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NASA SP-7037 (275) February 1992 AERONAUTICAL ENGINEERING A CONTINUING BIBLIOGRAPHY WITH INDEXES (NASA-SP-7017(27t>» AERONAUTICAL N92-28&79 ENGINFERING: A CONTINUING BIBLIOGRAPHY ** INDEX ! .PPLEMENT 275) (NASA) 112 p Uncl 00/01 0099273 STI PROGRAM SCIENTIFIC & TECHNICAL IMCORMATION NASA SP-7037 (275) February 1992 AERONAUTICAL ENGINEERING A CONTINUING BIBLIOGRAPHY WITH INDEXES National Aeronautics and Space Administration Scientific and Technical Information Program NASA Washington, DC 1992 INTRODUCTION This issue of Aeronautical Engineering—A Continuing Bibliography (NASA SP-7037) lists 379 reports, journal articles, and other documents originally announced in January 1992 in Scientific and Technical Aerospace Reports (STAR) or in International Aerospace Abstracts (IAA). Accession numbers cited in this issue are: STAR (N-10000 Series) N92-10001 - N92-11965 IAA (A-10000 Series) A92-10001 - A92-13248 The coverage includes documents on the engineering and theoretical aspects of design, con- struction, evaluation, testing, operation, and performance of aircraft (including aircraft engines) and associated components, equipment, and systems. It also includes research and develop- ment in aerodynamics, aeronautics, and ground support equipment for aeronautical vehicles. Each entry in the publication consists of a standard bibliographic citation accompanied in most cases by an abstract. The listing of the entries is arranged by the first nine STAR specific categories and the remaining STAR major categories. This arrangement offers the user the most advantageous breakdown for individual objectives. The citations include the original ac- cession numbers from the respective announcement journals. Seven indexes—subject, personal author, corporate source, foreign technology, contract number, report number, and accession number—are included. A cumulative index for 1992 will be published in early 1993. Information on availability of documents listed, addresses of organizations, and NTIS price schedules are located at the back of this issue. CONTENTS Category 01 Aeronautics (General) 1 Category 02 Aerodynamics 2 Includes aerodynamics of bodies, combinations, wings, rotors, and control sur- faces; and internal flow in ducts and turbomachinery. Category 03 Air Transportation and Safety 14 Includes passenger and cargo airtransport operations; and aircraft accidents. Category 04 Aircraft Communications and Navigation 19 Includes digital and voice communication with aircraft; air navigation systems (satellite and ground based); and air traffic control. Category 05 Aircraft Design, Testing and Performance 20 Includes aircraft simulation technology. Category 06 Aircraft Instrumentation 23 Includes cockpit and cabin display devices; and flight instruments. Category 07 Aircraft Propulsion and Power 24 Includes prime propulsion systems and systems components, e.g., gas turbine engines and compressors; and onboard auxiliary power plants for aircraft. Category 08 Aircraft Stability and Control 26 Includes aircraft handling qualities; piloting; flight controls; and autopilots. Category 09 Research and Support Facilities (Air) 30 Includes airports, hangars and runways; aircraft repair and overhaul facilities; wind tunnels; shock tubes; and aircraft engine test stands. Category 10 Astronautics 32 Includes astronautics (general); astrodynamics; ground support systems and facilities (space); launch vehicles and space vehicles; space transportation; space communications, spacecraft communications, command and tracking; spacecraft design, testing and performance; spacecraft instrumentation; and spacecraft propulsion and power. Category 11 Chemistry and Materials 33 Includes chemistry and materials (general); composite materials; inorganic and physical chemistry; metallic materials; nonmetallic materials; propellants and fuels; and materials processing. Category 12 Engineering 36 Includes engineering (general); communications and radar; electronics and electrical engineering; fluid mechanics and heat transfer; instrumentation and photography; lasers and masers; mechanical engineering; quality assurance and reliability; and structural mechanics. INTENTIONALLY BLANK. Category 13 Geosciences 45 Includes geosciences (general); earth resources and remote sensing; energy production and conversion; environment pollution; geophysics; meteorology and climatology; and oceanography. Category 14 Life Sciences 46 Includes life sciences (general); aerospace medicine; behavioral sciences; man/system technology and life support; and space biology. Category 15 Mathematical and Computer Sciences 47 Includes mathematical and computer sciences (general); computer operations and hardware; computer programming and software; computer systems; cybernetics; numerical analysis; statistics and probability; systems analysis; and theoretical mathematics. Category 16 Physics 53 Includes physics (general); acoustics; atomic and molecular physics; nuclear and high-energy physics; optics; plasma physics; solid-state physics; and ther- modynamics and statistical physics. Category 17 Social Sciences 56 Includes social sciences (general); administration and management; documen- tation and information science; economics and cost analysis; law, political sci- ence, and space policy; and urban technology and transportation. Category 18 Space Sciences N.A. Includes space sciences (general); astronomy; astrophysics; lunar and planet- ary exploration; solar physics; and space radiation. Category 19 General 57 Subject Index A- Personal Author Index B- Corporate Source Index C- Foreign Technology Index D- Contract Number Index E- Report Number Index F- Accession Number Index G-1 Appendix APP-1 VI TYPICAL REPORT CITATION AND ABSTRACT NASA SPONSORED ON MICROFICHE ACCESSION NUMBER - -N92-10979** United Technologies Research Center, East- • CORPORATE SOURCE Hartford, CT. TITLE - •DEVELOPMENT OF UNSTEADY AERODYNAMIC ANALYSES FOR TURBOMACHINERY AEROELASTIC AND AEROACOUSTIC APPLICATIONS AUTHORS- -JOSEPH M. VERDON, MARK BARNETT, KENNETH C. HALL, and TIMOTHY C. AYER Washingtion NASA Oct. 1991J12 CONTRACT NUMBER • -(Contract NAS3-25425) PUBLICATION DATE REPORT NUMBERS • - (NASA-CR-4405; E-6528; NAS 1.26:4405; R91-957907-3) Avail: AVAILABILITY SOURCE • -NTISHC/MFA06CSCL01/1 -. COSATI CODE PRICE CODE Theoretical analyses and computer codes are being developed for predicting compressible unsteady inviscid and viscous flows through blade rows. Such analyses are needed to determine the impact of unsteady flow phenomena on the structural durability and noise generation characteristics of turbomachinery blading. Emphasis is being placed on developing analyses based on asymptotic representations of unsteady flow phenomena. Thus, flow driven by small-amplitude unsteady excitations in which viscous effects are concentrated in thin layers are being considered. The resulting analyses should apply in many practical situations, lead to a better understanding of the relevent physics, and they will be efficient computationally, and therefore, appropriate for aeroelastic and aeroacoustic design applications. Under the present phase (Task 3), the effort was foucused on providing inviscid and viscid prediction capabilities for subsonic unsteady cascade flows. Author TYPICAL JOURNAL ARTICLE CITATION AND ABSTRACT NASA SPONSORED ACCESSION NUMBER - -A92-13210* National Aeronautics and Space Administration.- CORPORATE SOURCE Ames Research Center, Moffett Field, CA. TITLE -PROBE SHAPES FOR STREAMWISE MOMENTUM AND CROSS-STREAM TURBULENCE INTENSITY AUTHOR -VERNON ROSSOW, J. (NASA, Ames Research Center, Moffett - AUTHORS' AFFILIATION Field, CA) Journal of Aircraft (ISSN 0021-8669), vol. 28, Nov. 1991, p. 741-749. refs Copyright JOURNAL TITLE When the highly turbulent flowfields at the edges of jets, in augmentors, and in other jet-mixing devices are surveyed with conventional pilot probes, the values indicated by the instruments may contain a significant increment brought about by the dynamics of the eddies. Although the influence of turbulence on the measurements is usually negligible in streams where the turbulence level is 1 percent or less, the effect of turbulence on static and total pressure measurements can be around 20 percent when the turbulence level exceeds 40 percent. This paper describes a theoretical study that develops probe shapes that directly measure the time-averaged total pressure based on the streamwise component of the velocity vector to obtain a direct measurement of the streamwise momentum. The difference between the time-averaged pressure indicated by such a probe and one that measures the total head based on the entire velocity vector yields the cross-stream turbulence intensity. Author VII AERONAUTICAL ENGINEERING A Continuing Bibliography (Suppl. 275) FEBRUARY 1992 01 measured properties of currently available balloon construction materials. The resulting strains induced for various sized balloons is calculated and shown to be acceptable for a large variety of AERONAUTICS (GENERAL) sizes. The disadvantages of the production method are described and weighed in comparison to the advantage of decreased change-over time and increased production efficiency. Future plans for production equipment modernization to take full advantage of the ST process are presented. Author A92-10197 MANUFACTURE OF A PRIMARY FLIGHT STRUCTURE USING A92-11021# THERMOPLASTICS WHITHER SCIENTIFIC BALLOONING? PIERRE JOUIN, THOMAS LEE (McDonnell Douglas Helicopter Co., J. A. WINKER (Rekwin Co., Sioux Falls, SD) IN: AIAA International Mesa,
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