Cross Correlation Function of Transverse Load Values From East Conductor and SGll for Record NOS

CROSS CORRSUTION BBTWESN RooAeoom\AMa.iAMa MOOSGH aAMPUNORATE ' 10 SPS

AT

-«^i

Figure C.17b Cross Correlation Function of Transverse Load Values From Center Conductor and SGll for Record NOS 349 CROSS CORRSUTION BBTfESN RorjcoornuMS.) AND m7.scoa SAMPUMORATE 'IOSPS

Figure C.18a Cross Correlation Function of Trainsverse Load Values From West Conductor and SGOS for Record N07

CROSS CORBSUnON BBTWESN N0rjjooocnuMa.i AMB Nor.sci i aAMPUHORATE'IOSPS k*4

-*»

-*.«

Figure C.ISb Cross Correlation Function of Transverse Load Values From West Conductor and SGll for Record N07 350 CROSS comsunoN BBTWEBN RSTJ^OOCTRAMS.) AMD NB7.SGO0 aAMPUMROE 'IOSPS

Figure C.19a Cross Correlation Function of Trainsverse Load Values From West Conductor and SGOS for Record N07

CROSS CORRSUTION BBTWESN mrrjjeoociRAMa.i AND mr.seix aAMPUNORATE' tOSPS

Figure C.19b Cross Correlation Function of Transverse Load Values From West Conductor and SG12 for Record N07 351 CROSS CORRSUTION BETWEEN R07jjcoocrRANa.)AMD m7.seoo aAMPUHORATE 'IOSPS

XJ

x%

Figure C.20a Cross Correlation Function of Transverse Load Values From Center Conductor and SGOS for Record N07

CSOSS CORRSUTION BBTWESN NvrjjaHcnuMS.) AMD Marascos aAMPLBfORATE' lOSPS

C7

xt

• •I I I

Figure C.20b Cross Correlation Function of Transverse Load Values From East Conductor and SGOS for Record N07 352 CROSS CORRSUnON BBTWESN mTJ£00(TRANa.iAMD NOT.SeOO aAMPUHORATE 'IOSPS

•Al

•*.M'

Figure C.21a Cross Correlation Function of Trainsverse Load Values From Center Conductor aind SGOS for Record N07

CROSS CORRSUTION BBTWESN NorjcoofTRAMa.) AND mT.acix SAMPLBMRATE ' 10 SPS

Figure C.21b Cross Correlation Function of Transverse Load Values From Center Conductor and SG12 for Record N07 353 CROSS COKRSUnON BBTWESN NtOXCOOfTRXMS.) AMD NtOJKOO aAMPUHORATE' IOSPS

Xt-

x%

XI

Figure C.22a Cross Correlation Function of Trsuisverse Load Values From Center Conductor and SGOS for Record N16

CROSS CORRSUTION BBTWESN NisJcoornuMS.} AMD MIO^SGOO aAMPUHORATE 'IOSPS

Figure C.22b Cross Correlation Function of Transverse Load Values From Center Conductor and SG06 for Record N16 354 CROSS CORRSUnON BBTWESN H10JiC00rnUMS.)AMDNHLSCtt aAMPUHORATE 'IOSPS

Figure C.23a Cross Correlation Function of Transverse Load Values From Center Conductor and SGll for Record N16

CROSS CORRSUTION BBTWESN mOMCOOtTRANS.) AMD NtO^GIX aAMPUHORATE' IOSPS

Figure C.23b Cross Correlation Function of Transverse Load Values From Center Conductor and SG12 for Record N16 APPENDIX D POWER SPECTRA

a Pt»CR SPECTWJH OF «7.)6a5 a (TIKET SPECTRRL HlhCONI d a a 8

Figure D.la Power Spectrum of Wind Speed at 34 7 m for Record N07

po»cR sporrRui OF NIS-HSOB (TUKET SPEaRRL HlHKMl

^" f TTTT* 0.001 0.01 to.o FREQUENCY (HERTZ)

Figure D.lb Power Spectrum of Wind Speed at 34.7 m for Record N16 355 356 ™»€R SPECTWJI OF ND5.LCQ3 00 0 d ITOTFL) ^ § •-o^ «- (n (O 3 - U. :» 1 UJ § , 5 -^^ 1 1 2.00 0 flL V Q£ »— UJ § Q_ ^-

Figure D.2a Power Spectrum of Total Load Values F West Conductor for Record NOS rem

POICR SPCETRtM OF WS-LOB LONCmjOINrL OIRCCnCN

o ^^ to V. m

UJ

a.

Figure D.2b Power Spectrum of Longitudinal Load Values From West Conductor for Record NOS 357

3 POICR SPECTW* OF NDS.LCIII (Torn.)

o S • 3 a aj a 0^ 1— da " UJ 8 a. •^ _

Figure D.Sa Power Spectrum of Total Load Values From East Conductor for Record NOS

pvo spcnmjH OF WSLLCOI UONOmOINHL OIRECnON

^ § o d (O V. (O 8 u. i UJ

§ ai I u 8 UJ o S5 -

I I I II ll I I I I 11 ll ^ •^MX 0.001 0.01 0.1 1.0 10.0 FREQUENCY (HERTZ)

Figure D.Sb Power Spectrum of Longitudinal Load Values From East Conductor for Record NOS 358 8 POCR 9>CCT1tlM OF WB.inS I*. d (TOTRL) S? 3- o (O (O M 8 I 9 UJ d

i 0.001 0.01 FREQUENCY (HERTZ)

Figure D.4a Power Spectrum of Total Load Values From Center Conductor for Record NOS

RKR spcmnft OF ros.ijCQS § LOKXTlOINfl. OIRELnON

o

I UJ

ai 0^ CJ Ui 0.

I I I I I 1111f" ff I > i 11 n '0.001 0.01 0.1 1.0 10.0 FREQUENCY (HERTZ)

Figure D.4b Power Spectrum of Longitudinal Load Values From Center Conductor for Record NOS 359 3 P»CR SPECTRIH OF W7.LCa3 TOTAL

C3

UJ

^ 8 ai 2i oc CJ Ui a.

< I I I I lll| T I I I Mill "^^-vAAr-iw.. TT TT^ 0.001 0.01 0.1 1.0 10.0 FREQUENCY (HERTZ)

Figure D.Sa Power Spectrum of Total Load Values From West Conductor for Record N07

8 POICR SPBCTRtJH OF N07.Laa TRRNSVEKSE OIREaiGN

0.001 0.01 0.1 1.0 10.0 FREQUENCY (HERTZ)

Figure D.Sb Power Spectrum of Transverse Load Values From West Conductor for Record N07 360

8 POICR SPBCTRm OF ND7.U:Q3 a LONMTIDINR. OIRECTICN

C3 ., o S CD ^

TTTT I I 111 n ^ I llll llf ^"•^a^T 'I IIIII 0.001 0.01 0.1 1.0 10.0 FREQUENCY (HERTZ)

Figure D.6a Power Spectrum of Longitudinal Load Values From West Conductor for Record N07

POICR SPOnRlJH OF «7.LCW TOTTBL (M

a to o to \ • ai oc a. to

I I I llll ' 1-^ „„^AJ1 Uu ll 1.0 10.0 '0.001 0.01 0.1 FREQUENCY (HERTZ)

Figure D.6b Power Spectrum of Total Load Values From East Conductor for Record N07 361 3 POICR SPECTMJM OF MD7.iX0H TRRNSVEKSE DIRECTIOH

C3 to O to (O m

UJ I

oc h- tJ UJ a. to o 3 I I I I 11 ll I I SOlf >iy 0.001 0.01 0.1 1.0 FREQUENCY (HERTZ)

Figure D.7a Power Spectrum of Transverse Load Values From East Conductor for Record N07

8 P»»CR SPECTRUM OF NOT.LOTI

1 LOrCITUIINfl. DIRECTION 9. 0

C3 « s §

(O ^ i J 1 ri~ 1 VALU E 2.00 0 1 1.00 0

SPECTRA L j

00 0 . h °0. ni 0.01 0.1 1.0 10.0 FREQUENCY (HERTZ)

Figure D.7b Power Spectrum of Longitudinal Load Values From East Conductor for Record N07 362 8 P9€.K a»ECTRU1 OF fC7.LC0S a TOTAL

a (O o to (O

UJ §

ai oc

0. to o a I I ' ' llll i'i'% M-frPtiHi »• U 0.001 0.01 0.1 1.0 10.0 FREQUENCY (HERTZ)

Figure D.Sa Power Spectrum of Total Load Values From Center Conductor for Record N07

PO^R SPECTRIN OF NOT.LCOB 8 TRRNSVERSE OIREaiON

to M C3 d to (O 8 m ^ -I I UJ 8

8

^•^ » 'OLOOl 1.0 FREQUENCY (HERTZ)

Figure D Sb Power Spectrum of Transverse Load Values From Center Conductor for Record N07 363

8 PBICR SPECTRIH OF «7.|JC0S a LOMHTUlINn. OIRECTICN a to O

m

I UJ m a! 5» ai , 0^ 8 ^^ a CJ - a. to JL 0.001 0.01 0.1 1.0 10.0 FREQUENCY (HERTZ)

Figure D.9a Power Spectrum of Longitudinal Load Values From Center Conductor for Record N07

POICR SPEORUN OF N08.IX0a 8 rOTHL od

^ §

^O4 d" (O (O § U. ^ 1 UJ 5 ^ d ai a"i. i^ (^ H- [d § ^ -

1 r I i I I ii| I I llll) * iVirin 1.00 0 1.0 10.0 0. 001 0.01 0.1 FREQUENCY (HERTZ)

Figure D.9b Power Spectrum of Total Load Values From West Conductor for Record NOS 364 3 POICR sPGcrmji OF rcsLLOB a LONOmOINfL OIRCCnCN « o 1

s? 7.0 0

SI G § >^ a cant u. 9 1 n 00 0 UJ 3 ^ c—r1 >• 1 •> a! 9 K- 0 ^ CJ M §. SP E

llll) rrrj- I 11llj J. llll) 0.001 0.01 0.1 1.0 10.0 FREQUENCY (HERTZ)

Figure D.lOa Power Spectrum of Longitudinal Load Values From West Conductor for Record NOS

POICR 3>EnRlM OF NOOLimN rOTHL

^

I UJ a! c* ai oc a. to

§ I I I imr ^ -mrry I 1.0 '0.001 0.01 0.f lO.O FREQUENCY (HERTZ)

Figure D.lOb Power Spectrum of Total Load Values From East Conductor for Record NOS 365 POICR SPECTRIN OF NltLCOS TOTBL

'0.001 1.0 FREQUENCY (HERTZ)

Figure D. 11a Power Spectrum of Total Load Values From West Conductor for Record N16

POICR SPECTRtM OF N16.LCIS TRRNSVEKSE DIRECTION

0.001 10.0 FREQUENCY (HERTZ)

Figure D.lib Power Spectrum of Transverse Load Value; From West Conductor for Record N16 366 3 PdCR SPECTRIN OF NlfcLCOa « LOHMTlfllMflL OIRECTICN d

a d1 CO CD 8 u. o I UJ § 3 ° * 8 d Si Ui 2 to °

J V A-^rrtTf"*«oV 0.001 0.01 0.1 1.0 10.0 FREQUENCY (HERTZ)

Figure D. 12a Power Spectrum of Longitudinal Load Valu From West Conductor for Record N16 es

8 POICR SPECTRIN OF raSLLCGH TOTRL

o 8 in CO .i 8

UJ

a aJ ^ 8 CJ = to

I iiiiin I I iiiiiij it 0.01 0.1 0.001 FREQUENCY (HERTZ)

Figure D.12b Power Spectrum of Total Load Values From East Conductor for Record N16 367 3 P»CR SPEETRIH OF N16LLCW ^•••^SVERSE DIRECTION

o CO cn m

' I i^O^'Mlli i>^ 0.001 0.01 0.1 1.0 10.0 FREQUENCY (HERTZ)

Figure D.13a Power Spectrum of Transverse Load Values From East Conductor for Record N16

POWR SPECTRIN OF N16.LC(M LONOmJOIML DIRECTION

o .70 0 i _ to a 60 0 SI G 1 \ a tmo u. S 1 o UJ i 3 o a! 8 si a Oi CJ d" Ui 8 tQo- t - i I n I rv J- h MPI •AiMA ^ 0.001 0.01 0.1 1.0 10.0 FREQUENCY (HERTZ)

Figure D.13b Power Spectrum of Longitudinal Load Values From East Conductor for Record N16 368

8 PO«R SPECTRIN OF M1S-LCD5 TOTRL

a CO to m

^ §

a!

to

I I I I I III I I I I I I HI; I I I I I III 0.001 0.01 0.1 1.0 FREQUENCY (HERTZ)

Figure D.14a Power Spectrum of Total Load Values From Center Conductor for Record N16

POICR SPECTRIN OF N1S.LJC05 TRRNSVEKSE DIRECTION

'0.001 FREQUENCY (HERTZ)

Figure D 14b Power Spectrum of Transverse Load Values TTr^r^m rionter Conductor for Record N16 369

8 PO«R SPECTRIN OF M18.im5 f» LONOmOINfl. OIRECnON a

C3 60 0 to . O o ^^ to SO O to • m u. 8 1 9 o UJ 3^4

QC ^

<0 ci

'0.001 0.1 1.0 10.0 FREQUENCY (HERTZ)

Figure D.15a Power Spectrum of Longitudinal Load Values From Center Conductor for Record N16 370

P(»CR SPECTRIN OF NDSuSCOE i mftET SEPCTRRL MIMXMI

o to

UJ §

ai oc

O- to

I iillim I I ililH| i^*'i'—I'Fl'Hi •! W ^•^W-i-i-rr^ '0.001 0.01 0.1 1.0 10.0 FREQUENCY (HERTZ)

Figure D.16a Power Spectrum of Diagonal Strain Gage Located at SE Corner for Record NOS

P(90 SPECTRIN OF MK.SC12 (TIKET SPECTRRL MIMXMI

o CO ^i u. <^ I UJ ^ 8 ai 5 »— CJ Ui 0. to

I I I iii| I" Ff» '0.001 0.01 0.1 1.0 10.0 FREQUENCY (HERTZ)

Power Spectrum of Diagonal Strain Gage Figure D.16b Located at NW Corner for Record NOS 371 a Pt»CR SPECTRIH OF FO7.SD05 (TIKFT SPECTRRL HIWXMI

1.0 10.0 FREQUENCY (HERTZ)

Figure D.17a Power Spectrum of Main Strain Gage Located at SE Corner for Record N07

POICR SPECTRIN OF PC7.SC11 (TIKET SPECTRRL MINRMI

'^0.001 FREQUENCY (HERTZ)

Figure D.17b Power Spectrum of Main Strain" Gage Located at NW Corner for Record N07 372

POICR SPECTRIN OF ND7.SG06

(X (TIKET SPECTRRL HIMXMI a to o CO \ cn m

I UJ ai >- ai oc h- CJ Ui a_ to

0.001 0.01 0.1 1.0 10.0 FREQUENCY (HERTZ)

Figure D.18a Power Spectrum of Diagonal Strain Gage Located at SE Corner for Record N07

POICR SPECTRIN OF W7.SC12 (TVK£T SPECTRRL MI^G0M1

»-« CO ^ i I UJ => ai ai 1 oc H- CJ Ui a. to i f I I r mr L Ut.i.i, 0.001 0.01 0.1 1.0 10.0 FREQUENCY (HERTZ)

Figure D 18b Power Spectrum of Diagonal Strain Gage Located at NW Corner for Record N07 373

POKS SPECTRLH OF MMLSCOS i CnKT SPECTRRL MINMMI

o CO v.

I UJ 3 o a! 8 a! §

a. o to J i I I I I I iii| ^ I rrrr- La '0.001 0.01 0.1 1.0 10.0 FREQUENCY (HERTZ)

Figure D.19a Power Spectrum of Diagonal Strain Gage Located at SE Corner for Record NOS

Pa»l SPECTRIM OF N0B.SCI2 mKET SPECTRRL MIMXMI d' § S •>; ~ SI G 1 .00 0 V. «a <^ a i 9. 1 " UJ § ^ d _l ^ § ^i S •^- 1 SP E 1.00 0

I I iii|" '•III llf 1 l.OO O 10.0 '0.001 0.01 0.1 1.0 FREQUENCY (HERH)

Figure D.19b Power Spectrum of Diagonal Strain Gage Located at NW Corner for Record NOS 374 8 PIKR SPECTRIN OF N16.SC05 (TIKET SPECTRRL MIMXMI

0.001 0.01 0.1 1.0 FREQUENCY (HERTZ)

Figure D.20a Power Spectrum of Main Strain Gage Located at SE Corner for Record N16

8 POWl SPECTRIN OF N16.SC11 (TVKET SPECTRRL MIMIOMI o s_ s d SI G .00 0 L a ;;; m U. aM 1 o UJ o9 3 o

VA L § a ai o (^ PI CJ d" S5 o.

10.0 FREQUENCY (HERTZ)

Figure D.20b Power Spectrum of Main Strain Gage Located at NW Corner for Record N16 8 POO SPECTRUN OF N16.SC06 375 (TIKO SPECTRRL MIMXMI

a to O 1-^ CO cn M

I UJ ai ai oc 0-

FREQUENCY (HERTZ)

Figure D.21a Power Spectrum of Diagonal Strain Gage Located at SE Corner for Record N16

8 POWR SPECTRIN OF N1S.SC12 (TIKET SPECTRRL MIMXMI

CO 1 >^ d CO m

UJ ^

^ 8

Ui to

I I I 111m I I I 11 III! , i','iiii

Figure D 21b Power Spectrum of Diagonal Strain Gage Located at NW Corner for Record N16 APPENDIX E FREQUENCY RESPONSE FUNCTION

GRIN FltCTION CF f«S.MSOS flNO N0S.SC11

(M to m cn cd m I o O U.

I I I • 11ii| '0.001 0.01 FREQUENCY (HERTZ) Figure E.la Frequency Response Function Relating Wind Speed and NW Main Leg Strain Record for Record NOS

GRIN FUMineM OF M)8.)605 AND M08.SC11

a :^- CM

FU N i 3C M S 8. •

'0.001 0.01 FREQUENCY (HERTZ)

Figure E.lb Frequency Response Function Relating Wind Speed and NW Main Leg Strain Record for Record NOS 376 377 t3«H RfCnCN OF M)7.«0S (Hi N07.SG05

a

Mi

m

o I—« »— CJ

0.001 0.01 0.1 1.0 10.0 FREQUENCY (HERTZ)

Figure E.2a Frequency Response Function Relating Wind Speed and SE Main Leg Strain Record for Record N07

GRIN FUMrnCM OF MI7.I60S RN) Na7.SGll

'0.001 0.01 0.1' 1.0 FREQUENCY (HERTZ)

Figure E.2b Frequency Response Function Relating Wind Speed and NW Main Leg Strain Record for Record N07 378 GRIN FUNHICN OF N07.M50S 81 RN) N07.S606

cn 3 Mi * cn ^d-

CJ w

!_• O -

I I I I I IIIIIr! I TVT^HTlf^**!—#^!*T 0.001 0.01 0.1 • i.Q FREQUENCY (HERTZ)

Figure E.3a Frequency Response Function Relating Wind Speed and SE Diagonal Leg Strain Record for Record N07

GRIN RJNCnCN OF MI7.M5C5 RM) N07.SG12 31

CM cn Jl 8 cn

a' (X

\ T^^^^TTiH I I I iiiii|^ 'O.OOl 0.01 0.1 , 1.0 10.0 FREQUENCY (HERTZ)

Figure E.Sb Frequency Response Function Relating Wind Speed and NW Diagonal Leg Strain Record for Record N07 379 GRIN FUCnCN OF tOS.iaB §1 (TOTRLI no N06.SG05

J d

2 8-1 « 8-

Z 8- u. Ss^

tfff 1 'T f I 11 HI 0.001 0.1 1.0 10.0 FREQUENCY (HERTZ)

Figure E.4a Frequency Response Function Relating Total Load From West Conductor and SE Main Leg Strain Record for Record NOS

GRIN RJMniON OF NOLLOB in (TOTRLI (Ml Na6.S611

CM cii-n cn

V 8-^ ft

i-

•> I II W| T"^ mr,— ^^ 11 llf 0.001 0.01 0.1 1.0 10.0 FREQUENCY (HERTZ)

Figure E.4b Frequency Response Function Relating Total Load From West Conductor and NW Main Leg Strain Record for Record NOS 380

GRIN RlNCnON OF M)5.LC05 (TOTRLI WO NOS.S(»

10.0 FREQUENCY (HERTZ)

Figure E.Sa Frequency Response Function Relating Total Load From Center Conductor and SE Diagonal Leg Strain Record for Record NOS

GRIN RKHION OF MB.LCXB (TOTRLI mo N06.SC12

'0.001 FREQUENCY (HERTZ)

Figure E.Sb Frequency Response F'.inction Rela^ir.-; Total Load From Center Conductor and NW Diagonal Leg Strain Record for Record NOS 381 GRIN FUCnW OF M)7.L£0a (TOTRLI RM) N07.SGa5

10.0 FREQUENCY (HERTZ)

Figure E.Sa Frequency Response Function Relating Total Load From West Conductor aind SE Main Leg Strain Record for Record N07

GRIN FUCnCN OF M)7.LaB (TOTRL) no N07.S611

FREQUENCY (HERTZ)

Figure E.6b Frequency Response Function Relating Totil Load From West Conductor and NW Main Leg Strain Record for Record N07 382

GRIN RJNCnON OF M)7.IX03 81 (TOm.) RM) N07.SG06

CM cn Mi cn 9 u. d- o

CJ u.

0.001 10.0 FREQUENCY (HERTZ)

Figure E.7a Frequency Response Function Relating Total Load From West Conductor and SE Diagonal Leg Strain Record for Record N07

GRIN FUCnCN OF M)7.LCQa (TOTRLI no N07.S612 81

CM cn Mi cn

I I I i iii| T '0.001 0.01 0.1 1.0 10.0 FREQUENCY (HERTZ)

Frequency Response Function Relating Total Figure E.7b Load From West Conductor and NW Diagonal Leg Strain Record for Record N07 383 GRIN FUCnOI OF MI7.La» (TOTRL) RM) um.soas

0.001 1.0 10.0 FREQUENCY (HERTZ)

Figure E.Sa Frequency Response Function Relating Total Load From East Conductor and SE Main Leg Strain Record for Record N07

GRIN RJNCnON OF Mn.LCOt 81 (TOTRL) AM) N07.SG0C

CM cn icn U- d- I o

0.001 0.01 0.1 1.0 FREQUENCY (HERTZ)

Figure E.Sb Frequency Response Function Relating Total Load From East Conductor and SS Di^sigcnAl Leg Strain Record for Record N07 384

GRIN FUNCTION OF M)a.LCa3 81 (TOTRL) AND M)«.SG06

CM cn Mi cn 9 d-

CJ

0.001 0.1 1.0 FREQUENCY (HERTZ)

Figure E.9a Frequency Response Function Relating Total Load From West Conductor and SE Diagonal Leg Strain Record for Record NOS

GRIN RJMrntM OF M)a.LJCa9 aOTRL) RNO M)8.SC12

JO

m

m u. d- I o

'0.001 0.1 FREQUENCY

Figure E.9b Frequency Response Function Relating Tntal Load From West Conductor and NW DiBigonal Leg Strain Record for Record NOS 385 GRIN FUNCnm OF M)8.LaE 81 (TOTRL) mo M)8.SC06

(M cn Mi cn

Uu I d- o

0.001 FREQUENCY (HERTZ)

Figure E.10a Frequency Response Function Relating Total Load From Center Conductor and SE Diagonal Leg Strain Record for Record NOS

GRIN FUCnON OF MJOLLCOB aOTRL) RM) M)8.SC12

Ml cn

u. I d- o h- (J

rrrr '0.001 0.01 0.1 1.0 FREQUENCY (HERTZ)

Figure E.lOb Frequency Response Function R<=latin^ T'^^al Load From Center Conductor and NW Diagonal Leg Strain Record for Record NOS 386 GRIN FUCneW OF M)S.LCia 31 (TRRNS.) no M)5.SC06

(M (n ii 8 cn 9 o d

10.0 FREQUENCY (HERTZ)

Figure E.11a Frequency Response Function Relating Transverse Load From West Conductor and SE Diagonal Leg Strain Record for Record NOS

GRIN FUCnON OF M15.LC0a (TRIMS.) no M)5.SC12

CM cn 1 8 cn

O m 8

CJ

I 11ii| '0.001 0.01 0.1 1.0 10.0 FREQUENCY (HERTZ)

Figure E.lib Frequency Response Function Relating Transverse Load From West Conductor and NW Diagonal Leg Strain Record for Record NOS 387 GRIN FUCnOM SF MS.L£IN (TRfMS.) fW M)S.SC06

'0.001 FREQUENCY (HERTZ)

Figure E.12a Frequency Response Function Relating Transverse Load From East Conductor and SE Main Leg Strain Record for Record NOS

GRIN FUCnON OF MB.LnN § (TRms.) no M)5.xn

m i ^irt ft (O 9"N. u.

1 00 0

•-o< »— o § 00 0 u. L _

• • I I I llil 0.001 0.01 10.0 FREQUENCY (HERTZ)

Figure E.12b Frequency Response Function Relating Transverse Load From East Conductor and NW Main Leg Strain Record for Record NOS 388 GRIN FUCnW OF NOB.LOS (TRRNS.) RIO NOe.SGOS

CM o Mi cn 9 V § o ft

i

I ll I I llll 0.001 0.01 FREQUENCY (HERTZ)

Figure E.13a Frequency Response Function Relating Transverse Load From Center Conductor and SE Main Leg Strain Record for Record NOS

GRIN FUCmai OF M)8.LCa5 (TRRNS.) no Noa.scii

'0.001 10.0 FREQUENCY (HERTZ)

Figure E.13b Frequency Response Function Relating Transverse Load From Center Conductor and NW Main Leg Strain Record for Record NOS 389 GRIN FUCneN OF mJ.UCCB (TRfMS.) no N07.SG06

f I I I i iii| '0.001 0.01 FREQUENCY (HERH)

Figure E.14a Frequency Response Function Relating Transverse Load From West Conductor and SE Main Leg Strain Record for Record N07

GRIN FUNrnCM OF M17.Lin3 (TRftts.) no Mi7.scn

a §. CM - 0^ a « 1 cn irf- ii. V =• § 1 •—1 . - »- •» , CJ § § •^ ™-

2 900* 1 00 0 IW O 1 lll 1

11 I^SML 1

1 io.a *'o. 1 ' 0.01 0.1- 1.0 001 FREQUENCY (HERTZ)

Figure E.14b Frequency Response Function Relating Transverse Load From West ConduL-tor and NW Main Leg Strain Record for Record NO 7 390 GRIN FUCnON OF M)7.LaB (TRfMS.) PNO M)7.SG06 81

CM cn cn

0.001 FREQUENCY (HERTZ)

Figure E.15a Frequency Response Function Relating Transverse Load From West Conductor and SE Diagonal Leg Strain Record for Record N07

GRIN FUMHieN OF M)7.LaB 81 (TRfMS.) RNO M)7.SCt2

CM cn Mi cn m u. d- I o »— CJ

10.0 '0.001 FREQUENCY (HERTZ)

Figure E.15b Frequency Response Function Relating Transverse Load From West Conductor and NW Diagonal Leg Strain Record for Record N07 391 GRIN FUCnON OF MI7.LJCn (TRfMS.) no MI7.SG06

'0.001 FREQUENCY (HERH)

Figure E.16a Frequency Response Function Relating Transverse Load From East Conductor and SE Main Leg Strain Record for Record N07

GRIN FUCnON OF Mr7.LaM (TRfMS.) RM) ND7.SC06

CM cn Mi cn

d-

u

FREQUENCY (HERTZ)

Figure E.16b Frequency Response Function Relating Transverse Load From East Conductor and SE Diagonal Strain Record for Record N07 392

GRIN fUCnON OF M)7.LCI5 (HUMS.I no W)7.SG05

'0.001 0.01 10.0 FREQUENCY (HERTZ)

Figure E.17a Frequency Response Function Relating Trauisverse Load From Center Conductor and SE Main Leg Strain Record for Record N07

GRIN FUKnOM OF HOrT.inE (TRfMS.) no N07.X11

'0.001 10.0 FREQUENCY (HERTZ)

Figure E.17b Frequency Response Function Relating Transverse Load From Center Conductor and NW Main Leg Strain Record for Record N07 393

GRIN FUCnON OF M)S.LJCtS (LOM/.I flIO NC6.S(i06

FREQUENCY (HERTZ)

Figure E.18a Frequency Response Function Relating Longitudinal Load From West Conductor and SE Diagonal Leg Strain Record for Record NOS

GRIN FUCTION OF M)5.iJaB (LOMk) RM) N06.SG12

I f I iii| '0.001 0.01 10.0 FREQUENCY (HERH)

Figure E.ISb Frequency Response Function Relating Longitudinal Load From West Conduc-or .na NW Diagonal Leg Strain Record for Record NOo 394 GRIN fUCnON OF M)5.LaS (LONG..) HM) N06.S60S

0.1 1.0 10.0 FREQUENCY (HERTZ)

Figure E.19a Frequency Response Function Relating Longitudinal Load From Center Conductor fiuid SE Main Leg Strain Record for Record NOS

GRIN FVNCneN OF M)5.LC05 (ljaN&.i RM) NOS.SGOS

10.0 FREQUENCY (HERTZ)

Figure E.19b Frequency Response Function Relating Longitudinal Load From Center Cmduc-or nt. i SE Diagonal Leg Strain Record for Record NOS 395 GRIN FWCHDM OF MI7.LaH 81 (LONCI no N07.SG06

Mi

O Ml

FREQUENCY (HERTZ)

Figure E.20a Frequency Response Function Relating Longitudinal Load From West Conductor and r:>ii. Diagonal Leg Strain Record for Record N07

GRIN FUMrnCN OF N07.LCaa 81 (LOMk) no N07.S612

CM

10.0 FREQUENCY (HERTZ)

Figure E.20b Frequency Response Function Relating Longitudinal Load From West Conductcr and NW Diagonal Leg Strain Record for Record N07 396 GRIN FUCnm OF N07.LCIN iUHkl RM) N07.SG0S

10.0 FREQUENCY (HERTZ)

Figure E.21a Frequency Response Function Relating Longitudinal Load From East Conductor and SE Main Leg Strain Record for Record N07

GRIN FlfCnON OF M}7.LCIM (LOMk) RM) NQ7.S611

r IIH IIH '0.001 0.01 0.1 FREQUENCY (HERTZ)

Figure E.21b Frequency Response Function Relating Longitudinal Load From East Conductor and NW Main Leg Strain Record for Record N07 397 GRIN FUNCnCN OF W7.LCDS (LOMk) no N07.SG0S

CM cn Mi cn

C!) Ml u. I o ^- CJ u.

FREQUENCY (HERTZ)

Figure E.22a Frequency Response Function Relating Longitudinal Load From Center Conductor and SE Main Leg Strain Record for Record N07

GRIN FUCniM OF ND7.LaB 81 (LONGk) RM) N07.S606

CM cn cn

u. I o

O

0.001 10.0 FREQUENCY (HERTZ)

Figure E.22b Frequency Response Function Relating Longitudinal Load From Center Ccnduct^or and SE Diagonal Leg Strain Record for Record NO? 398 GRIN FUCnOI OF M)a.LaB a.aic) no NO8.SGO6

I I I 11IIi| .001 0.01 0.1 1.0 FREQUENCY (HERH)

Figure E.23a Frequency Response Function Relating Longitudinal Load From Center Conductor and SE Diagonal Leg Strain Record for Record NOS

GRIN FUCnON OF M)B.LCIB § 0.016.) RNO N08.X11

(M § cn 9 ^•M4i cn V 9 § •v ri~ z o 8 •N.-4 CiJ M

FREQUENCY (HERTZ)

Figure E.23b Frequency Response Function Relating Longitudinal Load From Center Conductor and NW Main Leg Strain Record for Record NOS APPENDIX F COHERENCE FUNCTION

COCRENCE FUCTION QF N0B.MS05 no H0S.SCI1

10.0 FREQUENCY (HERTZ)

Figure F.la Coherence Function Relating Wind Speed and NW Main Leg Strain Record for Record NOS

CaOBCE mCTION OF WB.MS05 no I09.SC11

to.o FREQUENCY (HERTZ)

Figure F.lb Coherence Function Relating Wind Speed and NW Main Leg Strain Record for Record NOS 391-1 400 COOBCE FUCTION CF NO7.MS05 RM) M)7.SC06

I I I I I iii| '0.001 0.01 10.0 FREQUENCY (HERTZ)

Figure F.2a Coherence Function Relating Wind Speed and SE Main Leg Strain Record for Record N07

CaOBCE FUCTION BF Mn.MSOs no MP.SGII

10,J FREQUENCY (HERTZ)

Figure F.2b Coherence Function Relating Wind Speci and NW Main Leg Strain Record for Record N07 401

COOBCE FUCTION OF Na7.US05 AM) M)7.SC06

10.0 FREQUENCY (HERTZ)

Figure F.3a Coherence Function Relating Wind Speed and SE Diagonal Leg Strain Record for Record N07

CaCRBCE FUCTION CT ran.MSOS PNO I07.»12

o CJ

"l d- QC o (J

10.0 '0.001 FREQUENCY (HERTZ)

Figure F.Sb Coherence Function Relating Wind Speed and NW Diagonal Leg Strain Record for Record N07 402 COOENCE FUCTION OF N07.LC03 RNO N07.SC06

oc

o

0.001 FREQUENCY (HERTZ)

Figure F.4a Coherence Function Relating Total Load From West Conductor and SE Main Leg Strain Record for Record N07

CflHBSCE FUCTION OF NO7.L003 RNO MJ7.SC11

'0.001 0.01 FREQUENCY (HERTZ)

Figure F. 4b Coherence Function Relating Total Loat From West Conductor and NW Main Leg Strain Record for Record N07 403 CHeSCE FUCTION tF mj.Loaa no NO7.SGOB

FREQUENCY (HERTZ)

Figure F. Sa Coherence Function Relating Total Load From West Conductor and SE Diagonal Leg Strain Record for Record N07

COOBCE FUCTION 8F MH.LOOS no M)7.SC12

'0.001 FREQUENCY (HERTZ)

Figure F.Sb Coherence Function Relating Total Load From West Conductor and NW Diagonal Leg Strain Record for Record N07 404 8 CflHOBCE FUCTION GF Na7.L00V RNO N07.SG06

FREQUENCY (HERTZ)

Figure F.Sa Coherence Function Relating Total Load From East Conductor and SE Main Leg Strain Record for Record N07

CflHBteCE FUCTION OF Wn.LCOH FMO »O7.SC06

'0.001 FREQUENCY (HERTZ)

Coherence Function Relating Total Load Figure F.6b From East Conductor and bE Diagonal Leg Strain Record for Record N07

illft&^_ 405

8 C8«BCE FUCTION OF o NOB.LOOS FMO N08.SC06,

10.0 FREQUENCY (HERTZ)

Figure F.7a Coherence Function Relating Total Load From Center Conductor and SE Diagonal Leg Strain Record for Record NOS

COCRSCE FUCTION (T W)a.L(a5 PNO M)8.SC12

10.0 '0.001 0.1 FREQUENCY (HERTZ)

Figure F.7b Coherence Function Relating Total Lo -A From Center Conductor and NW Dia^-nal Leg Strain Record for Record NOS 406 CaOOCE PUCTION OP § N07.LC05 no UD7.SG06 i ° §

FREQUENCY (HERTZ)

Figure F.Sa Coherence Function Relating Transverse Load From Center Conductor and SE Main Leg Strain Record for Record N07

cacxace PUCTIOH OF NO7.L00S PM) 107. sen

10.0 '0.001 FREQUENCY (HERTZ)

Figure F.Sb Coherence Function Relating Tranv.-rse Load From Center Conductor and NW M.-^in Leg Strain Record for Record N07 407 COCReCE FUCTION OF tm.Ltm no MO7.S(XS

FREQUENCY (HERTZ)

Figure F.9a Coherence Function Relating Transverse Load From East Conductor and SE Main Leg Strain Record for Record N07

CaOBCE FUCTION OF mJ.LOM no M)7.SG06

I I I I I llll '0.001 0.01 10.0 FREQUENCY (HERTZ)

Figure F.9b Coherence Function Relating Tranverse Load From East Conductor and SE Di^.'nil Leg Strain Record for Record N07 408

CWBJBCE FUCTION BF 'NB.LCOa RPO M)5.SC11

1.0 10.0 FREQUENCY (HERTZ)

Figure F. 10a Coherence Function Relating Transverse Load From West Conductor and NW Main Leg Strain Record for Record NOS

Ca«BCE FUCTION OF NOB. LCOS no M)5.SC12

0.1 1.0 FREQUENCY (HERTZ)

Figure F.lOb Coherence Function Relating Tranverse Load From West Conductor and NW Diagonal Leg Strain Record for Record NOS 409 cohemcE FUCTION r nm.Lcoa no to7.sG06

0.001 0.01 0.1* 1.0 10.0 FREQUENCY (HERTZ)

Figure F.11a Coherence Function Relating Longitudinal Load From West Conductor and SE Diagonal Leg Strain Record for Record N07

PUCTION CP mj.Lcna PNO MO7.SCI2

I I I I I in; '0.001 0.01 0.1- 1.0 FREQUENCY (HERH)

Figure F.lib Coherence Function Relating Longitudinal Load From West Conductor and NW Diagonal Leg Strain Record for Record N07 410 cacRecE FUCTION OF N07.LCQ4 no N07.SG06

10.0 FREQUENa (HERTZ)

Figure F.12a Coherence Function Relating Longitudinal Load From East Conductor and SE Main Leg Strain Record for Record N07

CaOBMZ FUCTION tf Wn.LOOii RNO M)7.Xn

3.0 FREQUENCY (HERTZ)

Coherence Function Relating Longitudinal Figure F.12b Load From East Conductor and NW Main Leg Strain Record for Record N07 APPENDIX G MOVING AVERAGE PARAMETERS

Time Series: NOS.WSOS MA Parameter Numerical Value 1 -0.4086 2 -0.2302 3 -0.2252 4 -0.1102 5 -0.0597 6 -0.0423

Variance of White Noise - 0.00145953 Constant Term Estimate = -7.702 E-05

411 412

Time Series: N07.WS05 MA Parameter Numerical Value 1 -0.7128 2 -0.1667 3 -0.1881 4 -0.0356 5 -0.0027 6 0.0400 7 0.0587 8 0.0694 9 0.0758 10 0.0643 11 0.0395 12 0.0431 13 0.0477 14 0.0197 15 0.0264 16 0.0486 Variance of White Noise = 0.109127 Constant Term Estimate = 0.00017568 413

Time Series: NOS.WSOS

MA Parameter Numerical Value

1 -0.8922 2 -0.3277 3 -0.2473 4 -0.0721 5 -0-0194 6 0.0193 7 0.0656 8 0.0746 9 0.1145 10 0.1069 11 0.0814 12 0.0656 13 0.0511 14 0.0621 15 0.0473 16 0.0370 17 0.0335 Variance of White Noise = 0.0430502 Constant Term Estimate = -0.00130541