Iowa State University Capstones, Theses and Retrospective Theses and Dissertations Dissertations

1-1-2002

Investigation of methods for real time determination of grain damage

Michael A. Brand Iowa State University

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This Thesis is brought to you for free and open access by the Iowa State University Capstones, Theses and Dissertations at Iowa State University Digital Repository. It has been accepted for inclusion in Retrospective Theses and Dissertations by an authorized administrator of Iowa State University Digital Repository. For more information, please contact [email protected]. Investigation of methods for real time determination of grain damage

by

Michael A. Brand

A thesis submitted to the graduate faculty

in partial fulfillment of the requirements for the degree of

MASTER OF SCIENCE

Major: Agricultural Engineering (Agricultural Power and Machinery)

Program of Study Committee: Graeme Quick, Co-major Professor Carl Bern, Co-major Professor Stuart Birrell Dan Nettleton Brian Steward Bruce Warman

Iowa State University

Ames, Iowa

2002

Copyright ©Michael A. Brand, 2002. All rights reserved. 11

Graduate College Iowa State University

This is to certify that the master's thesis of

Michael A. Brand has met the thesis requirements of Iowa State University

Signatures have been redacted for privacy 111

TABLE OF CONTENTS

LIST OF TABLES v

LIST OF FIGI:TRES

ACKNOWLEDGEMENTS 1X

CHAPTER ONE. GENERAL INTRODUCTION 1 Introduction 1 Thesis Organization 4 Literature Review 4 References 27

CHAPTER TWO. AIRFLOW SEPARATION OF DAMAGED CORN 33 Abstract 33 Introduction 33 Materials and Methods 35 Results and Discussion 40 Summary and Conclusions 45 References 60

CHAPTER THREE. ULTRAVIOLET DETECTION OF DAMAGED CORN 62 Abstract 62 Introduction 63 Materials and Methods 64 Results and Discussion 69 Summary and Conclusions 75 References 93

CHAPTER FOUR. GENERAL CONCLUSIONS 95 Phoenix Grain Damage Sensor 95 Airflow Separation Test Stand 96 Damage Measurement Design Parameters 96 Suggestions for Further Study 99 1V

Reference 100

APPENDIX A. R.AW DATA AND CALCULATIONS 101

APPENDIX B. ADDITIONAL TABLES 125 v

LIST OF TABLES

Table 1.1 USDA Grades and Grade Requirements for Corn 5

Table 2.1 Definitions of insert configurations and corresponding maximum airflow Values 57

Table 2.2 Mass of rewetted fines in each 3 kg corn sample for three damage levels and three moisture contents 57

Table 2.3 Mean damage quantities and Tukey comparisons of means from four common damage tests at three damage levels using pilot study data 58

Table 2.4 Mean damage measurements and Tukey comparisons of means for four common damage tests at three moisture contents and three damage levels 58

Table 2.5 Summary of significant differences in means at three moisture contents for three configurations of the airflow test stand 59

Table 2.6 Calibration regression coefficients and r2 values for predicting various common damage values using test stand response as input 59

Table 2.7 Evaluation regression coefficients and r2 values for predicting various common damage values using test stand response as input 60

Table 3.1 Mass of rewetted fines in each 3 kg corn sample for three damage levels and three moisture contents 91

Table 3.2 Mean damage measurements and Tukey comparisons of mean pairs for four common damage tests at three moisture contents and three damage levels 91

Table 3.3 Mean sensor response (pulses/kg) and Tukey comparisons of mean pairs for two flow rates of the Phoenix damage sensor at three moisture contents and three damage levels. 92

Table 3.4 Summary of regression coefficients for calibration number 1 using raw number of pulses as the sensor response 92

Table 3.5 Summary of regression coefficients for calibration number 2 using average number of pulses per second as the sensor response 92

Table 3.6 Summary of regression coefficients for calibration number 3 using number of pulses per kilogram of corn as the sensor response 93 vl

Table 3.7 Summary of model descriptors for 3 regression analyses and three common damage tests using grain damage sensor data 93

Table A1 Raw data from pilot study 102

Table A2 Raw data from low moisture study 107

Table A3 Raw data from mid moisture study 109

Table A4 Raw data from high moisture study 111

Table AS Phoenix damage meter calculations for pilot study data 113

Table A6 Phoenix damage meter calculations for low moisture data 114

Table A7 Phoenix damage meter calculations for mid moisture data 115

Table A8 Phoenix damage meter calculations for high moisture data 116

Table A9 Airflow test stand calculations for pilot study data 117

Table A10 Airflow test stand calculations for low moisture data 122

Table A11 Airflow test stand calculations for mid moisture data 123

Table Al2 Airflow test stand calculations for high moisture data 124

Table B1 Data summary and Tukey significance comparisons between means for pilot study data 126

Table B2 Data summary and Tukey significance comparisons between means for low moisture data 128

Table B3 Data summary and Tukey significance comparisons between means for mid moisture data 129

Table B4 Data summary and Tukey significance comparisons between means for high moisture data 130

Table BS Correlation coefficients for pilot study data 131

Table B6 Correlation coefficients for low moisture data 133

Table B7 Correlation coefficients for mid moisture data 134

Table B8 Correlation coefficients for high moisture data 135 Vll

LIST OF FIGURES

Figure 2.1 Test stand used for airflow separation of damaged grain 47

Figure 2.2 Wire screen used to close the top of the secondary chute 48

Figure 2.3 Two solid inserts and one grate insert between primary and secondary drop chutes 49

Figure 2.4 Calibration data for visual damage level using test stand data as input 50

Figure 2.5 Calibration data for BCFM measurement using test stand data as input 51

Figure 2.6 Calibration data for green dye damage level using test stand data as input 52

Figure 2.7 Validation data and prediction equation line for visual damage calibration 53

Figure 2.8 Validation data and prediction equation line for BCFM content calibration 54

Figure 2.9 Validation data and prediction equation line for green dye damage Calibration 55

Figure 2.10 Material stuck to grate with angled duct and insert configuration 1 at the completion of a fast cylinder damage test before and after the airflow was removed 56

Figure 3.1 Phoenix grain damage sensor test stand 77

Figure 3.2 Side by side comparison of funnels used to establish high and low flow rates 78

Figure 3.3 Calibration 1 data for BCFM test using raw number of pulses as damage sensor response 79

Figure 3.4 Calibration 2 data for BCFM test using average number of pulses per second as damage sensor response 80

Figure 3.5 Calibration 3 data for BCFM test using number of pulses per kilogram of corn a damage sensor response 81

Figure 3.6 Calibration 1 data for visual damage test using raw number of pulses as damage sensor response 82

Figure 3.7 Calibration 2 data for visual damage test using average number of pulses per second as damage sensor response 83 Vlll

Figure 3.8 Calibration 3 data for visual damage test using number of pulses per kilogram of corn as damage sensor response 84

Figure 3.9 Calibration 1 data for green dye damage test using raw number of pulses as damage sensor response 85

Figure 3.10 Calibration 2 data for green dye damage test using average number of pulses per second as damage sensor response 86

Figure 3.11. Calibration 3 data for green dye damage test using number of pulses per kilogram of corn as damage sensor response 87

Figure 3.12 BCFM verification data using three calibration techniques 88

Figure 3.13 Visual damage verification data using three calibration techniques 89

Figure 3.14 Green dye verification data using three calibration techniques 90 1X

ACKNOWLEDGEMENTS

I would like to thank Dr. Graeme Quick, Dr. Carl Bern, Dr. Brian Steward, Dr. Stuart Birrell, professors of Agricultural Engineering, Dr. Dan Nettleton, professor of Statistics, and Bruce Warman, John Deere Engineering, for serving as the program of study committee for my research. The supervision and guidance provided by the committee has been incredibly valuable in enhancing the quality of my research. In addition to serving on my program of study committee, I would also like to thank Bruce Warman and the John Deere World Wide Combine Product Development Center for providing the funding for this graduate study. I would also like to thank William Cooper of Phoenix International for providing background information on the characteristics and operation of the ultraviolet grain damage sensor provided for evaluation. Additionally, David Kmoch and Kevin Ehrecke of John Deere Engineering provided valuable advice relating to the practical application of a grain damage sensor. Additional thanks go to Leslie Anderson, Sarah Anderson, Brian Brand, and Jared Zumbach for their help in preparing corn samples for testing and carrying out the tedious process of screening samples for visible damage. Finally, I would like to thank my wife, Angela, for her understanding, patience, and support while I conducted my research and wrote this thesis. Your support has been much appreciated! 1

CHAPTER ONE. GENERAL INTRODUCTION

Introduction Mechanical grain damage can be defined as the damage inflicted upon grain by harvesting and handling equipment. This damage is often characterized by broken, cracked, split, and scuffed kernels, as well as by an increase in broken corn. Mechanical damage is a significant problem when dealing with grain commodities, as it interferes with handling, storage, processing, and use of the grain. Saul and Steele (1966) reported that molds and fungi reduce the quality of a grain crop and can make the grain dangerous for food or feed. Grain needs to be stored at a proper temperature and moisture to combat pest invasions and deterioration. Saul and Steele showed that in order to store corn with an acceptably low level of dry matter loss, corn with a high amount of mechanical damage and an initial moisture content of 28%needed to be dried for storage in 5 days or less, while hand shelled corn of the same moisture content needed to be dried for storage in 27 days or less. Steele (1967) reported that field shelled corn deteriorated two to three times faster than hand shelled corn of the same crop season. Bern and Hurburgh (1992) reported that the presence of corn fines causes an increase in airflow resistance, and that crop-drying fans are less effective when operating at a higher static pressure. As a result, the efficiency of the drying operation decreases while the power input requirement increases.

In addition to the financial burden on the farmer, mechanically damaged grain is often a burden to the processor and end user of the grain. Mold infestations in corn that result in the production of aflatoxin are hazardous to feed, and as a result, feed manufacturers must be aware of the possibility of mold infected lots (VanWormer, 1972). Mold infestations affect corn millers as well. Mechanical damage affects wet milling of corn by reducing the yield of extractable oil and starch. Molds growing on the germ of a kernel cause a depletion of the oil 2 in the kernel, and when the oil is refined, some of the remaining oil is lost when the free fatty acids produced by the molds are removed (Freeman, 1972). In addition, broken corn increases the starch and sugar content in the steepwater, resulting in increased bacterial activity. Wang and Eckhoff (2000) showed a linear relationship between solids in the steepwater and the amount of broken corn with an r2 value of 0.98. Mechanical damage affects dry milling by decreasing the amount of a delivered load that is available for processing because screenings are removed before processing. In dry milling, mold infestations and stress cracks impede the milling process (Roberts, 1972). Food corn is also affected by mechanical damage. Singh et al. (1997) showed that mechanical damage reduced the expansion volume of popcorn by 9.1 to 47.5%. A reduction of expansion volume leads to decreased palatability of the popped corn, resulting in dissatisfaction from the end user.

Mechanical damage in grain also impedes handling and transport. Mechanical damage causes problems at grain terminals by increasing the amount of time and money needed to deal with screenings. The screenings in grain cause shrink, as well as increased drying times and difficulty in storing (Dodds, 1972).

The quality of any grain is at its peak in the field before harvest; harvesting and subsequent handling will reduce the overall quality. Combine harvesters are capable of causing a large amount of damage in grain during harvest, and harvester settings have proven to be one factor in the amount of mechanical grain damage incurred during the harvest operation. Fox (1969) showed a linear relationship between combine cylinder speed and measured damage in a corn sample at a moisture content of 28%. More recent work by

Quick (2002) shows a quadratic relationship between cylinder speed and mechanical damage.

Mahmoud and Buchele (1975) determined that damage in a combine cylinder, as defined by visual inspection with green dye enhancement, is a function of moisture and the zone of the threshing cylinder from which the sample was taken. Their results show that mechanical damage in a combine cylinder could range from 15 to 45 percent. Currently, machine 3

operators have no objective feedback mechanism to relay the amount of damaged grain

passing through a combine. Therefore, machine settings are changed to obtain the lowest

level of grain damage based largely on visual inspection of bulk grain collecting in the combine hopper. To obtain a more objective measurement of grain damage in a combine, it is desirable to develop a method for monitoring grain damage at or near real-time. This feedback will provide a harvester operator with consistent, objective data to use in making decisions. regarding machine settings, and will allow the operator to minimize the amount of grain damage caused by the harvest operation.

In addition to allowing an operator to make informed decisions about machine settings, a grain damage monitor could be included with the on-machine yield and data collecting systems that are incorporated into modern combine harvesters. Recording data on grain damage, moisture, yield, losses, protein, and oil content, along with vehicle position, would allow a farmer to obtain a comprehensive picture of the crop being harvested. Devices to measure moisture and yield in relation to vehicle position have been in the marketplace for many years, and are now common in combine harvesters, available from some manufacturers as a factory installed option (Ag Leader, 2002; Case IH, 2002; John Deere, 2002). One sensor has been developed for measuring grain constituents such as oil, protein, and carbohydrate content in a stream of flowing grain, with the particular specification of being used in an agricultural combine (Mayes, 2000). However, this sensor has not yet become commercially available. This leaves grain damage as the one component of grain quality that is not currently measurable on a combine.

The objective of this research was to investigate methods for measuring grain damage at or near real-time, with a focus on technology for the evaluation of damage in corn. The resulting goal was to develop a reliable and reasonably priced grain damage sensing technology appropriate for use in a or as a stationary testing apparatus for use in elevators or inspection points. 4

Thesis Organization

This thesis is organized into a general introduction section, two papers drafted for submission to appropriate journals, and a general conclusion chapter. The general introduction contains a brief introduction to the topic, a statement regarding the organization of the thesis, and a review of literature. Each j ournal paper draft contains material on a particular grain damage sensing method. The general conclusion chapter provides a review and discussion of the research for the two grain damage detection methods investigated, as well as recommendations for further research. References are provided at the end of each. Raw data, additional figures, and additional tables are included as appendices.

Literature Review

Quantifying grain damage has been a difficult problem over the years with various standards and measurement methods used to describe grain damage. This literature review attempts to summarize some of the primary methods developed for evaluating grain damage.

Official Standards

The American Society of Agricultural Engineers (ASAE) and the United States

Department of Agriculture (USDA) have established two pertinent standards for defining damaged grain. The USDA grain grading policies determine the federal standard for grain damage in the United States grain trade, and the ASAE standard establishes a definition for damaged grain for use in agricultural engineering practice. The ASAE classifies grain damage as only the portion of the damage that is attributable to the machine, and is split into visible and invisible portions. Visible damage includes any kernel where the seed coat is visibly broken. Invisible damage is any damage that requires special procedures or instrumentation to discover (ASAE, 1998). 5

The original legislation creating standards for grain grading appeared in the U.S.

Grain Standards Act passed by Congress in 1916 (IJhrig, 1968). The grain grading standards are maintained by the USDA and are updated periodically to reflect the needs of the grain industry. However, changes have been minor, and the overall standard remains much the same as it was in 1916. The current grain grading standards for corn are summarized in

Table 1.1 and include measurements of test weight, damaged kernels, and broken corn and foreign material (BCFM) (USDA, 1996). The damaged kernels category includes measurements ofnon-mechanical damage including mold, fungal, and insect infestations, evidence of grain respiration, sprouting, and damage from artificial drying (USDA, 1997).

These damage evaluations are performed by a visual examination of the kernels by trained inspectors. BCFM content is frequently used as an indicator of mechanical damage, and is defined by the USDA to be any material that readily passes through a 4.76mm (12/64 inch) round hole sieve, and any material other than corn that remains in the sieved sample.

Although the USDA standard is used for the grain trade, the literature generally concedes

Table 1.1. USDA grades and grade requirements for corn

Maximum limits of: Minimum Test Broken Corn Weight per Heat Damaged Total Damaged Grade and Foreign Bushel (pounds) Kernels Kernels Material (percent) (percent) (percent) U.S. No. 1 56.0 0.1 3.0 2.0 U.S. No. 2 54.0 0.2 5.0 3.0 U.S . No . 3 52.0 0.5 7.0 4.0 U.S. No. 4 49.0 1.0 10.0 5.0 U.S. No. 5 46.0 3.0 15.0 7.0 U.S. Sample grade is corn that: (a) Does not meet the requirements for the grades U.S. Nos. 1, 2, 3, 4, or 5; or (b) Contains stones with an aggregate weight in excess of 0.1 percent of the sample weight, 2 or more pieces of glass, 3 or more crotalaria seeds (Crotalaria spp.), 2 or more substances) or a commonly recognized harmful or toxic substance(s), 8 or more cockleburs (Xanthium spp.), or similar seeds singly or in combination, or animal filth in excess of 0.20 percent in 1000 grams; or (c) Has a musty, sour, or commercially objectionable foreign odor; or (d) Is heating or otherwise of distinctly low quality. 6 that this measurement is inadequate for determining the total amount of damage in a corn sample. During the 1969 and 1970 crop years, Kline (1972) collected approximately 500 samples of corn from farms and elevator deliveries to analyze the amount of damage caused by combines. In this study, less than 1 % of the samples had their official grade changed due to the amount of BCFM found in the sample. The average BCFM content of the samples was 0.6%, and only two samples had more than 3%BCFM, the limit for a number 2 grade.

However, of the kernels in the analyzed samples, over 5%had visible mechanical damage, defined as less than whole kernels, and an additional 40% had hidden damage, defined as whole kernels with an indication of damage using green dye. Brass (1970) conducted a study to relate BCFM content to total damage and found that the only significant correlation relating the two was r2 = 0.14.

Due to the inability of the USDA test for BCFM to convey the total amount of mechanical damage in a grain sample, a number of other tests and techniques have been developed to attempt to accurately determine the amount of damage or other quality related factors in a crop sample. Due to differences in opinion between end users as to what constitutes damage or quality, the tests vary widely on techniques and acceptable results. A summary of some of these methods follows.

Visual Inspection

A number of grain damage studies have chosen to use a visual inspection of grain for damage as a standard damage measurement, with or without some form of enhancement. Waelti (1967) used visual inspection to quantify the amount of corn damage caused by various field conditions and combine settings. Visual inspection involves selection of a subsample of the grain of interest, typically SO-200 grams, where each kernel in the sample is individually appraised for damage. The damaged kernels are separated from the main lot, and the amount of damage is expressed as a percentage weight of the entire sample. Visual 7 grain inspection tends to be tedious and could have errors based on human judgment and fatigue (Chowdhury, 1978). A number of enhancements aid the task of visual inspection.

These enhancements fall into the categories of dyeing the kernel, water absorption and candling.

Kernel Dye: A number of different chemical dyes have been used to accentuate damage in various grains. Fast green FCF dye has been a popular dye in determination of corn damage (Chowdhury and Buchele, 1975; Kline, 1972; Brass, 1970). In this test, the corn is soaked for a certain length of time in a solution of dye, and is then rinsed with tap water. The dye adheres to any exposed starch in the kernel, but not to the seed coat itself. After the kernels are dried, they are subjected to a visual inspection. The green dye helps to accentuate small cracks or scuffs on the kernel, aiding in the visual inspection. Brass (1970) conducted a review of many various damage measurement techniques and concluded that using a visual inspection with fast green FCF dye was the best method to evaluate the damage characteristics of a new threshing cylinder design.

While using green dye is popular for corn, other dyes have been used to aid visual inspection as well. VanUtrecht et al. (2000) reported a test similar to the fast green FCF dye using a 1%indoxyl-acetate solution in . While the indoxyl-acetate test was not found to be the most desirable test under their circumstances, they reported that none of their results showed that the indoxyl-acetate test was unsuitable for use. The USDA has developed a test for legume crops where the seed is immersed in a solution of 100 mg of indoxyl-acetate, 25 ml of ethanol, and 73 ml of distilled water. After the immersion, the seeds are exposed to ammonium hydroxide gas for one minute, which turns the cracked seeds blue (Waelti, 1967). A test has also been developed using 2,3,5-triphenyl-tetrazolium chloride, which is a chemical that is colorless, but is reduced to a red state by living cells. . For the tetrazolium test, the embryo is removed from the seed (except in corn) and then is stained with the tetrazolium solution. For corn, the kernels are soaked in water, preferably 8 over night, and are then cut longitudinally to bisect the embryo. One half of each kernel is placed in a Petri dish and covered with tetrazolium solution. After three to four hours, the viable portions of the kernel should be stained red (Lakon, 1949).

Water Absorption: vanUtrecht et al. (2000) soaked soybeans in a 1%sodium hypochlorite solution for ten minutes, which caused the damaged soybeans in the solution to swell, making the damage easier to detect. They reported that this test was the most appropriate method for determining damage for a study of storage deterioration when compared against colorimetric tests, the tetrazolium staining test, and the indoxyl- acetate staining test. The strength of the test was that it was able to indicate cracks in the soybeans, without indicating scratches.

Candling: Candling has been used largely to detect stress cracks in grain. In general, the grain is illuminated from underneath, allowing any internal cracks to appear as shadows in the grain. Brekke (1968) used this technique with corn, and Desikachar and

Subrahmanyan (1961) used this technique with rice. Stermer (1968) modified the technique slightly by using polarized light and taking still images of rice grains with a standard 3Smm camera. The damage level was determined by counting cracks in the rice grains using the developed photographs.

Germination Testing

Germination tests are often used to determine seed vigor in response to damage. In germination tests, a known number of seeds are planted in a controlled environment to see how many will germinate and grow. There are a number of variations in the parameters on the germination test depending on the application of the test. Kolganov (1958) used germination tests to test the effects of a dual cylinder threshing system on grain damage. The threshed grain was planted and used find the percent germination, percent germinative energy, percent emergence, and plant weight compared to conventionally threshed grain. 9

Clark et al. (1969) used a cold germination test to study the effect of high velocity impact on cottonseeds. For this germination test, the seeds were subjected to cycling temperatures of

16 hours at 20 °C and 8 hours at 30 °C for seven days. At the end of seven days, the seedlings were inspected for normal, secondary, and abnormal root systems. Another variation of the germination test is the acid germination test. For this test, the seeds are soaked in a sulfuric acid solution, rinsed, soaked in a calcium carbonate solution, rinsed again, and then planted. The fundamental idea behind this test is that the acid will penetrate any breaks in the seed, destroying the embryo, and therefore preventing germination. A seed with an intact coat will protect the embryo from the acid. Arnold (1964) used this variation of the germination test to test the effect of various combine operating parameters on damage in wheat and .

Light Analysis

Many researchers have chosen to evaluate grain and food quality and damage based on the interaction of the seed and various wavelengths of light. This past research has taken on many manifestations, afew of which are summarized here.

Colorimetric: Chowdhury (1977, 1978) used fast green FCF dye to stain damaged grain kernels, as described in the visual inspection method with green dye enhancement. After the kernels were rinsed, they were subjected to a NaOH extracting solution, which removes a portion of the dye from the damaged portion of the kernels and holds it in suspension. The extracting solution is then analyzed with a colorimeter to determine the amount of dye in the solution. The concentration of dye in solution was found to be linearly proportional to the damage level in the grain with r2 values of 0.98 for corn, 0.99 for sorghum, and 0.98 for wheat. This colorimetric test has been found to be inadequate for soybeans with a 1% indoxyl-acetate dye and 0.5% NaOH extracting solution (vanUtrecht et al., 2000). 10

Stress Distribution: Arnold and Roberts (1969) used a photoelastic bench to visualize stress distributions in the cross section of wheat grains. Using these stress distributions, they developed a numerical model to simulate the stress fields inside the kernel for various loadings. The researchers concluded that a symmetrical wheat grain would be able to tolerate higher loads than anon-symmetrical grain. This model could potentially be used to evaluate interactions between the crop and combine, but would not be practical for measuring damage levels.

Color Sorting: Sarkar and O'Brien (1975) used a color sorting technique to predict tomato grades. This technique used an apparatus consisting of a lamp to illuminate the sample tomato and phototransistors behind green and red filters. Light that passes through the tomato is collected by the phototransistors. Using this setup, the optical density ratio between the light intensity at the green filter and the red filter was calculated. This ratio was used to predict tomato grades. The results showed significant differences between good and green tomatoes, but were unable to distinguish between moldy and below well color tomatoes. The researchers conjectured that the separation between the results could be improved by increasing the resolution of the signal processing circuit and increasing the scanning area of the tomato. A color sorting system has also been developed to remove colored kernels from a stream of white rice, but this system does not attempt to assess the damage level of the rice grains (Yamashita, 1993).

Light Transmittance: Johnson (1960) explored various means of determining smut content in wheat, but did not attempt to determine a level of mechanical damage. The first method he explored was using transmitted light. In this method, the wheat sample was rinsed with warm agar-Tween-water solution. The solution was then decanted through a 70-mesh screen with 10 ml of warm water. The filtrate and the washings were brought to boiling, and 10 mg of Takadiastase was added after cooling to SO °C. This suspension was tested in a 11 colorimeter and the smut content was found to be related to the absorbance level at 525 nm with a correlation coefficient of 0.81.

Light Reflectance: Johnson (1960) continued his investigation into means of determining smut content in wheat by exploring light reflectance. In this method, filter paper from rinsing wheat samples was measured for reflectance at 540 nm. The reflectance reading is correlated to the smut content with a logarithmic fit and a correlation coefficient of -0.80.

Near Infrared: Many researchers have used Near Infrared (NIR) radiation to measure various aspects of grain quality. Johnson (1960) explored NIR absorption in his studies of smut content in wheat. In this NIR absorption method, a sample of wheat was exposed to NIR radiation at 800 and 930 nm. Smut on the wheat changed the ratio of the absorbed light at the two wavelengths, which could be measured using a smut meter, developed for this study. Using the smut meter, a logarithmic relationship was found between the NIR meter reading and the smut concentration in the wheat with a correlation coefficient of 0.85.

Johnson (1962) used NIR radiation to measure damage in corn. He showed that damaged corn samples have different NIR absorbance spectrums than those of undamaged samples. Before data collection, fines were removed from the samples, and a standard damage level was assigned to the various samples by visual inspection. Absorbance comparisons were based on measurements taken at 800 and 930 nm because of their distance from effects of the corn's color. The slope of the absorbance curve between these two points was determined and used to estimate the damage in the sample. Data was taken on 315 samples, and duplicate readings were within 5% of the average often readings. Comparing the slopes of the absorbance curves to the "standard" damage level resulted in a linear equation with a correlation coefficient of 0.90.

Internal Quality: Several researchers have used a combination of light reflectance and transmittance measurements to estimate the internal quality of a product (Ganssle and 12

Webster, 1973; Webster, 1975; Massie and Norris, 1975; Webster, 1981). Ganssle and

Webster (1973) report that reflectance and transmittance measurements are able to detect certain features such as water core in apples and hollow hearts in potatoes. While these methods have been used to estimate internal quality in some food products, no attempt was made to correlate the findings to mechanical damage in cereal grains.

Fluorescence: Fluorescence properties have been used to measure mechanical damage in corn. Christenbury and Buchele (1976, 1977) used corn artificially damaged by splitting the kernels through the embryo. The damaged kernels were mixed with undamaged kernels to form 50 g samples with 0, 20, 40, 60, 80, and 100% damage per weight basis. The samples were exposed to a solution of 8-anilino- l -naphthalene sulfonic acid for 2 minutes, rinsed twice with tap water, and dried by placing the grain on paper towels. The dried samples were ground using a Wiley mill using a No. 20 screen. Grinding the grain eliminates any effects due to the orientation of the grain or the damage, and reduces a three dimensional phenomena to two dimensions. The ground sample is placed in a 4 cm sample holder and the fluorescence sensor was adjusted for a field of view of 3.5 cm in diameter.

The acid forms a fluorescent bond with the proteins exposed in the broken portions of the kernel, which can be visibly measured. The results show a linear relationship between induced fluorescence and exposed internal surface area with an r2 value of 0.97.

Another study used ultraviolet light to induce fluorescence in a damaged grain sample

(Brizgis, 1986; Brizgis et al., 1987). The sample was contained in a box illuminated only by ultraviolet light, and was monitored by a video camera connected to a digitizing board in a computer. The ultraviolet light caused any exposed starch in the corn kernels to fluoresce, resulting in the emission of visible light, which was detectable by the video camera. The camera and digitizing board converted the image to 64 levels of gray, and an appropriate gray threshold was found to discriminate between the damaged and undamaged regions of the image. The number of "white" pixels below the threshold was counted and was well 13 correlated to the damage level as determined by hand counts. One problem with the device was that differences in starch level between samples affected the white threshold level. This variation in starch content could be caused by varietal differences between corn samples as well as the effects of the growing year on the corn. Surface properties of the corn also affected the device. If a particular variety was lighter or shinier, the system was harder to adjust. In addition, if a sample of grain was dusty or moldy, the mold and dust had a tendency to cover the starch, impeding the analysis. Overall, two years of tests showed that the image analysis system achieved the same result as visual inspection, but proved to be much faster. In fact, the image analyzer could process about six times more samples in a given time period than hand counting.

Laser Candling: Some methods have been developed to detect cracked rice grains using a laser for illumination, and photocells or photo detectors behind the grain to detect the light passing through the grain. Satake (1986) developed a method that detects the amount of light that passes through the kernel, and compares the measured amount to a known threshold for a good kernel. This technique is shown to work with a stream of single kernels, as well as a batch of kernels in a special recessed plate. Murata (1975) used a technique that detected the amount of light that was scattered by the cracks in the kernel. Using this technique allowed the researchers to constantly evaluate the amount of cracked rice in a sample.

Machine Vision

A number of studies have been conducted to attempt to measure crop quality with machine vision. While these studies have been successful in their individual respects, none of the techniques used a moving stream of grain for sampling, and none of the tests used a subsampling technique to measure the total amount of mechanical damage in a larger grain sample. 14

Rehkugler and Throop (1987) used acomputer-imaging algorithm to evaluate apples for surface blemishes such as bruising, scab, bird pecks, insect stings, and hail damage. The bruise area predicted by the computer was compared to the actual bruise area with correlations of 0.64 to 0.73. To discriminate between damage types, each type was assigned a grayscale threshold. Comparing the amount of the image at each grayscale level allowed the researchers to identify the various damage types.

Howarth and McClure (1987) used a computer vision system to calculate physical parameters of sweet potatoes, using steel plates of known size and shape to calibrate the system. The system attempted to find two-dimensional characteristics such as area, perimeter, maximum length, width, form factor, curvature, and circularity. Each of the measurements were compared against measured actual values with errors less than 10% for all measurements except curvature which had errors between 10% and 50%.

Endsley et al. (1987) used a computer vision system to evaluate the coverage of a chemical application to corn at various points in an auger. A fluorescent dye was used to simulate the chemical of interest for the tests. For each test, a sample of corn was selected for computer vision analysis at the discharge end of the auger. When the samples were placed in the computer vision system, any kernels exposed to the dye would fluoresce. To negate the effect of the inherent fluorescence in corn, grayscale images of unexposed corn kernels were used to set a grayscale threshold level for measurement. Any grayscale level beyond the threshold was defined as having dye applied.

Sasser et al. (1987) utilized a computer vision system to measure the amount of trash in cotton samples. The system used was a Motion Control Inc. Type 423 HVI Color/Trash

Meter. The meter scans a sample of ginned cotton pressed against an observation window.

The sample is illuminated by two incandescent lights, and a black and white television camera captures the observation window with an image of 203,000 pixels. Trash is identified by any pixel that has a reflectance signal 30%below the average light level reflected from 15 the sample. The amount of trash in the ginned cotton is quantified by comparing the number of "trash" pixels to the number of "non trash" pixels.

Gunasekaran et al. (1988) used a computer vision system to differentiate between damaged and moldy portions of corn and soybeans. The system used a camera and computer system to take a grayscale picture of a sample (either single or multiple kernels) and used a threshold reflectance value to convert the grayscale image into a black and white image representative of the damaged and undamaged portions of the kernel. This system used white light for illumination for the corn mechanical damage measurements, but used a red filter (610 nm) over the camera lens for the mold measurements. The system was 100% successful in finding broken corn kernels, 83% successful in finding chipped kernels, 88% successful in finding starch cracked kernels, 84% successful in finding moldy kernels, and

80% successful in finding mold damaged soybeans. Success was defined as whether the computer system correctly identified the damaged regions ofpre-selected corn kernels and soybeans. Although no attempt was made to use the images to estimate the total damage levels, the researchers stated that a pixel counting routine could be used to determine the total amount of damage in the sample as indicated by the machine.

Ng et al. (1998a) used a computer vision system to obtain an image of both sides of a corn kernel and classify areas of a kernel as mold damaged or non-mold damaged. The goal of the research was to develop a calibrated neural network to account for variability in the response of a computer vision system to varying lighting conditions. The system was successful in detecting percent mold coverage on a kernel more reliably than lab workers classifying kernels from the same images, although the machine vision and the human classifications were very similar. While this system obtained images of both sides of the corn kernel, only one side was considered at a time, and in order for the neural calibration system to work, the kernel had to be placed upon a previously calibrated background color. 16

Steenhoek et al. (2001 a, 2001b) developed a computer neural network image- processing algorithm to evaluate corn kernels for germ damage from heating, blue eye mold, and mold damage. Using validation data, the neural network was 75% accurate at predicting the type of damage, with the greatest error occurring as a misclassification between damage levels, not between damaged and sound kernels. Adding an additional decision layer increased the system accuracy to 95%, but it was noted that image quality was crucial to the success of the algorithm. The damage determination was made by converting the red green and blue components (RGB) of an image of a corn kernel into arbitrarily selected grayscale values based on the RGB levels attributable to the various types of damage and other factors.

Once the RGB image was converted to a grayscale image, the computer was able to count the pixels of each grayscale area to determine the amount of the kernel with that particular characteristic. Using this system, the computer was able to correctly identify 92% of the damaged kernels and 93% of the sound kernels.

Misra and Shyy (1994, 1995) used an imaging routine to determine the shape, roughness, size, texture, and color of pharmaceutical products and soybeans. If any of the parameters deviated signifMicantly from a predetermined level, the pill or soybean was separated into a reject bin.

Acoustic Methods

Various acoustic methods have been used to predict seed mass and damage as well as grain loss, including acoustic transmittance, impact force, and acoustic loss.

Acoustic Transmittance: Misra et al. (1990) conducted an investigation comparing the acoustic transmittance properties of "good" soybeans and "bad" soybeans. "Bad" soybeans were considered those that were small or shriveled, and "good" soybeans were all others. The investigation placed a soybean between two piezoelectric P-wave transducers.

One transducer was excited with a voltage spike, sending an acoustic pulse through the seed 17 and into the second transducer. An FFT of the frequencies transmitted and absorbed by good and bad seeds was compared to find a relative absorption spectrum for a bad soybean. The results showed that it is possible to compare good and bad soybeans using acoustic transmission data, but when experimenting with seeds from various lots, they found that the transmission and absorption spectra varied from soybean to soybean, and it would be difficult to quantify the differences in absorption mathematically. In addition, the data collection process was slow because each soybean had to be carefully placed between the transducer plates. As a result, further research on this method was abandoned.

Impact Force: Misra et al. (1990) also explored an impact force response analysis, where soybeans were dropped individually onto a piezoelectric force transducer attached to a data collection system operating at 200 kHz. To separate sensor characteristics from seed characteristics, the researchers dropped homogeneous nylon beads on the sensor, and used the resulting data to deconvolve the data obtained from soybean impacts. The deconvolved data showed trends depending on the quality of the soybeans. A dual Gaussian curve fitting procedure was written in FORTRAN to develop an equation for the frequency spectra of the soybeans. However, this was deemed too slow and the researchers moved on to using a

Taylor series approximation. Using the Taylor series technique, the mass of the soybeans was predicted with a standard error of 6.6%. Shriveled or damaged soybeans often impacted the sensor more than once, resulting in a large variation in the measurement of lower frequencies, which resulted in a larger error of fit to the soybean mass. Using the larger error evident in the mass fit of damaged soybeans, it was possible to classify a soybean as diseased or damaged if its mass was measured to be below 0.09 grams, or if the error of fit was greater than 10%. This technique was successful in finding damaged or diseased soybeans with only

5% error. Misra and Shyy (1994) coupled this technique with the previously described vision system to estimate the quality of soybeans. For the combined system, the mass of the 18 soybean was measured by the impact force method before the imaging system analysis. The overall results of the two analyses were used to determine whether to discard the soybean.

Acoustic Loss: Kirk (1977) developed an acoustic sensor with high and low frequency band pass filters and comparator circuitry to determine if a particle hitting the sensor is grain or chaff. Due to variations in frequencies produced by an impact of grain or chaff, the comparator circuitry is able to distinguish between impacts of chaff and grain to allow quantification of grain loss. Larson and Leonard (1987) used a piezoelectric crystal attached to a rectangular sounding board as a grain loss sensor. The crystal was connected to an analog signal conditioning circuit, along with a 555 timer to generate a pulse for every kernel that hit the sensor. This system was tested with 100 kernels of barley, and counted the correct number of pulses to within 10% of the expected value at impact rates up to 35 kernels per second. The grain was also mixed with chaff and straw to determine if the additional trash would record impacts, but the sensor maintained its reliability in the presence of other crop material.

Electrical Methods

Another method previously used to measure grain damage is through the measurement of the electrical properties of the grain. Methods of measuring grain damage using electricity fall into the measurement of conductivity, dielectric properties, and resistance and capacitance.

Conductivity: Couto et al. (1998) measured damage to soybeans by measuring the conductivity of a mixture of distilled water and soybean samples. For the study, soybeans were artificially damaged by splitting the soybean in half with a razor, or by dropping a mass a known distance on to a group of beans. The artificially damaged beans were mixed with undamaged beans to create known proportions of damaged samples. The samples were immersed in distilled water, and the electrical conductivity of the solution was measured at 19 twenty-minute intervals. The researchers found that by agitating the solution, the conductivity values increased, allowing the soaking time required to differentiate the damage levels to be reduced. The results of the study show that for one soybean variety, the conductivity was linear with respect to the damage level, and for another variety, the relationship with damage level was quadratic.

Resistance and Capacitance: Holaday (1964) used three capacitance and three resistance readings from a sample of corn to predict the amount of drying damage in the sample. These readings from a well mixed 250 gram sample of corn were averaged and plotted on a semi-log graph. For undamaged samples between 10 and 20% moisture, the plot of resistance vs. capacitance was linear on semi log graph paper with a correlation of 0.998.

Samples damaged by drying were displaced from the regression line, and it was determined that the amount of displacement from the regression line of the undamaged samples was dependent on the degree of drying damage.

Dielectric Properties: Nelson (1987) measured the dielectric properties of spring barley, spring , hardy winter barley, semi hardy winter barley, soft red winter wheat, winter , and soybeans as a function of moisture, bulk density and sampling frequency.

The dielectric constants were repeatable in nature, and could be expressed as a quadratic or cubic model with similar error over a frequency range of 20 to 2450 MHz. Al-Mahasneh

(2001) used measurements of dielectric properties of corn samples at oscillation frequencies from 10 Hz to 13 MHz to measure mechanical damage, moisture, and bulk density. The dielectric properties were related to artificial and combine induced mechanical damage as indicated by visual inspection and the Chowdhury colorimetric damage test. The results showed that measurement frequencies less than 100 kHz showed good potential for the development of a mechanical damage sensor. However, moisture content and bulk density had a much larger effect on the dielectric properties of corn than damage, requiring a compensation for these two factors before a damage level can be evaluated. 20

Chemical Methods

A number of chemical methods have also been used to measure damage in grain.

Some of these include the measurement of carbon dioxide (CO2) production and tests for the quantity of free fatty acids.

CO2 Production: Steele (1967) found that production of CO2, a measure of grain deterioration by rate of mold respiration, is influenced by mechanical damage. His basis for comparison was the amount of respiration required to cause a given amount of dry matter loss in a sample. While his investigations into mechanical damage were confounded by other factors, he found consistent results verifying the effect of mechanical damage on the production of CO2. He found that combine shelled corn deteriorated 2 to 3 times faster than hand shelled corn of the same variety and year. While his tests provided positive results, his tests simulated conditions found above the drying layer in a grain storage system, not a harvesting system. In addition, this method of measurement requires special equipment and significant amounts of time (in some cases more than 500 hours) to collect appropriate data, making it inappropriate for use on a harvester. Ng Et al. (1998b) measured CO2 production in stored corn to estimate dry matter loss as a function of mechanical damage. Samples of various damage levels (0-50%) were created by blending damaged and undamaged kernels selected from combine-shelled corn. Their results show that mechanical damage is a good indicator of the rate of dry matter loss, and as a result, an estimator of allowable storage time.

For their analysis, damage as measured by a machine vision system provided the best regression vs. the mechanical damage multiplier for the CO2 production when compared against damage as measured by visual inspection, and damage as measured by the Chowdhury colorimetric test.

Fat Acidity: Baker et al. (1959) measured the content of free fatty acids in 500 samples of various grains and attempted to correlate it to various types of damage, including 21 field damage (immaturity, weevil, frost, etc.) and storage damage (rancid grain, heating, etc.).

The results found good correlations between the content of free fatty acids and the amount of storage damage in the grain. However, correlations between free fatty acid levels and field damage were not as good. No attempt was made to correlate free fatty acid content to mechanical damage, possibly because this study was undertaken before field shellers became popular.

Mechanical Damage Index

Chowdhury and Buchele (1976) developed a damage index to describe grain damage on a scale from 10 (the entire lot consists of sound kernels) to 100 (the entire lot consists of

BCFM). The damage index accounts for various levels of grain damage, including BCFM, severe damage, major damage, minor damage, and whole kernels. The various classifications of kernel damage were achieved by visual inspection enhanced by green dye.

The various classifications are defined as: D1 =broken kernels and fine material that passed through 4.76mm round hole sieve, D2 =severe damage —broken, chipped, and crushed kernels (more than 1/3 of the whole kernel is missing), D3 =Major damage —open cracks, chipped kernels, and severe pericarp damage, D4 =Minor damage —kernels with hairline cracks and spots of pericarp missing, and DS =whole kernels —kernels that did not absorb dye on any part except root tip. These damage categories were each assigned a weighting factor as determined by a germination test. When the various damage categories were subjected to a germination test, the percentage ofnon-germinating kernels in each category was divided by ten to provide a D factor for that damage level. For example, the severe damage had only 5% germination, leaving 95% of the seeds ungerminated, and a D2 value of

9.5. The amount of each type of damage in the sample was also given a d value based on the percent of the sample falling into that category by weight. The resulting equation for the damage index is: D.I. _ (Dldl+DZd2+D3d3+D4d4+DSd5)/10. The results of the investigation 22 showed that the level of BCFM is small in comparison to the level of total damage. The highest BCFM measurement was less than 1%, while total damage was near 18% for kernel moisture content of approximately 29%. The damage index value closely followed the amount of total damage across moisture levels, while taking into account the various proportions of damage levels. The researchers concluded that the multipliers (D values) for the damage index could be derived from various measures of grain damage, including CO2 production.

Rheological Methods

Mahmoud (1972) conducted asmall-scale unpublished experiment testing the coefficient of restitution of corn as an indicator of damage and moisture. Single seeds were dropped on an inclined plate, and a box with three compartments was provided for the seeds to drop in. It was observed that the sound kernels landed farther from the plate than the damaged kernels. He reported that the separation was not efficient, but it merited further study. In addition, Mahmoud investigated using changes in bulk density and strain during loading, measuring compressive energy, and time of relaxation to estimate damage levels.

He found that measuring the compressive energy and time of relaxation to be the most promising rheological methods of measuring damage in shelled corn.

X-Ray Methods

X-ray radiography has been utilized to find internal stress cracks in wheat. Chung and Converse (1968) used radiographs to study internal cracking in wheat based on factors of harvest method (hand vs. combine), variety, location, year, plus any factor interactions.

Milner and Shellenberger (1953) used radiographs of wheat to find internal fissuring of wheat grains. The study intended to find the environmental effects that cause fissuring in wheat, and what effect the fissuring has on the physical properties of the wheat itself. The 23 radiographs were used primarily to detect which wheat kernels were damaged. The study found that the radiographic technique is limited by the fact that it can only detect internal flaws of a certain size, based on the ratio of the size of the fissure to the diameter of the kernel. In this study, it was only possible to find fissures larger than 2% of the kernel diameter.

Breakage Testing Breakage testers have been used to determine how susceptible a lot of grain is to further breakage (McGinty and Kline, 1972; Finner and Singh, 1983). While these testers are unable to determine the amount of damage in a sample, they are indicative of the amount of breakage that a sample of grain will experience due to further handling and shipping.

Aspirator Separation

The flow of air is used in a combine cleaning system to separate material other than grain from the grain itself. This technique has been used in the laboratory as well. Al-Yahya et al. (1991) used a Kice Model 6DT4 Mini-Aspirator to find the amount of fines that were separated from a corn sample using various airspeeds. It found that removal efficiency for all sizes of corn fines increased as air velocity increased, but an increasing amount of whole corn was removed with increasing airspeed. About 98% of FM (material passing through a 2.4 mm sieve), 67% of BC (Broken Corn)+FM (material passing through a 4.8 mm sieve) and 39% of LB (Large Brokens)+BC+FM (material passing through a 6.4mm sieve) was removed without great amounts of whole corn being removed at an airspeed of about 13 m/s.

Control Methods

While a relatively large amount .of research has gone into determining techniques to measure grain damage, little has been published on the use of grain properties as an input to a 24 control system. Misra and Shyy (1991) automated the operation of an air screen seed cleaner by monitoring the amount of fine material being removed by the cleaning operation and adjusting the machine parameters accordingly to obtain the highest cleaning efficiency.

DePauw and Staiert (1982) developed a sensor and control system to monitor and control the speed of the threshing rotor of an Axial Flow combine by measuring the amount of damage in the harvested grain. The goal of the system- was to minimize grain damage while maximizing harvest rate. Their desire was to have a system that would not be affected by crop variety, moisture content, crop toughness, or density. The system was designed to minimize power consumption by operating the rotor at the maximum acceptable speed for a particular grain damage level. The sensor worked by delivering a known amount of grain onto a set of sieves. Material that passed through the first sieve, but which remained on the second sieve is directed towards an impact sensor. The first sieve retained whole kernels, allowing fines and broken kernels to pass through, and the second sieve retained the broken kernels, but allowed fines to pass through. Therefore, broken grain was measured, but fines and chaff were not. Control circuitry was used to control the rotor speed in response to the sensor reading. The overall system operated by having the combine operator use a dial to determine an allowable damage set point for the crop being harvested. If the amount of damaged grain was greater than the set point, the control system slowed the rotor speed, if the damaged grain was below the set point, the control system increased the rotor speed.

This allowed the rotor to run at a maximum speed allowable for a given amount of damage.

Damage Measurement Comparisons

While there is a relatively large amount of information regarding the benefits and drawbacks of particular techniques for measuring grain damage, little has been done to quantitatively compare the various methods. As previously discussed, Ng et al. (1998b) found that mechanical damage is a good indicator of the allowable storage time for combine- 25 shelled corn. Brass (1970) conduced a review of many various damage measurement techniques, and concluded that using a visual inspection with Fast Green FCF dye was the best method to evaluate the damage characteristics of a new design of shelling cylinder. In addition, he conducted a study trying to relate various damage types (severe, BCFM, etc) to total amount of damage, but met with limited results. The only significant r-value relating

BCFM to total damage was 0.37, and the significant r-values for obvious damage (kernels that are easily recognizable as being broken) were only 0.65 and 0.36. While there does appear to be a correlation, only 13-42% of the variability in damage is accounted for by these relationships in his tests. He concluded that measuring BCFM or severely broken kernels is not a reliable method of measuring total damage.

The dearth of studies attempting to relate damage measurement methods clouds the issue of grain damage measurement. By not having an accepted standard to accurately define the amount of damage in grain, none of the studies on measurement techniques can be adequately compared. This leads to interest in developing a measurement method that can correlate to multiple types of damage measurement techniques.

Damage Measurement Design Parameters

Chowdhury (1978) came to the same conclusion regarding grain damage measurement. He provided a detailed review of various techniques for measuring grain damage or quality, and concluded that none of the available methods were fast enough, accurate enough, or free enough from human judgment to be satisfactory for measuring mechanical damage in grain. He suggested some parameters for the design of a grain damage meter. They are:

1. The system must be applicable to all cereal grains and legumes, and must be able to deal with varietal differences within one type of grain. 26

2. The system must be able to account for grain moisture content. Therefore, the output must be either independent from, or a function of, moisture. 3. Due to differences between grain types, the technique must be independent of grain constituent content or kernel size and shape. 4. The sample size must be large enough to account for the inherent variation in grains, as well as to be able to reduce sampling error. The meter must also be able to accommodate various sample sizes for different grains.

5. Since grain is harvested over a wide range of temperatures, the test must be independent of temperature, or have an appropriate correction factor.

6. The time it takes to run a test should be as fast as possible while retaining accuracy. Ideally, the results of the test would be obtainable in 2 to 3 minutes. 7. The test must retain accuracy, and since no "standard" exists, an arbitrary scale or index must be developed for the meter. 8. The test must be free of human judgment factors. Overall, Chowdhury provided a complete list of parameters for a technique to measure grain damage. However, when considering the development of a grain damage sensor for a combine harvester, some modifications to this list should be made. Ideally, the system should be able to continuously measure a flowing stream of grain, or subsample a grain flow with results available in less than 20 seconds, rather than the 2 to 3 minutes suggested by

Chowdhury. In addition, the test should not require expendables such as chemical dyes, water, or photographic film. Finally, while the test does not have to have an arbitrary scale, the sensor display should be easily understandable by a typical combine operator, and should be reasonably priced. 27

References

Al-Mahasneh, M.A. 2001. Using radio frequency spectral measurements for determination of corn mechanical damage. Unpublished Ph. D. Thesis, Library, Iowa State University, Ames, Iowa.

Al-Yahya, S.A., C.J. Bern, and C.R. Hurburgh, Jr. 1991. Aspirator separation of corn-fines mixtures. Transactions of the ASAE 34(3): 944-949.

Arnold, R.E. 1964. Experiments with rasp bar threshing drums. Journal of Agricultural Engineering Research 9:93-131.

Arnold, P.C. and A.W. Roberts. 1969. An investigation of stress fields in wheat grains, using photo-elastic and numerical techniques. Journal of Agricultural Engineering Research 14(2): 126-133.

Ag Leader. 2002. Ag Leader Technology: Company Profile. http://v~►~wvv.agleader.com/profile-history.htm. Accessed Apri17, 2002.

ASAE Standards. 45th Edition, 1998. Grain harvest damage, St. Joseph, Michigan: ASAE.

Baker, D., M.H. Neustadt and L. Zeleny. 1959. Relationships between fat acidity values and types of damage in grain. Cereal Chemistry 36(3): 308-311.

Bern, C.J. and C.R. Hurburgh, Jr. 1992. Characteristics of fines in corn: review and analysis. Transactions of the ASAE 35(6): 1859-1867.

Brass, R.W. 1970. Development of a low damage corn shelling cylinder. Unpublished M.S. Thesis. Library, Iowa State University, Ames, Iowa.

Brekke, O.L. 1968. Corn dry-milling: stress crack formation in tempering of low moisture corn, and effect on degerminator performance. Cereal Chemistry 45(4): 291-303.

Brizgis, L.J. 1986. Image analysis system for measuring mechanical damage of corn. SAE Paper No. 861456.

Brizgis, L.J., D.B. Keleher, and V.D. Bandelow. 1987. Grain damage analyzer. U.S. Patent Number 4,713,781.

Case IH. 2002. Case IH: Products: Precision Farming: AFS —Advanced Farming Systems. http://v~►~►~vw.caseih. com/products/series.asp?Reg=NA&RL=ENNA&id=1962&mod=tr ue. Accessed April 7, 2002. 28

Chowdhury, M.H., and W.F. Buchele. 1975. Effects of the operating parameters of the rubber roller Sheller. Transactions of the ASAE 18(3): 482-486, 490.

Chowdhury, M.H. and W.F. Buchele. 1976. Development of a numerical damage index for critical evaluation of grain damage. Transactions of the ASAE 19(3): 428-432.

Chowdhury, M. H. 1977. Method of measuring mechanical damage to grain. U.S. Patent Number 4,020,682.

Chowdhury, M.H. 1978. Development of a colorimetric technique for measuring mechanical damage of grain. Unpublished Ph.D. Thesis. Library, Iowa State University, Ames, Iowa.

Christenbury, G.D., and W.F. Buchele. 1976. Method of measuring damage to grain. U.S. Patent Number 4,000,975.

Christenbury, G.D., and W.F. Buchele. 1977. Photoelectric system for measuring mechanical damage of corn. Transactions of the ASAE 20(5): 972-975.

Chung, D.S., and H.H. Converse. 1968. Internal damage of wheat by radiographical examination. ASAE Grain Damage Symposium. Agricultural Engineering Department, Iowa State University, Ames, Iowa.

Clark, R.L., G.B. Welch, and J.H. Anderson. 1969. Effect of high velocity impact on germination and crackage of cottonseed. Transactions of the ASAE 12: 748-751.

Couto, S.M., M.A. Silva, and A.J. Regazzi. 1998. An electrical conductivity method suitable for quantitative mechanical damage evaluation. Transactions of the ASAE 41(2): 421-426.

DePauw, R.A. and Staiert, R.W., 1982. Crop damage responsive control of rotor speed. U.S. Patent Number 4,348,855.

Desikachar, H.S.R. and V. Subrahmanyan. 1961. The formation of cracks in rice during wetting and its effect on the cooking characteristics of the cereal. Cereal Chemistry 38(4): 356-364.

Dodds, W. 1972. Costs of mechanical damage in shelled corn at grain terminals. ASAE Grain Damage Symposium. Agricultural Engineering Department, Ohio State University, Columbus, Ohio. pp. 29-32.

Endsley, J.C., J.F. Reid, and L.E. Bode. 1987. Measuring uniformity of coverage in auger application of fungicides. ASAE Paper No. 87-1604. 29

Finner, M.F. and S. Singh. 1983. Apparatus for testing grains for resistance to damage. U.S. Patent Number 4,422,319.

Fox, R.E. 1969. Development of a compression type corn threshing cylinder. Unpublished M.S. Thesis. Library, Iowa State University, Ames, Iowa

Freeman, J.E. 1972. Damage factors which affect the value of corn for wet milling. ASAE Grain Damage Symposium. Agricultural Engineering Department, Ohio State University, Columbus, Ohio. pp. 49-52

Ganssle, E.R., and D.R. Webster. 1973. Optical internal quality analyzer. U.S. Patent Number 3,765,775.

Gunasekaran, S., T.M. Cooper, and A.J. Berlarge. 1988. Evaluating quality factors of corn and soybeans using a computer vision system. Transactions of the ASAE 31(4): 1264-1271.

Holaday, C.H. 1964. An electronic method for the measurement of heat damage in artificially dried corn. Cereal Chemistry 41(6): 533-542.

Howarth, M.S. and W.F. McClure. 1987. Agricultural product analysis by computer vision. ASAE Paper No. 87-3043.

John Deere. 2002. John Deere Ag — Ag Management Solutions. http://customer.]ohndeere.com/ag/servicesupport/ams/index.html?currState=1111111 1000000000000000000. Accessed Apri17, 2002.

Johnson, R.M. 1960. Five proposed methods for determining smut content in wheat. Cereal Chemistry 37(3): 289-308.

Johnson, R.M. 1962. Determining damage in yellow corn. Cereal Science Today (1): 14- 15.

Kirk, T.G. 1977. Acoustic grain flow rate monitor. U.S. Patent Number 4,004,289.

Kline, G.L. 1972. Mechanical damage to corn during harvest and drying. ASAE Grain Damage Symposium. Agricultural Engineering Department, Ohio State University, Columbus, Ohio. pp. 79-82.

Kolganov, K.G. 1958. Mechanical damage to grain during the threshing (Russian Translation). Journal of Agricultural Engineering Research 3:179-184.

Lakon, G. 1949. The topographical tetrazolium method for determining the germinating capacity of seeds. Plant Physiology 24(3): 389-393. 30

Larson, R.G. and J.J. Leonard. 1987. Microprocessor-based monitoring of particle impacts on a grain loss sensor. ASAE Paper No. 87-3512.

Mahmoud, A.R. 1972. Distribution of damage in maize combine cylinder and relationship between physics — rheological properties of shelled grain and damage. Unpublished PH. D. thesis. Library, Iowa State University, Ames, Iowa.

Mahmoud, A.R. and W.F. Buchele. 1975. Distribution of shelled corn throughput and mechanical damage in a combine cylinder. Transactions of the ASAE 18(3): 448- 452.

Massie, D.R., and K.H. Norris. 1975. A high intensity spectrophotometer interfaced with a computer for food quality measurement. Transactions of the ASAE 18(1): 173-176.

Mayes, D.M. 2000. Grain quality monitor. U.S. Patent no. 6,100,526.

McGinty, R.J., and G.L. Kline. 1972. Development of a standard grain breakage test. ASAE Grain Damage Symposium. Agricultural Engineering Department, Ohio State University, Columbus, Ohio. pp. 185-186.

Milner, M., and J.A. Shellenberger. 1953. Physical properties of weathered wheat in relation to internal fissuring detected radiographically. Cereal Chemistry. 30: 202- 212.

Misra, M.K, B. Koerner, A. Pate, and C.P. Burher. 1990. Acoustic properties of soybeans. Transactions of the ASAE 33(2): 671-677.

Misra, M.K. and Y.Y Shyy. 1991. Automation ofair-screen seed cleaner. U.S. Patent Number 4,991,721.

Misra, M.K. and Y.Y. Shyy. 1994. Acoustic and video imaging system for quality determination of agricultural products. U.S. Patent Number 5,309,374.

Misra, M.K. and Y.Y. Shyy. 1995. Acoustic and video imaging system for quality determination of pharmaceutical products. U.S. Patent Number 5,422,831.

Murata, N. 1975. Method and apparatus for detecting cracks in unhulled grains. U.S. Patent Number 3,871,774.

Nelson, S.O. 1987. Frequency, moisture, and density dependence of the dielectric Properties of small grains and soybeans. ASAE Paper No. 87-6059.

Ng, H.F., W.F. Wilcke, R.V. Morey, and J.P. Lang. 1998a. Machine vision color calibration in assessing corn kernel damage. Transactions of the ASAE 41(3): 727-732. 31

Ng, H.F., W.F. Wilcke, R.V. Morey, R.A. Meronuck, and J.P. Lang. 1998b. Mechanical damage and corn storability. Transactions of the ASAE 41(4): 1095-1100.

Quick, G.R. 2002. Personal communication.

Rehkugler, G.E. and J.A. Throop, 1987. Image processing algorithm for apple defect detection. ASAE Paper No. 87-3041.

Roberts, H.J. 1972. Corn damage and its effect on dry milling. ASAE Grain Damage Symposium. Agricultural Engineering Department, Ohio State University, Columbus, Ohio. pp. 37-48.

Sarkar, S.C., and M. O'Brien. 1975. Measurement of power spectra for optoelectric sorting of tomatoes. Transactions of the ASAE 18(1): 177-180, 184.

Sasser, P., I.Hurst, D. Hinkle, and F. Shofner. 1987. An objective measurement of neps in raw cotton. ASAE Paper No. 87-1091.

Satake, T. 1986. Apparatus for detecting cracked rice grain. U.S. Patent Number 4,572,666.

Saul R.A. and J.L. Steele. 1966. Why damaged shelled corn costs more to dry. Agricultural Engineering 47(6): 326-329, 337.

Singh, V., N.L. Barreiro, J. McKinstry, P. Buriak, and S.R. Eckhoff. 1997. Effect of kernel size, location, and type of damage on popping characteristics of popcorn. Cereal Chemistry 74(5): 672-675.

Steele, J.L. 1967. Deterioration of damaged shelled corn as measured by carbon dioxide production. Unpublished Ph.D. thesis. Library, Iowa State University, Ames, Iowa.

Steenhoek, L.W., M.K. Misra, W.D. Batchelor, J.L. Davidson. 2001 a. Probabilistic neural networks for segmentation of features in corn kernel images. Applied Engineering in Agriculture 17(2): 225-234.

Steenhoek, L.W., M.K. Misra, C.R. Hurburgh Jr., and C.J. Bern. 2001b. Implementing a computer vision system for corn kernel damage evaluation. Applied Engineering in Agriculture 17(2): 235-240.

Stermer, R.A. 1968. Environmental conditions and stress cracks in milled rice. Cereal Chemistry 45(4): 365-373.

Uhrig, J.W. 1968. Economic losses of damaged grain. ASAE Grain Damage Symposium. Agricultural Engineering Department, Iowa State University, Ames, Iowa. 32

USDA, 1996. United States standards for corn. vv~ww.usda.gov/gipsa/reference-library/standards/810corn.pdf. Accessed April 10, 1002.

USDA, 1997. Federal grain inspection handbook, Book 2. pp. 4-19 — 4-21.

VanUtrecht, D, C.J. Bern, and I.H. Runkunudin. 2000. Soybean mechanical damage detection. Journal of Applied Engineering in Agriculture 16(2): 137-141.

VanWormer, M. 1972. Corn damage and its effect on feed manufacturing. ASAE Grain Damage Symposium. Agricultural Engineering Department, Ohlo State University, Columbus, Ohio. pp. 33-36.

Waelti, H. 1967. Physical properties and morphological characteristics of maize and their influence on threshing injury of kernels. Unpublished Ph.D. thesis. Library, Iowa State University, Ames, Iowa.

Wang D. and S.R. Eckhoff. 2000. Effect of broken corn levels on water absorption and steepwater characteristics. Cereal Chemistry 77(5): 525-528.

Webster, D.R. 1975. Optical analyzer for agricultural products. U.S. Patent Number 3,861,788.

Webster, D.R. 1981. Grain quality analyzer. U.S. Patent Number 4,260,262.

Yamashita, R. 1993. New technology in grain postharvesting. Farm Machinery Industrial Research Corp: Tokyo, Japan. 33

CHAPTER TWO. AIRFLOW SEPARATION OF DAMAGED CORN

A paper drafted for submission to Applied Engineering in Agriculture

M.A. Brands, G.R. Quick2, C.J. Bern3, S. J. Birre114, D.S. Nettleton5

Abstract

A method to measure the quantity of mechanically damaged grain in a sample by removing a portion of a stream of falling grain with a transverse airflow was investigated.

The amount of grain removed from the stream was collected and compared to the total amount of grain in the sample and expressed as a percent weight separated. While testing corn with moisture contents of 20 to 28% and damage levels created by shelling the grain by hand, as well as two combine cylinder speeds, one experimental configuration was found to distinguish damage levels while correlating well with three common damage tests. This configuration had r2 values of 0.879, 0.865, and 0.820 when compared to the USDA test for

Broken Corn and Foreign Material (BCFM), unaided visual inspection, and visual inspection aided by staining with fast green FCF dye, respectively. Further laboratory tests with other grains, as well as field tests with various grains, are required to further establish the suitability of this approach to grain damage measurement.

Introduction

Mechanical damage can be defined as damage inflicted upon grain by harvesting and handling equipment. This damage is often characterized by broken, cracked, split, and

1 Graduate student, Agricultural and Biosystems Engineering Department, Iowa State University, Ames, Iowa. 2 Adjunct professor, Agricultural and Biosystems Engineering Depar t~lient, Iowa State University, Ames, Iowa. 3 Professor, Agricultural and Biosystems Engineering Department, Iowa State University, Ames, Iowa. 4 Assistant professor, Agricultural and Biosystems Engineering Department, Iowa State University, Ames, Iowa 5 Assistant professor, Department of Statistics, Iowa State University 34 scuffed kernels. Mechanical damage of cereal grains interferes with handling, storage, processing, and end use of the grain. Damaged grain is a financial burden on farmers through molding and deterioration, which reduce the quality of the grain crop (Saul and Steele, 1966;

Steele, 1967), and through increased input costs for drying (Bern and Hurburgh, 1992). In addition to the financial burden to the farmer, mechanically damaged grain can impede processing (Freeman, 1972; VanWormer, 1972; Roberts, 1972; Wang and Eckhoff, 2000), handling and transport (Dodds, 1972), as well as food uses (Singh et al., 1997).

The quality of any grain peaks in the field before harvest; harvesting and subsequent handling reduce overall grain quality. Combine harvesters cause damage, and harvester settings affect the amount of mechanical grain damage (Fox, 1969; Mahmoud and Buchele, 1975; Quick, 2002). Currently, machine operators have no objective feedback mechanism to relay the amount of damaged grain passing through a combine in real-time. Machine settings are usually changed to obtain the lowest level of grain damage based on visual inspection of bulk grain collecting in the combine hopper. To obtain a more objective measurement of grain damage in a combine, it is desirable to develop a method for monitoring grain damage at or near real-time. This feedback would provide a harvester operator with a consistent, objective indicator to use in making decisions regarding machine settings, allowing the operator to minimize the amount of harvest grain damage.

The objectives of this study were to develop a test stand to investigate a method to measure damaged corn by removing the damaged portion of a stream of falling grain with a transverse flow of air and to correlate the test stand response to the amount of damage in the grain sample as measured by four common damage tests. 35

Materials and Methods Test Stand Description The test stand in this study used a metering device to drop grain at a constant rate into

a rectangular drop chute where it encountered a stream of air from a fan, causing a portion of

the damaged grain to cross a barrier wall into a second drop chute. The grain collected at the

base of each chute was weighed to find the total mass of the sample, as well as the amount of

grain separated by the device. The test stand is shown in Figure 2.1.

For this study, the moisture meter from the John Deere GreenStar system (John Deere

part number AH167407), which has its own sampling and grain metering system, was used to

control grain flow. The moisture measurement capabilities of the meter were not used, but

the paddlewheel for returning grain to the clean of the combine was used to

meter the grain into the test stand. An input of 12 vDC caused the wheel to turn at a rate of

15 revolutions per minute (RPM), resulting in a grain delivery rate of approximately 10 g/s.

The moisture meter dropped the grain into a primary chute with a cross section of 108 mm x

108 mm and a height of 940 mm. The primary chute was attached to a secondary chute with the same cross section and a height of 781 mm. The secondary chute was closed at the top with a wire screen to prevent grain particles from escaping. This screen is shown in Figure

2.2. The primary and secondary chutes were separated by a partition with three slotted openings, allowing various inserts, with dimensions of 108 mm x 136.5 mm, to be placed between the primary and secondary chutes. These inserts permit changing the characteristics of the grain components allowed to pass into the secondary chute. Two inserts were solid and one insert had a pattern identical to that of the 4.76 mm round hole sieve specified by the

USDA for Broken Corn and Foreign Material (BCFM) measurement in corn. These inserts are shown in one test stand configuration in Figure 2.3. The test stand was configured so that the airflow developed by the fan could be directed at 90 or 150 degrees in relation to the flow 36 of grain, and that the grain would encounter the air stream at approximately the level of the middle insert location, or 483 mm below the discharge of the moisture meter.

The length of the fan ducts was determined by the necessary length to establish fully developed flow with the fan being used. This length was determined empirically using a pitot tube and manometer to measure airflow in a cardboard duct that was shortened by 152.4 mm between airflow measurements. The shortest duct that allowed for fully developed flow was found to be approximately 760 mm. The airflow in this investigation was produced by a centrifugal fan 63.5 mm wide with a 127 mm diameter and a 121mm x 89 mm rectangular discharge. The fan was directly connected to the output shaft of an electric motor rated at 750 watts and 3450 RPM.

Test stand configurations were varied by changing the inserts between the primary and secondary chutes, airspeed, and duct angle. Varying inserts altered airflow characteristics enough to change the maximum airflow available from the fan between configurations. As a result, the airflow rate for each insert configuration is expressed as a percentage of the maximum airflow possible for that configuration. The maximum airflow for each configuration was measured with an Omega HH-600 series anemometer. Table 2.1 defines the various insert configurations and gives the corresponding maximum air velocity for each configuration.

Sample Preparation

Corn samples were prepared using a mixture of two Golden Harvest varieties grown near Nevada, Iowa, during the 2001 crop season. The corn was harvested on the ear in the fall of 2001 and stored until January 2002 at which time it was shelled at approximately 15 moisture content by a laboratory sheller using the cylinder, concave, and beater assembly from a John Deere 6600 combine. The cylinder was fed by placing ears on a rubber belt conveyor that emptied into the cylinder at the same location as the original feederhouse. The 37 front concave clearance was set at 38 mm, and the rear clearance was set at 21 mm for all cylinder speeds. A high damage level was created by operating the cylinder at 508 RPM. A mid damage level was created by operating the combine cylinder at 238 RPM for a pilot study and 318 RPM for the major study. A low damage level was created by hand shelling the corn. From hereon, the damage levels will be referred to by the shelling methods: "hand shelled," "slow cylinder," and "fast cylinder." To ensure sample consistency, each damage level was screened for fines using a Carter Day model XT3 dockage tester with a 4.76 mm round hole sieve in place. The fines for each damage level were collected separately and later evenly redistributed among the damage samples within that damage level.

To test for the effect of moisture on the test stand response, corn samples were rewetted to higher moistures. A pilot study was conducted with the grain at shelling moisture, and the major study was conducted with the grain rewetted to moisture contents of approximately 21 %, 23%, and 28%. These moisture contents are referred to as "low,"

"medium," and "high." The corn was rewetted by spraying distilled water from a 470 ml household spray bottle onto individual batches of approximately 8 kg of corn each. The rewetted corn was stored between 0 and 5 degrees Celsius for 12-24 hours to allow the individual batches to come to equilibrium. The batches were rewetted in stages, with each stage increasing the moisture content of the batch no more than 6 percentage points. When the individual batches reached the desired moisture content, they were recombined to reform the whole lot. The recombined lot was stored between 0 and 5 degrees Celsius for a minimum of 24 hours to allow it to equilibrate. Following this storage, the corn was bagged in 3 kg sample sizes and refrigerated until testing took place.

The fines collected from each sample with the dockage tester were rewetted using the same procedure as the corn samples. After rewetting, the fines for each damage level were weighed and divided so that each 3 kg sample of corn within that damage level would 38 contain an equal mass of fines. The mass of fines added to each sample is summarized in Table 2.2, with each measurement representing the rewetted mass.

Experimental Design The airflow test stand was first operated with corn at shelling moisture and with various test stand configurations as variables to determine the most promising configurations for further study. In the major study, test stand parameters were fixed to evaluate damage and moisture effects. Responses were compared to four common damage tests: the USDA test for BCFM, unaided visual inspection, visual inspection aided by fast green FCF dye, and the Chowdhury colorimetric test. A suitable response from the test stand showed significant differences between mean responses at the three damage levels, and showed a strong correlation between the test stand response and the response of the common tests.

The test stand variables investigated in the pilot study included duct angle (2 levels), insert configuration (3 levels within each duct angle), and airflow rate (3 levels within each combination of duct angle and insert configuration). Each combination of test stand variables was subjected to five replications of each damage level, resulting in the collection of 270 data points. The goal of the pilot study was to identify the best test stand configurations and not to optimize the test stand settings. Therefore, each combination of duct angle, insert configuration, and airflow rate was analyzed independently for suitable response characteristics.

The pilot study resulted in three test stand configurations (combinations of duct angle, insert configuration, and airflow rate) showing suitable responses. These test stand configurations were investigated further in the major study.

Test Procedure For each test, one corn sample was randomly selected from the appropriate lot, and one fines sample was selected from the corresponding lot. The corn and fines samples were 39 emptied into a container and briefly mixed together by hand. The mixed sample was loaded in the moisture meter at the top of the test stand, and the airflow speed was selected by setting the fan voltage with a variable transformer. The test process consisted of switching on the fan and the moisture meter paddlewheel, allowing the grain to drop into the air stream, separate, and collect in the bins below. When the moisture meter had completely emptied, the paddlewheel and the fan were switched off, and the gross mass of the bins was recorded.

After each test, the collection bins were emptied, and a tare mass was recorded before the next test.

Common Tests In addition to being able to accurately determine the damage level in a sample of grain, the test stand needs to be able to display the results of the measurement in an understandable manner. Due to the lack of awell-defined standard for accurately expressing the amount of mechanical damage in a grain sample, this study attempted to correlate the output of the test stand to four common grain damage measurement techniques used in prior research. These tests are the USDA test for BCFM, unaided quantitative visual inspection, the Chowdhury colorimetric test (Chowdhury, 1977), and quantitative visual inspection aided by the application of fast green FCF dye.

During each replication, one corn and one fines sample were randomly selected from each damage lot for evaluation with the common tests. These samples were divided into appropriate samples for each test with a Boerner divider. Approximately 90 g was used for the visual inspection and the BCFM test. 100 g was used for the Chowdhury colorimetric test as per the test instructions. The same sample used for the Chowdhury test was also used for the green dye aided visual inspection. Approximately 375 g of corn was used with a

Dickey-John GAC 2000 grain analysis computer to find the moisture content and test weight of the sample. The BCFM test was conducted by using a 4.76 mm round hole sieve to 40 remove small pieces of broken corn from the sample. The mass of any removed portion, as well as any non-grain material remaining on top of the sieve, was compared to the total mass of the sample and expressed as a percent. The visual damage test used the BCFM technique to remove small broken portions of corn, and then all remaining kernels were individually inspected for visible defects. Any kernel showing visible signs of damage was added to the previously removed portion of the sample. The total mass of corn with visible damage was compared to the total mass of the sample and expressed as a percent. The Chowdhury test consisted of the following steps:

1. A 1008 of sample of corn, with fines removed, was soaked in a solution of fast green FCF dye for 30 seconds

2. The dyed sample was immediately rinsed with tap water for 30 seconds 3. The rinsed sample was submerged in a NaOH extracting solution

4. A portion of the extracting solution was evaluated with a colorimeter calibrated to display an integer value indicative of the total amount of damage in the sample.

After the Chowdhury test sample was allowed to dry, the sample was used to conduct the green dye aided visual inspection. Each kernel of the sample was individually inspected for evidence of damage using the visual inspection procedure. The dye remaining from the Chowdhury test accentuated the damaged areas of the kernel, making the task of inspecting the kernels less tedious and allowing smaller areas of damage to be detected.

Results and Discussion Pilot Study

The first portion of the data analysis in the pilot study involved finding the mean damage level of the lots with the common tests. The mean damage values from five replications of each test are found in Table 2.3. The means were compared using a Tukey correction for multiple testing at a significance level of 0.05. Significant differences between 41 means indicated the ability of the test to differentiate between damage levels. These data are also found in Table 2.3. The table shows that the green dye aided visual inspection was the only test able to show statistical differences between all damage level means. The other common tests were unable to distinguish between the slow cylinder and hand shelled corn.

The difference between these two damage levels fell within the range of error of these common tests. As a result, a decision was made to increase the cylinder speed at the slow cylinder level to provide a larger difference between damage levels in the major study. The focus of the pilot study was to identify configurations that responded well at low moisture contents and eliminate those that exhibited little or no usable response from further consideration. Each configuration consisted of a duct angle, an insert configuration, and an airflow speed, as introduced in Table 2.1. Analysis of the test stand data from the pilot study involved comparing the means from five replications of each configuration at each damage level using a Tukey correction for multiple comparisons, as was done with the means from the common tests. In addition, a linear correlation coefficient was calculated between the test stand response for each replication and the means of the common tests using the CORBEL spreadsheet function in

Microsoft Excel. These correlation coefficients were averaged across replications to find a mean correlation coefficient for each common test, resulting in four correlation coefficients for each test stand configuration.

The preceding analysis resulted in six test stand configurations that could differentiate between the fast cylinder shelled corn and the hand shelled corn, as well as between the fast cylinder shelled corn and the slow cylinder shelled corn. None of the configurations were able to differentiate between the slow cylinder shelled corn and the hand shelled corn. However, since three out of four of the common tests were unable to make the same comparison, the test stand configurations that had two significant mean pairs were considered comparable to the common tests. 42

Of the test stand configurations that had significant differences in the mean pairs, three had mean r2 values greater than 0.85 for linear correlations for all the common tests, and two of these three configurations had r2 values greater than 0.96 for all the common tests.

These three configurations were as follows:

1. Insert configuration 2 with the horizontal duct and 100% airflow rate

2. Insert configuration 1 with the angled duct and 100% airflow rate

3. Insert configuration 3 with the angled duct and 50% airflow rate

Due to the design of the test stand, the SO% airflow rate was impractical with the angled duct, as the airflow was insufficient to keep kernels from falling into the duct and hitting the fan. As a result, the 100% airflow rate was substituted for the 50% airflow rate in the major study with the angled duct. The angled duct with insert configuration 3 and 100% airflow was in the original group of six that showed significant differences between damage level means. However, the r2 values for the common tests ranged from 0.74 to 0.84. These values were slightly below the values observed for the other three configurations, but were still deemed acceptable.

Major Study Analysis of the data in the major study was broken into three segments. First, the mean responses from five replications of each common test were compared to determine significant differences in the responses, just as in the pilot study. Second, the same analysis was performed on the five replications for each moisture content and damage level for each of the three test stand configurations. Third, the test stand data were analyzed to find calibration equations for the test stand response in relation to the common tests.

The first portion of the data analysis involved determining the damage level of the three lots of grain using the four common tests. These data are summarized in Table 2.4. 43

Using the same Tukey comparison as in the pilot study, all of the common tests showed significant differences between means of all damage levels at all moisture contents with the exception of the Chowdhury test. These data are also summarized in Table 2.4. The

Chowdhury test was unable to resolve the differences between the slow cylinder and the hand shelled corn at any moisture content, and was unable to resolve differences between any of the damage levels at the high moisture content. In addition, the Chowdhury test did not display an increasing response with an increase in damage at the high moisture content. The inconsistency of the Chowdhury test at the high moisture content was enough to skew the results for the entire study. As a result, the Chowdhury test was not considered in the development of calibration equations for the test stand.

Just as in the pilot study, the means for five replications at each damage level and moisture content were compiled to investigate the resolution of the test stand configurations.

At the high and medium moisture contents, the horizontal duct with insert configuration 2 and the angled duct with insert configuration 1 were able to distinguish between all damage level means at a significance level of 0.05. The angled duct with insert configuration 3 was only able to distinguish between the fast cylinder and slow cylinder means, and the fast cylinder and hand shelled means. At the low moisture content, the angled duct with insert configuration 1 was once again able to distinguish between all three means. The horizontal duct with insert configuration 2 and the angled duct with insert configuration 3 were only able to distinguish between the fast cylinder and slow cylinder shelled means, as well as the fast cylinder and hand shelled means. These data are summarized in Table 2.5. These data show that only the angled duct with insert configuration 1 was able to distinguish between damage levels with a statistical consistency at all moisture contents. For this reason, part three of the analysis was restricted to this test stand configuration.

The third portion of the data analysis involved developing a calibration equation for the selected test stand configuration in relation to the three remaining common tests. The 44 regression analysis was performed using proc reg in SAS software version. 8.2 (SAS Institute,

Inc., Cary, NC) with a Predicted Residual Sum of Squares (PRESS) statistic used to determine the most appropriate model for each common test. The PRESS statistic estimates error in the prediction model by removing each data point one at a time from the data set, fitting the regression model to the other n-1 data points, and then using the estimated model to predict the response variable associated with the excluded observation. The squares of the n prediction errors are then added to form the PRESS statistic. The PRESS statistic attempts to measure how well a particular model will perform when predicting future observations that were not used to estimate the model parameters. Models with low PRESS statistics will tend to give more accurate predictions for future observations than models with higher PRESS statistics.

This analysis resulted in a simple linear model of the form

damagelevel =intercept +slope * (test stand response) for each of the common tests, where damagelevel represents the predicted level of damage for each of the common tests, and the test stand response is the percent of material separated by the test stand. The regression coefficients and associated r2 values are presented in Table 2.6. The calibration data are plotted in Figures 2.4-2.6. The figures show a quantization of the test stand response, which is likely due to experimental error in measuring the mass of the separated material in the test stand. The mass of the catch bins was measured with a laboratory balance that displayed the mass in even integers, resulting in a measurement of the actual mass separated +/- 1 g. The small amount of material actually separated by the test stand resulted in a quantization error of approximately +/- 5%.

Because all of the recorded data points were used to generate the calibration equations, no independent data remained to evaluate the performance of the test stand in predicting the amount of damage for each of the common damage tests. To evaluate the performance of the test stand, it was necessary to remove a portion of the data and generate a 45 new calibration based on the remaining data. SAS was used to accomplish this task by randomly removing one data point from each combination of moisture content and damage level from the original data set. This resulted in a new calibration model based on 36 data points, leaving nine data points to evaluate the performance of the calibration model. A regression analysis based on the PRESS statistic was performed for the new data set, resulting in the regression coefficients presented in Table 2.7. The resulting "new" calibration equations were used to predict the damage level of the nine test stand responses that had been removed from the original data set. The predicted damage level for these nine points is plotted against the actual damage level of those points in Figures 2.7-2.9.

Figures 2.7-2.9 show that the new calibration equations generally work well in predicting the damage level for the selected samples. A linear regression of the predicted damage values vs. the actual damage values results in r2 values of 0.976, 0.992, and 0.957 for the BCFM, visual inspection, and green dye tests, respectively. These figures show a general tendency to underestimate the total damage level when compared to the 1:1 ratio provided by the calibration equation, particularly in the green dye and BCFM predictions. The quantization of the test stand response also becomes obvious in the prediction model with the predicted values taking on three discrete values for each common test.

From a functional standpoint, the test stand configurations using the grate insert showed problematic material buildup on the grate as the test progressed, which fell off when the airflow stopped. This behavior is presented in Figure 2.10. Screen blinding would cause a reduction in effectiveness of the test stand with larger sample sizes, and should be remedied in future studies.

Summary and Conclusions

The technique of using a transverse air flow to separate damaged portions from a controlled stream of falling corn shows potential in being able to predict the mechanical 46 damage level of the corn sample. The most reliable configuration involves directing a 5.5 m/s air flow at an angle of 150 degrees to the direction of grain flow to force damaged corn components across a grate with a hole pattern identical to that of a 4.76 mm round hole sieve.

The proportion of material pushed across the grate expressed as a percentage of the total is a good indicator of the amount of mechanical damage in the sample, and correlated to three common damage tests with r2 values of 0.879, 0.865, and 0.820. Comparing the full calibration model in Table 2.6 to the validation model in Table 2.7 shows that removing a portion of the data does not drastically alter the results of the regression analysis. This leads to the conclusion that the calibration equation is essentially the same as the validation equation, which performs well in predicting the actual damage level of a sample on three separate damage scales. While this technique generally performs well, operation at an optimum level with large sample sizes will require a means for reducing or eliminating material buildup on the grate.

Further studies with this airflow technique for grain damage measurement should focus on the following points:

1. Develop a means to eliminate buildup of material on the grate insert.

2. Install mass flow sensors capable of measuring the flow rates in the two chutes.

Comparing the flow rates in the chutes in real time should give the proportion of

grain being separated directly and eliminate the need to weigh components of the

sample after each test, thereby reducing or eliminating the quantization error from the

laboratory balance. In addition, this will allow for testing of larger samples.

3. Conduct tests of all test stand configurations with other grains.

4. Develop an "on board" sensor appropriate for field testing using the results of points 1-3 to explore the effect of machine dynamics and field conditions on the response of the sensor. 47

Figure 2.1. Test stand used for airflow separation of damaged grain 48

secondary chute Figure 2.2. Wire screen used to close the top of the 49

Figure 2.3. Two solid inserts and one grate insert between primary and secondary drop chutes 50

~~ Visual = 49.9*:Response - 3.65 RZ = 0.865 ~t~ a a

~~ ~~;. ~- e .,r f'~.

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~ 15

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S t~

c~ ~ High Moisure Data Low Moisture Data n ~iid M:oi sture Data ------Prediction Equation

t).1 t).2 0.3 o.~ U.7 Test Stand Response (% Separation}

Figure 2.4. Calibration data for visual damage level using test stand data as input 51

~.~ B~F~~ = x.71*Response - U.~~8 R~ = Q.879 ~.a .. ~ ~ b f ... -~ .~~ O

2.{ ~ ~ ~ :' / `~ C .~'/~ ~ tl ./~ ~_ .i .-',, ~%) %~ /~. !.~~ 1.5 . ~:

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/~ ~ ~. -',Q, ' o High. M:oi sure :Data t).0 .. ~r~-----~~ f Lo~~r Moisture Data ~ Mid Moisture Data ~t~.~ . ------~---- Prediction :equation ,~ t).3 t~.(~ E~.2 4). ~ 0.5 Q.0 C1.7' Test stand .Response {% Separations

Figure 2.5. Calibration data for BCFM content using test stand data as input 52

44 green Dye ~ 57.3*.Response - 4.02

~~ R' = 0.820 n a

30

?5 e .~ e y c~ 0 0 '~ ~o 0 a:~ ~.y is a C 4

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o High 1~.oisure .Data 0~ Lo~v Moisture Data a ~9id ~l~ioisture Data ...... Prediction Equation

Q.Q 0.1. q.2 Q.3 0.~ O.S p.d Q.7 '['est Stand Response (`Yo Separation)

Figure 2.6. Calibration data for green dye damage level using test stand data as input 53

2~ - ;. ,~,..-- .-=~'l, + ..,-`+ + ~ /"~ f

i' ~l~ r f /' f

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Figure 2.7. Validation data and prediction equation line for visual damage calibration 54

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♦ ,'~' N

t) ~ ~ ~ Predicted Green Dye Damage ...... l : l Ratio -3 3() i5 ~0 Actual Green I)ye Damage Lewel (Qfa)

Figure 2.9. Validation data and prediction equation line for green dye damage calibration 56

Figure 2.10. Material stuck to grate with angled duct and insert configuration 1 at the completion of a fast cylinder damage test before and after the airflow was removed 57

Table 2.1. Definitions of insert configurations and corresponding maximum airflow values Insert 100% Duct Inserts Configuration Airflow (m/s) Top: Solid Horizontal 1 Middle: None 9.5 Bottom: Solid Top: Solid Horizontal 2 Middle: . Grate 6.5 Bottom: Solid Top: Solid Horizontal 3 Middle: None 9.5 Bottom: None Top : Grate Angled 1 Middle: Solid 5.5 Bottom: Solid Top: None Angled 2 Middle: None 11.5 Bottom: Solid Top: None Angled 3 Middle: Grate 9.5 Bottom: Solid

Table 2.2. Mass of rewetted fines in each 3 kg corn sample for three damage levels and three moisture contents Hand Shelled Slow Cylinder Fast Cylinder Lot (g) Lot (g) Lot (g) Pilot Study 8 16 86 Low Moisture 10 28 108 Medium Moisture 10 26 102 High Moisture 10 28 118 58

Table 2.3. Mean damage quantities and Tukey comparisons of means from four common damage tests at three damage levels using pilot study data Damage Damage Damage Level Test Measurement Hand Shelled 0.212 A BCFM Slow Cylinder 0.410 A (%Damage) Fast Cylinder 2.S 9 B Hand Shelled 0.340 A Visual Slow Cylinder 3.22 A (%Damage) Fast Cylinder 20.4 B Hand Shelled 0.800 A Chowdhury Slow Cylinder 2.00 A Fast Cylinder 5.60 B Hand Shelled 3.50 A Green Dye Slow Cylinder 13.2 B (%Damage) Fast Cylinder 48.0 C Means within the same letter grouping are not statistically different at the 0.05 level.

Table 2.4. Mean damage measurements and Tukey comparisons of means for four common damage tests at three moisture contents and three damage levels Damage D Low Mid High amage Level Test Moisture Moisture Moisture Hand Shelled 0.040 A 0.038 A 0.000 A BCFM (%) Slow Cylinder 0.525 B 0.592 B 0.652 B Fast Cylinder 2.58 C 2.57 C 2.72 C Hand Shelled 0.798 A 0.756 A 0.585 A Visual (%) Slow Cylinder 5.59 B 6.59 B 6.26 B Fast Cylinder 24.4 C 25.8 C 20.4 C Hand Shelled 2.60 A 5.40 A 4.80 A Chowdhury Slow Cylinder 4.00 A 7.60 A 2.20 A Fast Cylinder 10.8 B 13.2 B 3.60 A Hand Shelled 0.497 A 0.468 A 0.419 A Green Dye Slow Cylinder 7.79 B 7.95 B 7.17 B ~%~ Fast Cylinder 31.4 C 28.0 C 22.5 C Means within the same letter grouping are not statistically different at the 0.05 level. 59

Table 2.5. Summary of significant differences in means at three moisture contents for three configurations of the airflow test stand Airflow Test Stand Damage Low Mid High Configuration Level Moisture Moisture Moisture Hand Shelled A A A Horizontal Duct Insert Slow Cylinder A B B Configuration 1 Fast Cylinder B C C Hand Shelled A A A Angled Duct Slow Cylinder B B B Insert Configuration 1 Fast Cylinder C C C Hand Shelled A A A Angled Duct Slow Cylinder A A A Insert Configuration 3 Fast Cylinder B B B Means within the same letter grouping are not statistically different at the 0.05 level.

Table 2.6. Calibration regression coefficients and r2 values for predicting various common damage values using test stand response as input Damage Slope Intercept r2 Prediction Model

BCFM 5.71 -0.498 0.879

Visual Inspection 49.9 -3.65 0.865

Green Dye 57.3 -4.02 0.820 Inspection 60

Table 2.7. Evaluation regression coefficients and r2 values for predicting various common damage values using test stand response as input Damage Slope Intercept r2 Prediction Model

BCFM 5.56 -0.497 0.860

Visual Inspection 50.1 -3.76 0.837

Green Dye 55.6 -3.89 0.789 Inspection

References

Bern, C.J. and C.R. Hurburgh, Jr. 1992. Characteristics of fines in corn: review and analysis. Transactions of the ASAE 35(6): 1859-1867.

Chowdhury, M. H. 1977. Method of measuring mechanical damage to grain. U.S. Patent Number 4,02 0,6 8 2 .

Dodds, W. 1972. Costs of mechanical damage in shelled corn at grain terminals. ASAE Grain Damage Symposium. Agricultural Engineering Department, Ohio State University, Columbus, Ohio. pp. 29-32.

Fox, R.E. 1969. Development of a compression type corn threshing cylinder. Unpublished M.S. Thesis. Library, Iowa State University, Ames, Iowa

Freeman, J.E. 1972. Damage factors which affect the value of corn for wet milling. ASAE Grain Damage Symposium. Agricultural Engineering Department, Ohio State University, Columbus, Ohio. pp. 49-52

Mahmoud, A.R. and W.F. Buchele. 1975. Distribution of shelled corn throughput and mechanical damage in a combine cylinder. Transactions of the ASAE 18(3): 448- 452.

Quick, G.R. 2002. Personal communication.

Roberts, H.J. 1972. Corn damage and its effect on dry milling. ASAE Grain Damage Symposium. Agricultural Engineering Department, Ohio State University, Columbus, Ohio. pp. 37-48. 61

Saul R.A.}_and J.L. Steele. _1966. V~hy damaged shelled. corn costs moro__to dry. Agricultural Engineering 47(6): 326-329, 337.

Singh, V., N.L. Barreiro, J. McKinstry, P. Buriak, and S.R. Eckhoff. 1997. Effect of kernel size, location, and type of damage on popping characteristics of popcorn. Cereal Chemistry 74(5): 672-675.

Steele, J.L. 1967. Deterioration of damaged shelled corn as measured by carbon dioxide production. Unpublished Ph.D. thesis. Library, Iowa State University, Ames, Iowa.

VanWormer, M. 1972. Corn damage and its effect on feed manufacturing. ASAE Grain Damage Symposium. Agricultural Engineering Department, Ohio State University, Columbus, Ohio. pp. 33-36.

Wang D., and S.R. Eckhoff. 2000. Effect of broken corn levels on water absorption and steepwater characteristics. Cereal Chemistry 77(5): 525-528. 62

CHAPTER THREE. ULTRAVIOLET DETECTION OF DAMAGED CORN

A paper drafted for submission to Applied Engineering in Agriculture

M.A. Brands, G.R. Quick2, C.J. Bern3, S. J. Birrell4, D.S. Nettleton5

Abstract

The performance of test models of a prototype grain damage sensor developed by

Phoenix International (a subsidiary of Deere and Company) was studied. This sensor measured the quantity of mechanically damaged grain in a sample by illuminating the grain flow passing by a sensor window with ultraviolet light. The light source induces fluorescence in any exposed starch of a cracked or broken kernel. The intensity of fluorescence was measured by a photocell, and when the fluorescence exceeded a preset threshold, the sensor emitted a 20 ms (nominal) TTL compatible voltage pulse. For this investigation, the sensor was evaluated with 3 kg corn samples at moistures of 20 to 28% and damage levels established by shelling the grain by hand as well as at two combine cylinder speeds. The response of the sensor was expressed in terms of pulses per kg of corn in the sample for an initial analysis of sample means, but other sensor responses were considered for calibration, including average pulses per second, and the raw number of pulses counted.

Tukey comparisons of mean responses (using pulses/kg) within each moisture content indicated that the sensor was unable to reliably distinguish between damage levels at a significance level of 0.05. The inability to distinguish between damage levels was due to higher variability at elevated damage levels. This variability is likely due to subsampling

1 Graduate student, Agricultural and Biosystems Engineering Department, Iowa State University, Ames, Iowa. 2 Adjunct professor, Agricultural and Biosystems Engineering Department, Iowa State University, Ames, Iowa. 3 Professor, Agricultural and Biosystems Engineering Department, Iowa State University, Ames, Iowa. 4 Assistant professor, Agricultural and Biosystems Engineering Department, Iowa State University, Ames, Iowa 5 Assistant professor, Department of Statistics, Iowa State University 63 error of the sensor. It is recommended that for the sensor to have a practical application, the grain should be presented at a constant mass flow rate, and the sample size of the sensor should be increased, either by sampling the stream of grain with multiple sensors or by increasing the size of the sensor window.

Introduction

Mechanical damage can be defined as damage inflicted upon grain by harvesting and handling equipment. This damage is often characterized by broken, cracked, split, and scuffed kernels. Mechanical damage of cereal grains interferes with handling, storage, processing, and end use of the grain. Damaged grain is a financial burden on farmers through molding and deterioration, which reduce the quality of the grain crop (Saul and

Steele, 1966; Steele, 1967), and through increased input costs for drying (Bern and

Hurburgh, 1992). In addition to the financial burden to the farmer, mechanically damaged grain can impede processing (Freeman, 1972; VanWormer, 1972; Roberts, 1972; Wang and

Eckhoff, 2000), handling and transport (Dodds, 1972), as well as food uses (Singh et al.,

1997).

The quality of any grain peaks in the field before harvest; harvesting and subsequent handling reduce overall grain quality. Combine harvesters cause damage, and harvester settings affect the amount of mechanical grain damage (Fox, 1969; Mahmoud and Buchele,

1975; Quick, 2002). Currently, machine operators have no objective feedback mechanism to relay the amount of damaged grain passing through a combine in real-time. Machine settings are usually changed to obtain the lowest level of grain damage based on visual inspection of bulk grain collecting in the combine hopper. To obtain a more objective measurement of grain damage in a combine, it is desirable to develop a method for monitoring grain damage at or near real-time. This feedback would provide a harvester operator with a consistent, 64

objective indicator to use in making decisions regarding machine settings, allowing the operator to minimize the amount of harvest grain damage. The objectives of this study were to conduct an independent performance evaluation of a prototype grain damage sensor developed by Phoenix International (a subsidiary of Deere and Company), and to correlate the sensor response to the amount of damage in the grain sample as measured by four common damage tests.

Materials and Methods This investigation used a prototype grain damage sensor provided by Phoenix International and Deere and Company for independent evaluation. The sensor design was based on laboratory research into ultraviolet detection of damaged grain conducted previously at John Deere (Brizgis, 1986; Brizgis et al., 1987). The sensor illuminated grain

with ultraviolet light at a wavelength of 254 nm, and measured the induced fluorescence at a wavelength of 300 to 400 nm with a Siemens SFH530 photodiode with built in amplifier. Based on previous studies, the sensor was pre-set so that any fluorescence event that resulting in a response of 0.1 V or greater from the photodiode triggered internal circuitry that emitted a 20 ms TTL compatible voltage pulse, thereby converting analog input into

digital output. This digital pulse was measured with a computer data acquisition system (Cooper, 2002).

Test Stand Description For this study, the sensor was mounted in the grain sampling trough (John Deere part number H152923) that is presently installed in the grain tank of the John Deere 50 series combines. This would not be a permanent mounting location for a production sensor, but it did provide an adequate and convenient channel for flowing grain in this small-scale study.

The sampling chute was inclined at an angle of 44 degrees to allow grain flow past the sensor 65 without installing a flow metering apparatus. The corn was placed in a 5.7-L funnel at the top of the test stand at the beginning of the test and allowed to flow out of the funnel, creating a flow of grain past the sensor. Two flow rates were established by modifying the outlet of two identical funnels. The test stand is shown in Figure 3.1, and the funnels are compared in Figure 3.2.

Data Collection System

Data were collected using a PC30GA data acquisition card from Eagle Technology installed in a Gateway 2000 PS-75 microcomputer. A program was written in Microsoft

Visual Basic to collect analog data from the moisture sensor at a frequency of 1 kHz. The analog data was exported to a Microsoft Excel spreadsheet by the data acquisition program for analysis. The data collection software did not perform any calculations on the data.

Sample Preparation

Corn samples were prepared using a mixture of two Golden Harvest varieties grown near Nevada, Iowa, during the 2001 crop season. The corn was harvested on the ear in the fall of 2001 and stored until January 2002 at which time it was shelled at approximately 15 moisture content using a laboratory sheller using the cylinder, concave, and beater assembly from a John Deere 6600 combine. The cylinder was fed by placing ears on a rubber belt conveyor that emptied into the cylinder at the same location as the original feederhouse. The front concave clearance was set at 38 mm and the rear clearance was set at 21 mm for all cylinder speeds. A high damage level was created by operating the cylinder at 508 RPM. A mid damage level was created by operating the combine cylinder at 318 RPM. A low damage level was created by hand shelling the corn. From hereon, the damage levels will be referred to by the shelling methods: "hand," "slow cylinder," and "fast cylinder." To ensure sample consistency, each damage lot was screened for fines using a Carter Day model XT3 66 dockage tester with a 4.76-mm round hole sieve in place. The fines for each lot were collected and later evenly redistributed among the damage samples in the lot.

To test for the effect of moisture on the sensor response, corn samples were rewetted to moisture contents of approximately 21%, 23%, and 28%. These moisture contents will be referred to as "low," "medium," and "high." The corn was rewetted by spraying distilled water from a 470 ml household spray bottle onto individual batches of approximately 8 kg of corn each. The rewetted corn was stored between 0 and 5 degrees Celsius for 12-24 hours to allow the individual batches to come to equilibrium. The batches were rewetted in stages with each stage increasing the moisture content of the batch no more than 6 percentage points. When the individual batches reached the desired moisture content, they were combined to reform the whole lot. The recombined lot was stored between 0 and S degrees

Celsius for a minimum of 24 hours to allow it to reach equilibrium. Following this storage, the corn was bagged in 3 kg sample sizes and refrigerated until testing took place.

The fines collected from each sample with the dockage tester were rewetted using the same procedure as the corn samples. After rewetting, the fines for each lot were weighed and divided so that each 3 kg sample of corn within that damage level would contain an equal mass of fines. The mass of fines in each sample is summarized in Table 3.1, with each measurement representing the rewetted mass.

Experimental Design

The data collection was organized into a multiple split-plot experimental design with three moisture contents as the whole plots, high and low flow rates as the split plots, five repetitions nested within moisture and flow rate, and three damage levels in each repetition.

The application of the flow rate and damage level factors was randomized, but the application of the moisture contents was not. 67

Test Procedure

Each test began by entering appropriate comments and filenames in the data acquisition system and selecting the funnel for the desired flow rate. A damage sample was randomly selected from the appropriate lot, and one fines sample was randomly selected from the corresponding lot. The corn and fines samples were emptied into a container and briefly mixed together by hand. The mixed sample was placed in the funnel, which was closed by the experimenter's hand. The data acquisition system was started, and the corn was released from the funnel when the computer indicated that data collection had begun.

The amount of time required for the funnel to empty was measured with a stopwatch, and the total mass of the grain passing by the sensor was recorded to establish a mass flow rate. The duration of the individual test was a function of the sample flow rate. As a result, the high flow rates had shorter overall sampling times, and the low flow rates had longer overall sampling times. Following the test, the analog data was charted using Microsoft Excel, and the pulses generated by the sensor were counted manually and recorded. Due to the unequal sampling times, the initial comparison of means expressed the sensor response as a number of pulses per kilogram of corn to account for a portion of the flow rate effects.

Common Tests In addition to being able to accurately determine the damage level in a sample of grain, the grain damage sensor needs to display the results of the measurement in an understandable manner. Due to the lack of awell-defined standard for accurately expressing the amount of damage in a grain sample, this study attempted to correlate the output of the grain damage sensor to four common grain damage measurement techniques used in prior research. These tests are the USDA test for Broken Corn and Foreign Material (BCFM), unaided quantitative visual inspection, the Chowdhury colorimetric test (Chowdhury, 1977), and a quantitative visual inspection aided by the application of fast green FCF dye. 68

During each replication, one corn and one fines sample were randomly selected from each lot for evaluation with the common tests. These samples were divided into appropriate samples for each test with a Boerner divider. Approximately 90 g was used for the visual inspection and the BCFM test. 100 g was used for the Chowdhury colorimetric test as per the instructions. The same sample used for the Chowdhury test was also used for the green dye aided visual inspection. Approximately 375 g of corn was used with aDickey-John

GAC 2000 grain analysis computer to find the moisture content and test weight of the sample. The BCFM test was conducted by using a 4.76 mm round hole sieve to remove small pieces of broken corn from the sample. The mass of any removed portion, as well as any non-grain material remaining on top of the sieve was compared to the total mass of the sample and expressed as a percent. The visual damage test used the BCFM technique to remove small broken portions of corn, and then all remaining kernels were individually inspected for visible defects. Any kernel showing visible signs of damage was added to the previously removed portion of the sample. The total mass of corn with visible damage was compared to the total mass of the sample, and expressed as a percent. The Chowdhury test consisted of the following steps:

1. A 1008 of sample of corn, with fines removed, was soaked in a solution of fast green

FCF dye for 30 seconds

2. The dyed sample was immediately rinsed with tap water for 30 seconds

3. The rinsed sample was submerged in a NaOH extracting solution

4. A portion of the extracting solution was evaluated with a colorimeter calibrated to

display an integer value indicative of the total amount of damage in the sample.

After the Chowdhury test sample was allowed to dry, the sample was used to conduct the green dye inspection. Each kernel of the sample was individually inspected for evidence of damage using the visual inspection procedure. The dye remaining from the Chowdhury test 69

a.coontuat~d-thy da~~aged areas -of-the-kernel-,- ~Y'lalL~~'lg the task of inspecting-tie ke~~~els ~es~ tedious and allowing smaller damaged areas to be found.

Results and Discussion

Analysis of the data was broken into three segments. First, the mean responses from five replications of each common test were compared to determine significant differences in the responses. Second, the same analysis was performed on the five replications at each flow rate and moisture content for the sensor data using pulses per kilogram as the sensor response. Third, the data were analyzed to find calibration equations for the test stand response in relation to the common tests for three possible sensor response variables.

The first portion of the data analysis involved determining the mean damage level of the three lots of grain using the four common tests. These data are summarized in Table 3.2.

The means were compared using a Tukey correction for multiple testing at a significance level of 0.05. Significant differences between means indicated the ability of the test to differentiate between damage levels. All of the common tests showed significant differences between means of all damage levels at all moisture contents with the exception of the

Chowdhury test. These data are also summarized in Table 3.2. The Chowdhury test was unable to resolve the differences between the slow cylinder corn and the hand shelled corn at any moisture content, and was unable to resolve differences between any of the damage levels at the high moisture content. In addition, the Chowdhury test did not display an increasing response with an increase in damage at the high moisture content. The inconsistency of the Chowdhury test at the high moisture content was enough to skew its results for the entire study. As a result, the Chowdhury test was not considered in the development of calibration equations for the grain damage sensor. ~o

The second portion of the data analysis involved comparing the mean responses from the sensor at each damage level across five replications at each flow rate and moisture content. These means were also compared using a Tukey correction for multiple testing with a significance level of 0.05. At the high moisture content, data could not be obtained at the low flow rate due to grain bridging in the funnel. At the mid moisture content and low flow rate, the sensor was able to distinguish between all mean pairs. At the low moisture content and low flow rate, the sensor was able to distinguish only between the fast cylinder and hand shelled pair, and the fast cylinder and slow cylinder pair. These data are summarized in

Table 3.3

At the high and mid moisture contents and high flow rate, the sensor was only able to distinguish between the fast cylinder and hand shelled corn. At the low moisture content and high flow rate, the sensor was able to distinguish between the fast cylinder and hand shelled pair, and the fast cylinder and slow cylinder pair. These data are also summarized in Table

3.3. By comparison, all the common tests, with the exception of the Chowdhury test, were able to show significant differences between mean responses at all moisture contents. Table

3.2 presents the mean damage levels as measured by the various common tests.

The inability of the damage sensor to consistently distinguish between all of the selected damage levels casts doubts on its ability to reliably measure damage in corn with the present sensor configuration. This is likely due to subsampling error in the sensor. The sensor is only able to detect damage in the layer of grain closest to the sensor window. As a result, a thick layer of grain over the sensor would present fewer damaged kernels as a percent of the volumetric flow than a thin layer of grain, assuming a random distribution of damage in the grain flow. Compounding this error is the fact that the sensor window is only a portion of the width of the grain stream, which further reduces the amount of grain being sampled. The small subsample under consideration likely increases the variability in the sensor response due to random characteristics of the particulate flow past the sensor. While 71 the amount of variation in the sensor response was large enough to cast doubts on the practicality of the sensor, an additional interest was to determine if there was a correlation between the measured response of the sensor and the common damage tests. This led to part three of the analysis.

The final portion of the data analysis involved developing a calibration equation for the grain damage sensor in relation to the three remaining common tests. The sensor did not have an internal correction for grain flow rate, and as a result, the sensor response could be expressed in three ways: the number of pulses measured for each 3 kg corn sample, the average number of pulses per second as the grain passed by the sensor, or the number of pulses per kilogram of the sample. The optimum method for expressing the sensor output has not been previously identified, resulting in three distinct regression analyses, one based on each of the response expression methods. All regression analyses were performed using proc reg in SAS software version 8.2 (SAS Institute, Inc., Cary, NC) with a Predicted

Residual Sum of Squares (PRESS) statistic used to determine the most appropriate model for each common test. The PRESS statistic estimates error in the prediction model by removing each data point one at a time from the data set, fitting the regression model to the other n-1 data points, and then using the estimated model to predict the response variable associated with the excluded observation. The squares of the n prediction errors are then added to form the PRESS statistic. The PRESS statistic attempts to measure how well a particular model will perform when predicting future observations that were not used to estimate the model parameters. Models with low PRESS statistics will tend to give more accurate predictions for future observations than models with higher PRESS statistics.

This analysis resulted in a multivariate linear prediction model for each of the common tests. The initial model for each calibration had factors for the sensor response, corn flow rate, moisture content of the grain, and all main factor interactions. Calibration 1 used the raw number of pulses counted per 3 kg corn sample as the sensor response. The 72 final model for all three damage tests in this calibration included parameters for the intercept, the sensor response expressed as the number of pulses recorded for the sample, the moisture of the sample expressed as percent wet basis, flow rate expressed in kilograms per second, and an interaction between the number of pulses and the measured flow rate. The regression coefficients for calibration 1 are listed in Table 3.4. Calibration 2 used the average number of pulses emitted by the sensor per second as the sensor response. The final model for the visual damage and green dye damage measurements included parameters for the intercept, the sensor response expressed as the average number of pulses per second, the flow rate expressed in kilograms per second, and an interaction between the sensor response and the flow rate. The final model for the BCFM content included the same parameters, and added a parameter for the moisture of the sample, expressed as a percent wet basis. The regression coefficients for calibration 2 are listed in Table 3.5. Calibration 3 used the number of pulses per kilogram of corn as the sensor response. The final model for the visual damage test included parameters for the intercept, the sensor response expressed in pulses per kilogram of corn, the moisture of the sample expressed as a percent wet basis, the elapsed time of the sample expressed in seconds, and an interaction between the elapsed time and the sample moisture. The final model for the green dye damage test included the parameters of the visual damage model, while adding an interaction between the sensor response and the elapsed time. The final model for the BCFM content included all the factors of the green dye damage test, and added the interaction between the sensor response and the sample moisture, as well as the three-way interaction between sensor response, sample moisture, and elapsed time. The regression coefficients for calibration 3 are listed in table 3.6.

The calibration data for the each of the three damage tests and three calibration sets are displayed in Figures 3.3 — 3.11. These figures show an increase in variation of the damage prediction with an increase in damage level, regardless of calibration set or common damage test. This is a visual description of the results of the Tukey comparison of means, as 73 the variation in response makes it difficult to resolve between damage levels based on the predicted values. Before this sensor will be able to provide an adequate response in relation to damage, the amount of variability in the response at high damage levels will need to be addressed. Figures 3.3 -- 3.11 also show a general tendency to overestimate the amount of damage at low damage levels, and underestimate the amount of damage at high damage levels. This is likely due to the inability of the linear model to account for changes in variability with changes in damage level and should be addressed in future studies.

A second portion of the regression analysis was to evaluate the performance of the grain damage sensor in predicting the amount of damage for each of the common damage tests. Because all of the recorded data points were used to generate the calibration equations, no independent data remained for the performance evaluation. As a result, it was necessary to remove a portion of the data and generate new calibration coefficients based on the remaining data. SAS was used to accomplish this task by randomly removing one data point from each combination of moisture content, damage level, and flow rate from the original data set. This resulted in new calibration models based on 72 data points, leaving 18 data points to evaluate the performance of the calibration models. The regression coefficients found in the original three calibration models were recalculated based on the reduced data set, and these coefficients were used to predict the damage level of the remaining 18 data points. The predicted damage level for these 18 points is plotted against the actual damage level of those points for all calibration sets in Figures 3.12-3.14.

Figures 3.12-3.14 show that all three calibration sets perform similarly for all three common damage tests. As with the original calibration data, the general tendency of the models is to overestimate the amount of damage at low damage levels and underestimate the amount of damage at high damage levels. In addition, there do not appear to be dramatic differences in variability within each damage level for the three calibrations. 74

The plots of the calibration and verification data do not indicate that one calibration model is superior to the others, requiring additional information to evaluate the performance of the models. Table 3.7 displays the number of factors in each calibration model, as well as the associated r2 values and PRESS statistics. In general, calibration 3 accounts for the most variability in the prediction, as it has the lowest PRESS statistic for each common damage test, and it has the highest r2 value for the BCFM test and the green dye test. However, calibration 3 also has the greatest number of factors for the BCFM and green dye tests. Calibration 2 has the least number of factors for all damage tests, and has the second lowest

PRESS statistics for all damage tests. The press statistic increases approximately l o% from calibration 3 to calibration 2 for the BCFM and visual inspection tests, and increases only 1 from calibration 3 to calibration 2 for the green dye test. The r2 value decreases approximately 9% from calibration 3 to calibration 2 for the BCFM test and decreases approximately 3%from calibration 3 to calibration 2 for the green dye test. Calibration 2 results in the highest r2 value for the visual damage test. From a practical standpoint, calibrations 1 and 2 would most likely be easiest to measure on a combine. Sensors currently exist to measure mass flow rate, as well as moisture, which are input directly to each of these prediction models. Calibration 3 would require additional calculations to allow the response of the grain damage sensor to be expressed in terms of the number of pulses per unit mass of grain. Current mass flow sensors have a response in terms of mass of grain per unit time, which is not directly input into calibration 3. Instead, additional calculations would be required to compare the number of pulses from the grain damage sensor to the actual mass of grain during a particular length of time, resulting in an extra layer of complexity in determining the sensor response.

An additional issue to consider for each of the calibration models is that of sensor "windowing" or "averaging." Increasing the number of samples recorded between output cycles of a sensor has a tendency to reduce overall variability in the measured response. This ~s is generally accomplished by averaging the response of a sensor over a known period, and using the average response as the sensor output. Calibrations 2 and 3 contain time related factors that would easily account for changes in the window duration. Calibration 1 is time independent, which would complicate any decisions on selecting an appropriate window duration. The data obtained in this study was insufficient to determine the effect of varying window durations for the three calibration models. Two window times were considered in this study as a result of using identical sample sizes and two flow rates. The window time was approximately 10 seconds for the high flow rate, and approximately 25 seconds for the low flow rate. Further study should be conducted to investigate the effect of various sampling windows.

Summary and Conclusions

The Phoenix grain damage sensor shows potential in being able to determine mechanical damage levels in corn. A large number of pulses generated at the higher damage levels indicate that the sensor generally performs well when a damaged kernel is presented to the sensor. However, a large amount of variation in the response of the meter at the high damage level limits the accuracy and applicability of the prediction models.

Three different techniques for measuring the sensor response were considered, and measuring the sensor response in the average number of pulses per second appears to be the most useful. The various response models performed in statistically similar manners, but measuring the sensor response in pulses per second resulted in a calibration model with the fewest parameters. In addition, the combine instrumentation required to provide inputs to this model are already in place. Finally, time is a parameter in the model, which would allow various averaging window durations to be accounted for while optimizing the sensor response. 76

Before the grain damage sensor can be considered suitable for use in a combine harvester, the following items should be further investigated:

1. A larger sample should be considered, through increasing the size of the sensor

window, sampling the stream of grain with multiple sensors, or increasing the amount of time the sensor response is measured before a damage level is recorded.

2. The grain stream should be presented to the sensor at a constant and known flow rate to control the effect of flow rate on the predicted damage level.

3. The effect of various lengths of averaging windows on the three calibration models

should be investigated before making a final decision as to how to measure the sensor response. 77

Figure 3.1. Phoenix grain damage sensor test stand ~s

Figure 3.2. Side by side comparison of funnels used to establish high and low flow rates 79

{~ BCFM = -1..76+0,0169*pulses+0.0898*mois#ure+0.477*flowrate+0,Ob986*flowrate*pulses ~ = 0,568 PRESS = 4'7,45 o High .flowrate, high maisture data High flowrate, low moisture data n :High flowrate, mid moisture data Low flowrate, high moisture data (missing} ~ Low fl awrate, I ow moi sture data o :Low flowrate, mid moisture data ...~.~ ... l : ~ Ratio 0

~ ~a .Q-, a.

0

~a

~ a 0 0 a p p8 a 1 4~ ~

e -=`' ~ ~ ~ ~~ ~

U ().5 1 l .~ 2 2.~ 3 3.5 Actual BCF1~I content (°l~~

Figure 3.3. Calibration 1 data for BCFM test using raw number of pulses as damage sensor response 80

:~.s BCF'M = -1.41+0.907*pulses/s+0.699*moisture+0.687*flowrate-1.49*flowrate*pulses/s ~ = O.S92 P12~SS = 44.67 p :E-~igl~ flowrate, high moisture data ~ High flowrate, tow moisture data 3.5 b E-~igh flowrate, mid moisture data Low flowrate, high moisture data (missing} ~ Low flowrate, low moisture data Q Low flowrate, mid moisture data ~ ~ f,..~- ~~~ ' ...... l : l .l?atio , s ~f'`'' r-~ e D .r' ~~ ~ ,~~' ~ p ~r ..- ~ a ,,,,.,- ~ o p

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t).5 ~ ~ ~ ~'71C 71C -'

U z ~~ . ~ f {~ t). S 1 I.~ 2 2.~ 3 :~.5 Actual BCFM. Content {°/<,~

Figure 3.4. Calibration 2 data for BCFM test using average number of pulses per second as damage sensor response 81

BC~Fn1= -0.28-0.828*putseslkg+~.o~#35*time+o.031.I*moisture+o.o~74*pulseslkg*time +~.t}~~Q*pulseslkg*moisture~0.Uo2~o*moistu ~•e*time-U.aU220*moistu ~•e*time* pulses/kg r~ = 0.68 PRESS = 39.81 o High flow~rate, high moisture data ~ High ~lowrate, low moisture data ~ High flow~rate, mid moisture data Lot~~ flowrate, high moisture data (missing} ~ Low ~1 overate, low moisture data c Low flo~Trate, mid nl.oisture data a .,.' , ~~ ~ ~- 1:1 Ratio o :--~' a -~~ .-~''~ ''~ o ,,•'~`" ~ - O ,, ~O r,~ f-.~~ .- '~ 4 , o c --~~' o c ~~, -~' ~ l ~ ~ ~ ~ ~ , ~;. ~

t1.5 e ~ ~ ~

U [) ().3 1 1.5 2 2.5 3 3.S Victual BCFM Content (%}

Figure 3.5. Calibration 3 data for BCFM test using number of pulses per kilogram of corn as damage sensor response 82

~~ visual = -9.87+0.1..78*pulses+0.50*moisture+5,55*flowrate+o.~32*flowrate*pulses rz = 0.630 _PRESS = 3757 ~n o High flowrate, high :moisture data ~ High flowrate, lotiv moisture data ~~ ~ High flowrate, Enid moisture data :Low flowrate, high moisture data (missing) ~' . ~ Lor~v flowrate, low moisture data ,,. ~ :Low flowrate, nud .moisture data o * ~ f , ,.-' l : l Ratio ~.- _f.- o c ,• Q ..-a-' ~,.r ~. ,,:- -' tx

,,- -~'~'~ ~ o r te'

... ''~'!

p8 '' f~ 4 ~' ~ 4 Q to 1 ~ ~~ rte. ~ .-f

-'.~,. ~

U c~ tU 15 ?U 25 3U 35 Actual visual Damage ("lo}

Figure 3.6. Calibration 1 data for visual damage test using raw number of pulses as damage sensor response 83

~s visual. = 1...71+9.1.$*pulsesls+b.43*flowrate-15.b*flowrate*pulsesls r~ = O.b~~ PRESS = 3522 ~~ o High flowrate, high moisture data. ~ High ~"lowrate, low moisture data :;5 n High flowrate, mid moisture data o ;--~_ .r te / 3 :Low flowrate, high moisture data (missing) ,,..,.~-~'"` ~ Low fl overate, l Ow IIIO1StUre data .. ~ f ~ Low flo~~Trate, mid moisture data ~ ,-~'~ ~ ,. s' o ~ ~--~--~--~~l : ~l Ratio ,.~~~ 4

f ~./~ Q ~!..~ --~` a -~~ ,,~ a~

l ~' /f'~ '/ O ~l 1 `~ ,- ~' e

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ww .. b ~ O ~ l t.) ~ . ii ~ .,1,. 11~ ~ = ~ ~ !;. ~ ~ o ~ .4 ~C S .. n ,~ : ~ p ' ~ o ~ ,.- ` ~ _ O ~` ,r~' ' ~ f ~i ~

.~' . ; l~

~~ ?L~ { J t.y .l~ flctual Visual Damage {°/p)

Figure 3.7. Calibration 2 data for visual damage test using average number of pulses per second as damage sensor response 84

~c~ Visual = -38.9+0.972*pulses/l~.g+2.75*time+2.12*moil#ure-0.138*m.oisture*#ime ~ = Q.b38 PRESS = 3130 :~; ,~ o High flowrate, high moisture data .-~ ® High flowrate, low moisture data ~ f,,~'~ a High flowTrate, mid moisture data ° %'f 3C) :Low flowrate, high rnoish.rre data (,missing) ~ f•'~-' f.~~' ~c Low fl overate, 1ow moisture data ~, a o ~~ a L,ow flowrate, mid moisture data r -'~~ ...... l : l Ratio !~. ..'" . ~c ;-~c.-- .. = ~ ,- .~ 4 .~'`~~ J t.. ~ ~.. `~ 8 t' C~ 0 r 0 . ~' f o ° ~ .. 10 o -. € p ~.~' ~ n a °g ~,• ~ e ~ ~i., o ® t~

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Figure 3.8. Calibration 3 data for visual damage test using number of pulses per kilogram of corn as damage sensor response 85

fU Green Dye = -b.75+Q.1.85*pulses+o.451*moisture+3.74*~o~rate+o.871*flowrate*pulses ~ ; Q.b12 PRESS = 5059 o High. flowrate, high moisture data SU High flowrate, low moisture data n High flowrate, mid moisture data. Low flowrate, high ~~~oisture data (missing) ~ Low flowrate, low moisture data. o Low flo~~~rate, mid moisture data o ,.,,...~..-. l :l Ratio 0 0 o ~ 0 fl

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a . lU IS 2U 25 3U i5 4p Actual Green Dye Damage Level (°/a}

Figure 3.9. Calibration 1 data for green dye damage test using rave number of pulses as damage sensor response 86

~o Green Dye = 2.59+1.o.2*pulses/s+5.28*flo~~rate-1G.4*flowrate*pulses/s rz = 0.63o PRESS = 4b83 o High flowrate, high moisture data ~0 4 © High flowrate, low moisture data ,-~ a High flowrate, m i d moi store data ...0 Low flowrate, high moisture data (missi~~g} w ao ~ Low flowrate, low moisture data o ,,.- o Low flowrate, mid moisture data ,, :--.

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Figure 3.10. Calibration 2 data for green dye damage test using average number of pulses per second as damage sensor response 87

~~c~ Green Dye = -28.7+1.92*pulseslkg+2.1.8*time+1.52*moisture-0.0343*pulsesfkg*time -0.103*moisture*time ~ = 0.650 .PRESS = 4635 ~a o High flowrate, high moisture data High flowrate, low moisture data o :High flowrate, mid moisture data Low flowrate, high moisture data (missing} ~ Lo1~r flowrate, low moisture data Q Low flowrate, mid moisture data a r,,~ . -- ~-~-~~~ 1:1 Ratio ~. ®a J

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Figure 3.11. Calibration 3 data for green dye damage test using number of pulses per kilogram of corn as damage sensor response 88

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Figure 3.12. BCFM verification data using three calibration techniques 89

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Figure 3.13. Visual damage verification data using three calibration techniques 90

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Figure 3.14. Green dye verification data using three calibration techniques 91

Table 3.1. Mass of rewetted fines in each 3 kg corn sample for three damage levels and three moisture contents Hand Shelled Slow Cylinder Fast Cylinder Lot (g) Lot (g) Lot (g) Low Moisture 10 28 108 Medium Moisture 10 26 102 High Moisture 10 28 118

Table 3.2. Mean damage measurements and Tukey comparisons of mean pairs for four common damage tests at three moisture contents and three damage levels Damage Low Mid High Damage Level Test Moisture Moisture Moisture Hand Shelled 0.040 A 0.038 A 0.000 A BCFM (%) Slow Cylinder 0.525 B 0.592 B 0.652 B Fast Cylinder 2.58 C 2.57 C 2.72 C Hand Shelled 0.798 A 0.756 A 0.585 A Visual (%) Slow Cylinder 5.59 B 6.59 B 6.26 B Fast Cylinder 24.4 C 25.8 C 20.4 C Hand Shelled 2.60 A 5.40 A 4.80 A Chowdhury Slow Cylinder 4.00 A 7.60 A 2.20 A Fast Cylinder 10.8 B 13.2 B 3.60 A Hand Shelled 0.497 A 0.468 A 0.419 A Green Dye Slow Cylinder 7.79 B 7.95 B 7.17 B ~%~ Fast Cylinder 31.4 C 28.0 C 22.5 C Means within the same letter grouping are not statistically different at the 0.05 level. 92

Table 3.3. Mean sensor response (pulses/kg) and Tukey comparisons of mean pairs for two flow rates of the Phoenix damage sensor at three moisture contents and three damage levels Low Mid High Grain Flow Damage Level Moisture Moisture Moisture Rate (pulses/kg) (pulses/kg) (pulses/kg) Hand Shelled 0.398 A 0.864 A 1.59 A High Slow Cylinder 3.17 A 4.50 A B 4.00 A B Fast Cylinder 14.4 B 9.61 B 6.93 B Hand Shelled 0.399 A 2.40 A Missing Low Slow Cylinder 2.91 A 8.21 B Data Fast Cylinder 16.7 B 32.2 C Means within the same letter grouping are not statistically different at the 0.05 level.

Table 3.4. Summary of regression coefficients for calibration number 1 using raw number of pulses as the sensor response Visual Regression BCFM Green Dye Damage Parameter Model Model Model Intercept -1.76 -9.87 -6.75 Pulses 0.0169 0.178 0.185 Moisture (%) 0.0898 0.540 0.185 Flow rate (kg/s) 0.477 5.55 3.73 Pulses *Flow rate 0.0699 0.632 0.871

Table 3.5. Summary of regression coefficients for calibration number 2 using average number of pulses per second the sensor response Visual Regre s slon ' BCFM Green Dye Damage Parameter Mo d e1 Model Model Intercept -1.41 1.71 2.59 Pulses/s 0.901 9.18 10.2 Moisture (%) 0.0699 N/A N/A Flow rate (kg/s) 0.687 6.43 5.28 Pulses/s *Flow rate -1.49 -15.6 -16.4 93

Table 3.6. Summary of regression coefficients for calibration number 3 using number of pulses per kilogram of corn as the sensor response Visual BCFM Green Dye Regression Parameter Damage Model Model Model Intercept -0.249 -38.9 -28.7 Pulses/kg -0.828 0.972 1.92 Moisture (%) 0.311 2.12 1.52 Time (s) 0.0436 2.75 2.18 Pulses/kg *Time 0.0470 N/A -0.0343 Pulses/kg *Moisture 0.0440 N/A N/A Time *Moisture -0.00250 -0.138 -0.103 Pulses/kg *Time *Moisture -0.00220 N/A N/A

Table 3.7. Summary of model descriptors for 3 regression analyses and three common damage tests using grain damage sensor data Damage Test Calibration 1 Calibration 2 Calibration 3 Number of Factors 5 5 8 BCFM r2 Value 0.568 0.592 0.648 PRESS 47.45 44.67 39.81 Number of Factors 5 Visual 4 4 r2 Value 0.630 Inspection 0.644 0.638 PRESS 3757 3522 3130 Number of Factors 5 5 6 Green Dye r2 Value 0.612 0.630 0.650 PRESS 5059 4683 4635

References

Bern, C.J. and C.R. Hurburgh, Jr. 1992. Characteristics of fines in corn: review and analysis. Transactions of the ASAE 35(6): 1859-1867.

Brizgis, L.J. 1986. Image analysis system for measuring mechanical damage of corn. SAE Paper No. 861456.

Brizgis, L.J., D.B. Keleher, and V.D. Bandelow. 1987. Grain damage analyzer. U.S. Patent Number 4,713,781. 94

Chowdhury, M. H. 1977. Method of measuring mechanical damage to grain. U.S. Patent Number 4,020,682.

Cooper, W.F. 2002. Personal communication.

Dodds, W. 1972. Costs of mechanical damage in shelled corn at grain terminals. ASAE Grain Damage Symposium. Agricultural Engineering Department, Ohio State University, Columbus, Ohio. pp. 29-32.

Fox, R.E. 1969. Development of a compression type corn threshing cylinder. Unpublished M.S. Thesis. Library, Iowa State University, Ames, Iowa

Freeman, J.E. 1972. Damage factors which affect the value of corn for wet milling. ASAE Grain Damage Symposium. Agricultural Engineering Department, Ohio State University, Columbus, Ohio. pp. 49-52

Mahmoud, A.R. and W.F. Buchele. 1975. Distribution of shelled corn throughput and mechanical damage in a combine cylinder. Transactions of the ASAE 18(3): 448- 452.

Quick, G.R. 2002. Personal communication.

Roberts, H.J. 1972. Corn damage and its effect on dry milling. ASAE Grain Damage Symposium. Agricultural Engineering Department, Ohio State University, Columbus, Ohio. pp. 37-48.

Saul R.A. and J.L. Steele. 1966. Why damaged shelled corn costs more to dry. Agricultural Engineering 47(6): 326-329, 337.

Singh, V., N.L. Barreiro, J. McKinstry, P. Buriak, and S.R. Eckhoff. 1997. Effect of kernel size, location, and type of damage on popping characteristics of popcorn. Cereal Chemistry 74(5): 672-675.

Steele, J.L. 1967. Deterioration of damaged shelled corn as measured by carbon dioxide production. Unpublished Ph.D. thesis. Library, Iowa State University, Ames, Iowa.

VanWormer, M. 1972. Corn damage and its effect on feed manufacturing. ASAE Grain Damage Symposium. Agricultural Engineering Department, Ohlo State University, Columbus, Ohio. pp. 33-36.

Wang D. and S.R. Eckhoff. 2000. Effect of broken corn levels on water absorption and steepwater characteristics. Cereal Chemistry 77(5): 525-528. 95

CHAPTER FOUR. GENERAL CONCLUSION

The objective of this research was to investigate possible methods for measuring grain damage in real-time, with a focus on technology for the evaluation of damage in corn. The aim was to develop a reliable and reasonably priced grain damage sensing technology appropriate for use in a combine harvester or as a stationary testing apparatus for use in elevators or inspection points. To this end, a performance evaluation was conducted on a prototype grain damage sensor developed by Phoenix International, a subsidiary of Deere and Company, and a technique for airflow separation of damaged corn was explored. This investigation focused on two techniques of grain damage sensing, but many more techniques were reviewed. Some of the other reviewed methods may prove useful as well.

Phoenix Grain Damage Sensor The Phoenix grain damage sensor used an ultraviolet light source to induce fluorescence in damaged corn kernels. The intensity of the induced fluorescence was measured with a photocell, and any fluorescence event that generated a voltage of 0.1 V or greater from the photocell triggered circuitry to emit a 20ms TTL compatible voltage pulse. This sensor generally performed well in the sense that it was able to reliably detect any damaged corn kernels that were presented. However, the characteristics of the sensor only allowed it to monitor a very small portion of a stream of corn. As a result, variations in the grain flow rate can have dramatic effects on the output of the sensor, as the portion of the grain that the sensor monitors may or may not be a statistically accurate description of the entire grain sample. For this reason, efforts should be made to correct the subsampling error.

This could be manifested by sampling the stream of grain with multiple sensors, or by simply making the sensor aperture larger, allowing it to "view" more grain. 96

Three potential sensor responses were considered when developing calibrations for the Phoenix grain damage sensor. The responses considered included measuring the raw number of pulses generated by the sensor, the average number of samples per second, and the number of samples per kilogram of corn. Overall, the three response measurement methods performed similarly, with no model having a clear advantage over the others. However, the model using the average number of pulses per second has the fewest factors for all common damage tests. In addition, this model would be able to account for changes in sensor averaging times. These practical advantages may provide justification for using this response, but the data recorded in this study were unable to provide proper insight to the "windowing" phenomenon, which is left to future studies.

Airflow Separation Test Stand The airflow test stand used a transverse flow of air to separate damaged portions of a stream of falling grain. The mass of the separated grain was compared to the mass of the total sample as a percent. Six test stand configurations were tested with three different airflow rates, and only one configuration was able to distinguish between the damage levels with a statistical confidence of 95%. This configuration was used to generate a prediction equation for four types of common damage tests with resulting r2 values greater than 0.8. One drawback of this test stand configuration was that material had a tendency to build up on the grate, which could hinder the accuracy of the test stand with larger sample sizes. A wiper assembly or another suitable apparatus should be installed to keep the grate clear in future studies.

Damage Measurement Design Parameters. As noted previously, Chowdhury (1978) suggests some parameters for the design of a grain damage meter. In summary, they were: 97

1. The system must be applicable to a range of cereal grains and legumes, and must be

able to deal with varietal differences within one type of grain.

2. The system must be able to account for grain moisture content. Therefore, the output

must be either independent from, or a quantifiable function of, moisture.

3. Due to differences between grain types, the technique must be independent of grain

constituent content or kernel size and shape.

4. The sample size must be large enough to account for the inherent variation in grains,

as well as to be able to reduce sampling error. The meter must also be able to

accommodate various sample sizes for different grains.

S. Since grain is harvested over a wide range of temperatures, the test must be

independent of temperature, or have an appropriate temperature correction factor.

6. The time it takes to run a test should be as fast as possible while retaining accuracy.

Ideally, the results of the test would be obtainable in 2 to 3 minutes.

7. The test must retain accuracy, and since no "standard" exists, an arbitrary scale or

index must be developed for the meter.

8. The test must be free of human j udgment factors.

Chowdhury generated a good list of parameters for a technique to measure grain damage.

However, when considering the development of a grain damage sensor for a combine harvester, some additions and modifications to this list should be made:

9. The system should be able to continuously measure a flowing stream of grain, or

subsample a grain flow with results available in less than 20 seconds, rather than the 2 to 3 minutes suggested by Chowdhury.

10. The test should not require expendables such as chemical dyes, water, or photographic film.

11. The sensor display should be easily understandable by a typical combine operator.

12. The sensor should be reasonably priced. 98

Referring to the numbered points above, this research addresses some of these points, while others are left to further research.

1. Both of the sensor technologies in this study were only tested in corn. While a mix of

two varieties was used, the varieties were not tested independently~and therefore

effects of varietal differences could not be determined.

2. Both of the damage measurement techniques proved to be independent of moisture

content.

3. No attempts were made to determine the effect of constituent content, size, or shape

of the kernel.

4. Both of these measurement techniques can accommodate large and small sample

sizes by changing the length of the sampling time. The constant flow characteristics

of both measurement techniques allow a large amount of flexibility in sample sizes.

5. All of the laboratory tests were conducted at room temperature (20 C). No attempt

was made to determine if there was a temperature effect.

6. Each measurement technique had a test time of well under three minutes.

7. The airflow test stand turned out to be accurate in estimating the amount of damage in

a sample, accounting for over 80% of the variation in the damage measurement when

compared to three common damage tests. Due to subsampling error inherent in the

sensor configuration, the Phoenix damage sensor was only able to account for just

over 60% of the variation in the damage measurement when compared to the same

three common damage tests. Due to the strong correlations with the common testing

methods, no arbitrary scale needed to be developed.

8. Both damage measurement methods were quantitative. Human judgment was not a factor.

9. Neither damage measurement technique was equipped to provide instant results in

this study. However, both have the capability of providing near real-time data with 99

the only delay due to sensor averaging needed to obtain accurate readings. As provided, the Phoenix damage sensor only needs appropriate software to provide real- time data, while the airflow test stand will require the development of mass flow

sensors capable of measuring the flow in the two chutes before real-time data can be obtained.

10. Neither grain damage measurement method required expendable materials. 11. The correlation with common damage tests would allow an operator to select a

damage level to be displayed based on personal preference or comfort level with a particular common method.

12. An economic analysis of the grain damage measurement methods was not performed. However, neither method required the use of specialized laboratory equipment, leading to the conclusion that the cost of the sensors would not be prohibitive.

Suggestions for Further Study The following suggestions should be considered in further studies to before either grain damage measurement technique should be incorporated into a production sensor:

1. Tests need to be performed with both measurement methods with a range of crops and varieties, including various sizes and shapes of grains.

2. Tests should be conducted to obtain the effect of temperature on the measurement techniques.

3. Amass flow sensor should be developed for the airflow test stand to provide real- time data on the damage level of the grain.

4. The subsampling error of the Phoenix damage sensor should be reduced or eliminated by the consideration of a larger sample with multiple sensors or by increasing the sensor window aperture. 100

5. Field tests need to be conducted for each measurement technique to verify laboratory results under field conditions.

Reference

Chowdhury, M.H. 1978. Development of a colorimetric technique for measuring mechanical damage of grain. Unpublished Ph.D. Thesis. Library, Iowa State University, Ames, Iowa. 101

APPENDIX A. RAW DATA AND CALCULATIONS 102

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Table A5. Phoenix damage meter calculations for pilot study data

Sample Sample Flow Rate Flow Rate Damage Type #pulses Pulses/k Re lication _ Ma~~ (gl Time (sl (k /~l g p Low Hand Shelled 3012 16.9 0.179 0 0.000 1 Low Slow Cylinder 3018 17.3 0.175 15 4.97 1 Low Fast Cylinder 3086 18.2 0.170 55 17.8 1 High Hand Shelled 3012 5.7 0.5 3 3 1 0.3 3 2 1 High Slow Cylinder 3020 6.1 0.497 6 1.99 1 High Fast Cylinder 3086 6.2 0.502 47 15.2 1 Low Hand Shelled 3010 17.0 0.178 0 0.000 2 Low Slow Cylinder 3014 17.3 0.175 11 3.65 2 Low Fast Cylinder 3084 17.2 0.179 58 18.8 2 High Hand Shelled 3014 5.8 0.517 0 0.000 2 High Slow Cylinder 3020 6.1 0.498 10 3.31 2 High Fast Cylinder 3084 6.1 0.506 36 11.7 2 Low Hand Shelled 3014 17.6 0.172 2 0.664 3 Low Slow Cylinder 3012 17.4 0.173 13 4.32 3 Low Fast Cylinder 3084 17.6 0.175 82 26.6 3 High Hand Shelled 3014 5.7 0.531 0 0.000 3 High Slow Cylinder 3016 6.2 0.485 7 2.32 3 High Fast Cylinder 3084 6.1 0.506 41 13.3 3 Low Hand Shelled 3014 17.2 0.176 1 0.332 4 Low Slow Cylinder 3014 17.3 0.175 12 3.98 4 Low Fast Cylinder 3082 17.1 0.181 77 25.0 4 High Hand Shelled 3014 5.7 0.525 0 0.000 4 High Slow Cylinder 3012 6.2 0.489 8 2.66 4 High Fast Cylinder 3084 6.0 0.512 34 11.0 4 Low Hand Shelled 3012 17.1 0.176 2 0.664 5 Low Slow Cylinder 3014 17.3 0.174 22 7.30 5 Low Fast Cylinder 3080 17.1 0.181 91 29.5 5 High Hand Shelled 3012 5.8 0.516 1 0.332 5 High Slow Cylinder 3010 6.0 0.502 9 2.99 5 High Fast Cylinder 3082 6.2 0.495 39 12.7 5 114

Table A6. Phoenix damage meter calculations for low moisture data

Sample Sample Flow Rate Flow Rate Damage Type #pulses Pulsesik Re lication Mass (g~ Time (s~ (kg/s~ g p Low Hand Shelled 3008 25.3 0.119 2 0.665 1 Low Slow Cylinder 3028 23.0 0.132 14 4.62 1 Low Fast Cylinder 3106 29.1 0.107 99 31.9 1 High Hand Shelled 3028 7.4 0.411 2 0.661 1 High Slow Cylinder 3028 7.8 0.387 6 1.98 1 High Fast Cylinder 3086 10.0 0.310 37 12.0 1 Low Hand Shelled 3006 26.3 0.114 1 0.333 2 Low Slow Cylinder 3028 22.8 0.133 4 1.32 2 Low Fast Cylinder 3108 28.9 0.107 23 7.40 2 High Hand Shelled 3004 8.2 0.369 2 0.666 2 High Slow Cylinder 3026 8.1 0.372 19 6.28 2 High Fast Cylinder 3106 8.4 0.372 85 27.4 2 Low Hand Shelled 3010 24.1 0.125 2 0.664 3 Low Slow Cylinder 3026 22.7 0.133 9 2.97 3 Low Fast Cylinder 3104 25.5 0.122 62 20.0 3 High Hand Shelled 3010 8.1 0.373 0 0.000 3 High Slow Cylinder 3028 7.5 0.406 5 1.65 3 High Fast Cylinder 3108 8.0 0.389 19 6.11 3 Low Hand Shelled 3006 26.6 0.113 0 0.000 4 Low Slow Cylinder 3026 23.3 0.130 7 2.31 4 Low Fast Cylinder 3106 21.5 0.144 19 6.12 4 High Hand Shelled 3010 8.1 0.373 2 0.66 4 High Slow Cylinder 3028 7.6 0.397 11 3.63 4 High Fast Cylinder 3106 8.2 0.380 56 18.0 4 Low Hand Shelled 3010 22.7 0.132 1 0.332 5 Low Slow Cylinder 3028 22.8 0.133 10 3.30 5 Low Fast Cylinder 3106 23.3 0.133 57 18.4 5 High Hand Shelled 3008 7.8 0.384 0 0.000 5 High Slow Cylinder 3022 7.8 0.385 7 2.32 5 High Fast Cylinder 3108 7.8 0.401 26 8.37 5 115

T-able A7. Phaen~x d~~nag-~ meter calculations for mid- - moisture data

Sample Sample Flow Rate Flow Rate Damage Type #pulses Pulses/k Re lication Mass (g~ Time (sl (kgJsl g p Low Hand Shelled 2520 31.6 0.080 4 1.59 1 Low Slow Cylinder 2430 32.0 0.076 21 8.64 1 Low Fast Cylinder 3096 30.0 0.103 91 29.4 1 High Hand Shelled 3010 8.7 0.347 2 0.664 1 High Slow Cylinder 3022 8.9 0.341 13 4.30 1 High Fast Cylinder 3100 8.8 0.3 52 3 5 11.3 1 Low Hand Shelled 2524 31.3 0.081 7 2.77 2 Low Slow Cylinder 3024 27.9 0.109 28 9.26 2 Low Fast Cylinder 3100 27.6 0.112 101 3 2.6 2 High Hand Shelled 3010 8.5 0.354 4 1.33 2 High Slow Cylinder 3024 8.3 0.366 11 3.64 2 High Fast Cylinder 3010 9.1 0.332 1 0.332 2 Low Hand Shelled 3010 28.9 0.104 10 3.32 3 Low Slow Cylinder 3028 31.8 0.095 21 6.94 3 Low Fast Cylinder 2990 31.3 0.096 87 29.1 3 High Hand Shelled 3012 10.0 0.3O 1 0 0.000 3 High Slow Cylinder 3024 9.1 0.332 16 5.29 3 High Fast Cylinder 3100 9.3 0.3 3 3 23 7.42 3 Low Hand Shelled 3010 30.7 0.098 6 1.99 4 Low Slow Cylinder 3020 29.6 0.102 21 6.95 4 Low Fast Cylinder 3100 27.9 0.111 120 38.7 4 High Hand Shelled 3006 8.9 0.3 37 3 1.00 4 High Slow Cylinder 3026 9.9 0.305 15 4.96 4 High Fast Cylinder 3100 9.4 0.3 31 43 13.9 4 Low Hand Shelled 3012 29.1 0.104 7 2.32 5 Low Slow Cylinder 3028 28.2 0.107 28 9.25 5 Low Fast Cylinder 3098 28.8 0.108 97 31.3 5 High Hand Shelled 3008 9.6 0.313 4 1.33 5 High Slow Cylinder 3024 8.2 0.370 13 4.30 5 High Fast Cylinder 3100 8.3 0.373 47 15.2 5 116

Table A8. Phoenix damage meter calcula~ons for high moisture data

Sample Sample Flow Rate Flow Rate Damage Type # Pulses Pulses/kg Replication Mass ~gl Time lsl (kgisl Low Hand Shelled 1 Low Slow Cylinder MISSING DATA 1 Low Fast Cylinder 1 High Hand Shelled 3018 12.6 0.240 12 3.98 1 High Slow Cylinder 2868 10.5 0.273 9 3.14 1 High Fast Cylinder 2904 11.2 0.260 19 6.54 1 Low Hand Shelled 2 Low Slow Cylinder 2 Low Fast Cylinder MISSING DATA 2 High Hand Shelled 2 High Slow Cylinder 2616 15.3 0.171 12 4.59 2 High Fast Cylinder 2362 13.1 0.181 13 5.50 2 Low Hand Shelled 3 Low Slow Cylinder MISSING DATA 3 Low Fast Cylinder 3 High Hand Shelled 2136 14.1 0.151 0 0.000 3 High Slow Cylinder 2790 13.5 0.207 6 2.15 3 High Fast Cylinder 2070 13.3 0.155 16 7.73 3 Low Hand Shelled 4 Low Slow Cylinder MISSING DATA 4 Low Fast Cylinder 4 High Hand Shelled 2038 15.3 0.133 3 1.47 4 High Slow Cylinder 2920 14.0 0.208 16 5.48 4 High Fast Cylinder 2342 10.7 0.219 8 3.42 4 Low Hand Shelled 5 Low Slow Cylinder MISSING DATA 5 Low Fast Cylinder 5 High Hand Shelled 2186 13.2 0.165 2 0.915 5 High Slow Cylinder 3004 12.1 0.247 14 4.66 5 High Fast Cylinder 2794 13.1 0.214 32 11.5 5 117

Table A9. Airflow test stand calculations for pilot study data

Total Insert Airflu~r ~irfloti~~ Duct # Damage Tti=pe Test # UD Bin Net D Bin Net Sample Config Speed {°/u) Speed (mis} S~ Separated 1V[axs f~l Hand Shelled 1 2826 1.86 3U 12 6.18% l0U`Y~ 9. ~ 1 Slow Cylinder 2 282=1 188 301.2 b.24% .Fast C~-linder 3 2880 198 3U78 6.43% Hand Shelled 4 2836 120 29Sfi 4.U6% Config 3 SU% 4.75 2 Sloes° Cylinder 5 2864 1()4 2968 3.50`l0 Fast Cylinder 6 2926 1U6 3032 3.SU% Hand Shelled 7 2891) 110 3uUO 3.67°l0 U% U 3 Slow Cylinder 5 2908 lUfi 3()14 3.52% Fast Cylinder 9 29=16 121) 3Ufi6 3.91% Hand Shelled 1() 2938 7U 3t)U8 2.33% l0U°J~ 9.5 4 Slow Cvlirxler 11 2948 68 3U1fi 2.25% Fast Cylinder 12 2t~95 74 3(172 2.4I% Hand Shelled 13 2896 60 295b 2.t)a% Horizont<~l Config 1 SU% =1.75 ~ Slow Cylinder 14 291U 52 2962 1.76`% Fast. Cylinder 1 ~ 296fi Sfi 3022 1..85% Hand Shelled 16 3()()5 () 3U08 O.U()U% U% () G Sloe Cylinder 17 31)1.0 2 3012 U.(}66% Fast Cylinder 18 3U58 8 3U66 0.261°h Hand Shelled 19 2956 U 2956 U.(}OU% 100%► 6.5 7 Slo«~ Cylirxier 2U 296E U 2966 U.UUU°:° Fast Cylinder 21 3026 U 3U26 O.UOU°/a Hand Shelled 22 3():16 2 3018 0.066% Config 2 t)% () 5 Slow Cylinder 23 31)14 () 3U1.4 O.UOU% Fast. C~rlinder 2=1 3()68 fi 307=1 C),I95% Hand Shelled 25 2728 2t) 2748 0.728% SU°io 3.25 9 Slo« Cylinder 2G 2730 2t) 275U U,727% Fast C~jlinder 27 277U 18 2788 0.646% Hand Shelled 25 2872 26 2598 0.897°!° t}% t} I E) Slot~~ Cyliiuier 29 2516 24 2540 1).945% Fast Cylinder 3U 2886 38 2924 1.30% Hand Shelled :? 1 2970 3b 301)6 1.2U% Cortfif; 3 SU% 4.75 I 1 Slog- Cy°finder 32 298=1 3U 3U 1=1 1.UO`% Fast C~rlinder 33 3()24 44 3068 1..43% Hand Shelled 34 2858 1.52 31)10 5.05% lU0% 9.5 12 Sloss Cylinder 35 2574 136 3U1t} 4.52% Fast C~°finder 36 295[) .121) 3U7U 3.91% Hand Shelled 37 291)2 84 29813 2.51.% 10()%► 11.5 13 Slo«~ Cylinder 38 289E 78 2974 2.62% Fast C~-linder 39 2820 86 2906 2.96% Hand Shelled 4t) 27U4 64 2768 2.31% Angled Config 2 5(}% 5.75 I4 Slow° Cylinder 41 2685 fib 275=1 2.40% Fast Cytlinder 42 2720 fi4 278=1 2.3U% Hand Shelled 43 :1004 () 31)04 0.000%, U% U 15 Slow Cylinder 44 3010 2 3012 U,U66%~ Fast Cylinder 45 3U24 10 31)34 ().330°1° Hand Shelled 46 293U U 2930 O.U()U% l0U% S.S 16 Slo«- Cylinder 47 2946 2 2948 U.t)68°!° Fast C~-linder 48 2898 4 291)2 0.138% Hand Shelled =19 274E U 2746 U.ODU`% Config 1 SU% 2.75 17 Slow Cylinder SU 2745 U 2748 0.000% Fast: t~llinder 51 2755 U 2788 U.(}OU% xaT~d Shelled 52 2806 202 31)08 6.72% ()`.'f° () 18 Sloe Cylinder 53 2840 182 3022 6.02% Fast C~-finder 54 2898 1.7E 3U74 5.73% 118

Table A9. Continued

Tatal °~° Insert Airflow Airflow # UD Bin Net D Bin Net 5amp►le Duct Set # Damage Ty°j~e Test Scparatecf Canfig Sped ~°l►) Speed (m/s) Mass (~} Hand Shcllcti 55 2826 186 31112 6.18%a :~U% ~L.7S 19 Sloe Cylinder S6 282=1 188 3U 12 6.24% Fast Cylinder 57 288{) 198 3{)78 6.43%° Hand Shelled S8 283fi l2t} 2956 4.t}6% Conlig 3 1(}0% 9.S 2{} Slo~~~ Cy°°finder 5;) 28~i4 1(}:} 2968 3.S(}% Fast Cylinder fU 292C 1tXi 3(}32 3.St}% Ha~ad Shelled C1 2891} 1.1U 311()() 3.67°;° U% {) 21 Sfo~~~ Cylinder G2 29()8 lt)fi 3014 3,52% Fast Cy=l:indcr 63 29=16 1.2t) 3UG6 3.91.°:° Hand Sheffed 64 2938 7U 3008 2.33% 1{)U°fo {).S 22 Slog° Cyrfinder 6S 2948 G8 3U16 2.25% Fast Cylinder G6 2998 74 3U72 2.=11% Hand Shelled 67 2896 {i0 295E> 2.03°/u Horizontal Config 1. U% () 23 Slo«~ Cylinder 68 291U S2 2962 1.76% Fast C}-finder 69 29b6 Sb 3U22 1.85% Hand Shelled. 70 3008 (} 3UU8 0.000% 5{}% =1.75 24 Sloti~° Cylinder 71 3UlU 2 301.2 O.UGG% Fast C'~=finder 72 3058 8 3U6G 0.26:1% Hand S1lelicd 73 2956 0 295b O.UUO% (}'% 0 2S Slo«~ Cylinder 74 2966 U 2966 tl.t>UU% Fast Cy-under 7S 3U26 t1 3U26 c).UUO% Hand Shcllcd 7G 3Ulb 2 3018 U.U66% Coz~b 2 SU% 3.25 2E Sloti~ Cylinder 77 3{}i4 0 3U14 0.UU0%o Fast G~~linder 78 3U68 G 3074 U.195% Hand Shelled 79 2728 20 27=18 0.728% 1{)0% G.5 27 Slo«~ Cylinder 80 273() 20 2750 U.727°io Fast C~-lindcr 81 2770 i8 2788 U.G4G% Hand Shelled 82 2872 26 2898 0.897°;0 U% U 28 Slo~~~ CyliYrdcr 83 2516 24 254U 0.945% Fast Cylinder 84 2886 38 292=1 1.3U% Hand Shelled 85 2~)7() 36 3{}{?6 .1.2{}% Confi"ig 2 SU% 5.75 29 Slo«~ Cy°finder 86 298=1 3t} 31)1.4 1.(){}% Fast. C~ finder 87 3()24 ~~ 3068 1..43% Hand Shelled 88 2858 1.52 3Ult} 5.{)5% lUU% 11..5 3U Sloe' C}~li:nder 89 287=1 lift 301() 4.52% Fast Cylinder 9t) 295{} 1.2{) 307U 3.91.% Hand Sheffed 9l 291)2 84 2986 2,81% 1()U°fo S.5 31 Slo«~ Cylinder 92 289f 78 2974 2.62%u Fast C~~finder 93 282() 86 29UG 2,96% Hand Shelled 94 270=1 G4 27Ci8 2. l Angled Conl"ig 1 SU% 2.75 32 Slo«~ Cylinder 95 2688 66 2754 2.40% Fast Cylinder 96 2720 G4 2?84 2.3(}% Hand Shelled 97 3004 {} 3004 0.(}00% {)% () 33 Slo~~~ Cylinder 98 3t)lU 2 3U12 O.UGb% Fast Cylinder 99 3024 10 3034 0.33U% Hand Shelled l0U 2930 0 2930 O.UUU°io ()'% 0 34 Sloz~' Cylinder lUl 2946 2 2948 U.U68% Fast C~-lindcr lU2 2898 =1 2902 U.138% Hand Shcllcd lU3 2746 U 274b U.UUU% Co~~~ 3 1OU% 9.5 35 Slow Cylinder lU4 2748 0 27=18 O.UUO% Fast C~~linder lU5 2788 U 2788 0.000% Hand Shelled lU6 2806 202 3UU8 6.72% SU% =1.75 36 Slo«~ Cylinder lU7 2841) 182 3U22 6.02% Fast C}-lindcr IU8 2898 176 3U74 5.73% 119

Table A9. Continued

Total % Insert Airflow Airflov~~ Duct Set # Damage Tz°pe Test # UD Bin Net D Bin Net Simple Config Speed (%} Speed (mis~ Se ~arated Mass (u) 1 Hand Shelled lU9 2$26 l86 3012 6.1$% U% U 37 Slow C~~linder llU 282=1 188 3t):12 b.24°l0 :Fast C}°liT~der 111. 288U 1.9R 3t)7f~ 6.~3% Hand Shelled :112 2836 12U 2956 ~.(}fi% Conf"~g 1 5t)% 4.75 38 Sloe° Cylinder 11.3 2864 lU4 29(18 3.SU°fo Fast C~~linder 114 292{i 1U6 3U32 3.SU% Hand Shelled. 115 2$9U 110 3UUU 3.67% l0U% 9.5 39 Sloe' C~°under 11G 29Ug lU6 3U1~ 3.52°r'o Fast Cylinder. :11.7 294G 120 30CG 3.91°l0 .Hand Shelled 118 2938 70 3(}OR 2.:13°l° U% 0 4U Slo« Cylinder :11.9 2948 68 3016 2.25% :Fast C}.flinder 12U 2998 7=1 3U72 2.41.% Hand Shelled 121 2806 f() 2956 2.03% Horizontal Col~fig 3 1{)U% ~?.S ~l Slo~c~ C}linder 122 291U 52 2962 1.76%0 Fast. Cylinder 123 2966 5fi 3022 1.85°l0 Hand Shelled 124 3UU$ U 3UU$ U.ODU°:° 5U"!° 4.75 42 Sloe- Cylinder 125 3UlU 2 3012 O.UG6% Fast Cy°tinder 12C :lU5A 8 3UGG 0.261.`,'fo .Hand Shelled 127 29aG 0 294E O.U()U% 50°l0 3.25 43 Slo~i~ C}~•li~~der :128 2~1f6 U 2966 O.OU(}% Fast C}jlinder 1.29 3()26 0 3U2G U.t)UU% Hand Shelled I3t) 3U ifi 2 3018 U.UfiG% Colyfig 2 0°'n U ~~ Slo«~ Cylinder 131 301=1 {) 3U 14 O.OU()°l° Fast C}Minder :132 30E8 G 3074 U.I95% Ha~~d Shelled 133 27213 20 274$ U.72$% 1()0°!° 6.5 45 Sloe C}Tinder 134 273U 2U 2750 0.727% Fast C~jlir~der 1.35 2770 1.8 278$ O.E4t% Hand Shelled .136 2$72 26 2898 U.897% lUU% S.5 46 Slog{~ Cylinder 137 2516 2=1 2540 U.94S°!o Fast Cylinder 138 28136 3$ 224 1.3U°ro Hand Shelled 139 2970 3d 3006 1.2U°lo Con("~g 1 U%° U 47 Slo~~~ C~°under 1~#U 2984 3{) 3U1=1 I.UU'% Fast C}~linder. :1=11 3024 44 30f8 1..43°l0 Ha~~d Shelled 1.=12 2858 1.52 301U 5.05% 5U% 2.75 48 Sloe Cylinder 143 2874 136 3U1C) 4.52% Fast Cti-under 1=14 295U 12U 3070 3.91% Hand Shelled 1.45 291)2 $~ 2.9$6 2.81% 1UU°f. 9.5 49 Slot~~ Cylinder 115 289E 78 297=1 2.C2% Fast C}Minder 147 282U $6 2906 2.96% Hand Shelled 1=113 27U4 64 2768 2.31°l0 Angled Con~g a 0% 0 40 Slo~~~ C}~°under 119 ZG$f3 GG 27>4 2.4U°lo Fast Cylinder :150 2'12U 64 2784 2,3U% .Hand Shelled 15:1. :3UU4 0 3UU4 C).(}(}U°i° 5()% 4.75 51 Sloe Cr~linder 142 301.0 2 3012 0.0(16% Fast C~°under 153 3024 1U 3U3~i 0.33()% Hand Shelled 15=1 2930 U 2)3U O.UUU% U°'° 0 52 Sloc~~ Cylinder 155 2946 2 2.94$ U.0G8% Fast. Cylinder I SG 2898 4 29U2 C).13$% Hand Shelled 157 2746 U 2746 t}.UOU`i° Config 2 100% 1:1..4 53 Slow Cylinder 158 274$ 0 2748 OAUU% Fast Cylinder 159 2788 U 2788 U.U00% Hand Shelled 1dU 280Ei 2()2 3t)U8 6.72% SU% 5.75 54 S101~' C}'lillder 161 2$4U 182 3U22 fi.02% Fast C`~flinder 1 G2 2898 l 76 3074 5.73% 120

Table A~. continued

Total Insert Airflo«- Airflowr °!o Duct Set # Damage T~°pe Test # UD Bin Net D Bin Net S€tmple Config Speed (%} Speed (m/s) Separated Mass tom) Hand Shelled 163 2826 18G 3012 6.18% U% U S5 Slot~~ Cylinder 1G4 282=1 188 3012 6.24% Fast Cylinder 16S 2880 1.98 3078 6.43`Yo Hand Shelled 1GG 283E 120 29SG 4.06% Config 1 IUU% 5.5 SG Slo~cy Cylinder. 167 28G4 1.04 29G8 3.50"/0 Fast Cylinder 1G8 292E lUG 3032 3.SU% Hasid Shelled 1G9 2890 1lU 3000 3.67"0 5t)"~° 2.75 57 Slo~y Cylinder 17f) 29(.►8 lUG 3().14 3.52% :Fast Cylinder 171 29~1G 12f) 30GG 3.91% Hand Shelled 172 2938 7U 30()8 2.33% Sf)'~, 4.75 58 Slo~~~ Cylinder 173 2948 68 3016 2.25% Fast Cylinder 174 2998 7=l 3072 2.41"/0 Haim Shelled 17a 289E 6U 29SG 2.03% Angled C`ontig 3 l Ut}% 9.S S9 Sloc~~ t~`ylinder 17b 2910 >2 29G2 1.7G% Fast Cylinder :177 296E SG 3022 1.85% Hand Shelled 178 3U()8 () 3Uf)8 ().t~U()°l0 U% U GU Sloe C}Minder :179 3():1.0 2 3012 U.U(~fi% Fast Cylinder 18U 3U58 8 3066 ().2G1% Hind Shelled 181 29SG U 2956 (),UfJU% 1f)0% 11.5 61 Slor~~ Cylinder 182 29fiG 0 29fiG U.()UU%, Fast Cylinder 183 3()2G () 3026 O.Of}0% Hand Shelled :18=1 3U:1G 2 3018 ().OG6°o Con~g 2 U`% 0 G2 Slow Cylinder. 185 3U14 0 301=1 O.U00% Fast Cylinder 18G 3Ufi8 6 3074 U.195% Hand Shelled 187 2728 2f) 27=18 0.728% SU% S.7S E3 Sloe' Cylinder 188 2730 2U 2750 U.727% Fast C}Minder 1.89 277() l8 2788 ().G4G% Hand Shelled .19(1 2872 26 2898 0.897% SU% 4.75 G4 Slog{~ Cylinder 191 251G 2=1 2540 U.94S% Fast Cylinder 192 28x6 38 2924 1.30% Hand Shelled 193 297f) 3G 30Ufi 1.2U% Config 1 lUU%° 9.a GS Slo~c~° Cylinder 19=1 2984 3U 3()14 1.U0'% Fast Cylinder :195 3024 44 30ti8 1..~#3% Hand Shelled 19fi 2858 lag 3ti10 a.U5~j0 0`% () GG Slo~y Cylinder 197 2874 13G 30.11) 4.52% Fast Cylinder 19t{ 2950 12() 3U7U 3.91% Hand Shelled 1.99 29(:)2 84 2986 2.81% ()`Y0 0 67 Slo«~ Cylinder 2UU 289G 78 2974 2.62% Fast Cylinder 2U 1 2820 86 290G 2.9G% Hand Shelled 202 27U4 64 2768 2.31% Horizontal Config 2 IUO°~t~ 6.5 G8 S1o~~~ Cylinder 2U3 2688 GG 2754 2.40% Fast Cylinder 204 272() fi4 2?84 2.3U% .Hand Shelled 2t)S 30()4 0 3t:)04 U.Uf){)% SU% 3.25 G9 Sloe• C`ylillder 206 30:1.0 2 3012 f).Of>fi% Fast Cylinder 2t)7 302=1 lf) 303=1 0.33{)% Hand Shelled 2U8 293U U 293U U.000% U% U 7U Slor~° Cylinder 2U9 294G 2 2948 U.(>68% Fast Cylinder 210 2898 4 2902 U.:138% Hand Shelled 211 274E t) 274G U.(1tX)% Con~g 3 1C)U"/0 t.),5 71 Sloe Cylinder 2l2 2748 0 2748 O.UUU°/a Fast Cy°tinder 21.3 2788 U 2788 U,Ut~°io Hand Shelled 214 28C)f 202 3008 G.72% SU% 4.75 72 Sloti~• Cylinder 21a 2840 182 3U22 6.02% Fast C}Minder 216 2898 1.7E 307=1 5.73% 121

Table A9. Continued

Total % insert Airflow Airflow Duct Set # Damage Tyre Test # UD Bin Net D Bin Net Sample Con~i~ Sp+~d (%} Speed (m/s} Separated Mass (~) Hand Shelled 217 2826 186 3012 6.18% SU% 2.75 73 S1o~~ Cylinder 218 2824 188 3012 6.24% Fasl Cylinder 219 2K8U 198 3U78 6.43% Hand Shelled 22U 2836 1.20 29>G 4.UG% Conf'ig 1 lUU% S.5 74 Slo~c~' Cy-under 221 28b4 lU4 2968 3.SU% .Fast Cylinder 222 2926 1.06 3032 3.SU% Hand Shelled 223 289E) 110 300U 3.67% 0% U 7i Sloe° Cylinder 224 2908 1.U6 31)14 3.52% Fast C~~linder 22S 2946 120 306E 3.91% Hand Shelled 226 2938 7U 3U08 2.33% 50% 5.75 76 Sloe- Cylinder 227 2948 G8 3U 16 2.25% Fast Cy=linder 228 2998 7=1 3072 2.41% Hand Sliclltxl 229 2896 GU 29S{ 2.U3°i° Angled Config 2 loo°i, 11.5 77 Slot~~ Cylinder 23U 2910 52 2962 1.76% .Fast Cylinder 231 2966 SG 3U22 1.85`x° Hand Shelled 232 3UU8 U 3008 {).UOU% U% () 78 Slo«~ Cylinder 233 3UlU 2 3U12 O.O6G% Fast Cylinder 23=1 3()58 8 3U6G U.2G1% Hand Shelled. 235 295E U 29SG O.UUU% SU% 4.75 79 Sloe• C~-•under 236 29f6 U 2966 U.()UU°1° Fast Cylinder 237 3026 U 3U2G U.UUU°~~ Hand Shelled 238 3U16 2 3UI8 U.UG6% Config 3 lUU% 9.5 8U Slow Cylinder 239 3U14 U 301=1 U.(lUU% Fast Cyli~ider 24{) 3()68 G 3074 0.195% Hand Shelled 2=11 2728 2U 2748 U.728% 0% U 81 Slo~~~ Cylinder 242 273U 2U 27SU U.727% Fast C~°under 243 277U 18 2788 U.C46% Haiul Shelled 244 2872 26 2898 0.897% 0°to U 82 Slo«• Cylinder 24S 2S:1G 24 2S4U U.94S% Fast C}=finder 24fi 2886 38 292=1 1.30% Hand Shelled 247 297U 36 3UU6 1..20% Config 1 SU% =1.75 83 Sloe Cylinder 2=18 2984 3{) 3U14 i.UU% Fast Cylinder 249 3{)24 44 3UG8 1.=13% Hand Shelled 2~() 2858 1S2 301{) 5.U5% l U{)% 9. S 84 Sloe- Cylinder 251 2874 136 3U 10 4.52°i° Fast C`y°finder 2S2 2950 120 3U7U 3.91% .Hand Shelled 253 29U2 84 2986 2.81.% SO°lo 4.75 8S Sloe• Cylinder 2S4 2890 78 2974 2.62% Fast CtiTlia~der 255 2820 8b 29Uf 2.96`% Hand Shelled 2SG 27U4 64 2708 2.31% Hori~oiital Config 3 l U0% 9. S 8G Slo«~ Cy-under 2S7 2688 6C 2.754 2.4{)% Fast. Cylinder 258 272U G4 2784 2,30% :Hand Shelled 2S9 3UU4 0 3UU4 O.UUU% U% U 87 Slo~ti• Cylinder 26{) 3{) lU 2 3U 12 U.UG6% Fast C~°under 261 3U24 1U 3034 U.33U% Hand Shelled 262 2930 U 293U O.UUO% U% 0 88 Slo~~~ C~°finder 263 2946 2 2948 U.068% Fast Cylinder 264 2898 4 2902 0.:138% Hand Shelled 26S 2746 U 2746 U.ODU% Coiifig 2 lUU% G.5 89 Slow Cy linden 2Gfi 2748 {) 2748 U.UU{)% Fast C}Minder 267 2788 U 2788 O.U(x)°lo Hand Shelled. 268 28UG 2U2 3UU8 6.72% SU% 3.25 90 Sloe- Cylinder 269 2840 1.82 3022 6.U2°`° Fast C`~°linden. 27U 21398 17ti 3U74 5.73% 122

Table Alo. Airflow test stand calculations for low moisture data

Total % Insert Airflow Airl'lo~v Duct Set # Damage Type Test # UD Bin Net D Bin Net Sample Canflg Speed (%) Speed (m/s) Separated Ititass (~l Slo~y Cylinder 4 3Ui2 2 3U1.4 O.OGfi% "~ H. orizontal. 2 lUU"/o 9.5 2 .Fast Cylinder S 30G8 1() 3U7K U.32S% Hand Shelled G 30UG 2 3008 O.UfG% '.~ Hand Shelled 10 30U4 2 3UUG a,UG7~%, ~; Angled 1 lU(l°i° S.S ~ Fast Cylinder 1.1 307U 14 3U84 0.454% ~ Slo~y Cylinder 12 3{} I4 R 3022 t).2GS% ~ Slog;~ Cylinder l.3 29A=t 3fi 3U2U 1..19°l0 ~/. A:ngled 3 IO{)°r'° 9.S 5 Hand Shelled 14 29G4 32 299E I.U7% Fast C~°under 1S 3U32 GU 3U92 1,9~% :Hand Shelled 22 298G 2 2988 0.UG7% N Horizontal 2 :100% 9.5 8 Slow Cylinder 23 30U4 ~ .~UUB x.133% Fast Cylinder 24 3{}8G G 3U92 0.194% 0 • •-• .Fast Cylizzder ZS 3072 1 G 30813 U.S l l3°10 Augled 1 l UU%, 9.5 9 Slog Cylinder 26 30U8 6 3U 14 0.199% 4.) Hazel Shelled 27 299U 4 2994 U.134% Hand Shelled 28 29fi8 34 3(lU2 1.I3% ~/~. Angled 3 lUU°/v 9.5 lU Sloti~ Cylinder 29 2t)7f 42 3U1.8 1.39°/u Fast Cy under 3() 3(238 SK 3()9C~ l .K?af° Sloe Cylinder 37 3U1.0 4 3U14 t).:133% M Horizontal 2 I.00% 9,S 13 Hand Shelled 38 3UUG 2 3UU8 O.UGG% Fast Cylinder 39 3{}74 12 3U8t~ 0.3$9% • •-: Slow Cylinder 40 2978 42 3U2U 1.39°l0 A:zzgled 3 IUt}%, 9.S l4 Nand Shellod 4:l 29'74 32 3000a I.UG%, ~ Fast Cylinder 42 3U22 G2 3UK4 2.U1% ~ .Fast Cylinder 49 2Gt18 l 2 2? l O U.443°>0 ~/. Angled 1 1t)U% S.S 17 Hand Shelled SU 3002 ~ 3UUG 0..133% Slotiy Cylinder S 1 3()74 14 3(1K8 0.453% Hand Shelled b4 293:} 2b 2960 0.878% ~ Augled 3 lU0% 9.5 22 Slo~y Cylinder GS 284U 38 2K78 1.:12°!° Fast Cylinder GG 3U1.4 G4 3U78 2.UK'/o ~; Slow CF Linder fa7 3()U2 4 30tlEi 0.133% ~, Horizonta.I 2 IOU% X3.5 23 Hand Shelled GK 2992 2 2994 O.007% 4~ Fast Cylizxler fig 30G4 I0 3U74 U,32S% ~ Hand Shelled 7U 299G 2 299$ O.UG7°!° ~/~. Angled 1 I.UU% S.5 24 Fast Cylinder 71 3Ufi4 1G 3UKU (1.519% Sloe Cylinder 72 3010 G 3Ui6 U.199% Slow Cylinder 7b 2996 2 291)8 O.UG7°/a ~ Horizontal. 2 lUU% 9.S 2fi Fast Cylinder 77 3{}=IK I2 :TOGO {).392% .Hand Shelled 78 299G 0 0 2996 U.OQU% • ~ Hand Shelled 79 29GU 44 3UU4 1.46°l° An led 3 It}U°lo 9.5 27 Fast C lznder 80 3U24 G4 .~ g y 3U88 2.U?% ~ Slow Cylinder K1 2984 38 1022 1.26% ~'' Fast Cylinder 88 303U 12 3042 0.394% 4~ ~/. Angled 1 1()0°f° S.S 3U Hand Shelled 89 3UU2 2 3UU4 U.067% Slow Cylinder 90 1014 A 3022 U.2G5°l, 123

Table A11. Airflow test stand calculations for mid moisture data

Total Insert Aixflow Airflow °fo Duct Set # Damage T~~pe Test # U~D Bin Net D Brn Net Sample Confi~ Spec€! (°lo) Speed (m!s) Separated Mass tul Fast C~'linder ~ 3064 10 3074 0.325% Horizontal 2 IUU°% 9.5 2 Hand Shelled ~ 299=1 2 2996 U.Uti7~'/° Slow- Cylinder 6 3U 16 ~ 3020 0.:1:12°l0 Hand Shelled 1.0 299E 2 2998 0.067% Angled. l 10t}% 5.5 4 Fast Cylinder 1.1 306Ci 14 3080 0.455% Slow C~rlindcr 12 3006 C 301.2 0.:199% Sloe C~'linder 1.6 2962 ~~ 2996 1..13% Angled :l 1(}0% 9.5 6 .Hand Shelled 17 2948 3K 2986 1.27°l0 .Fast C~-under 18 30:1.=1 f2 3076 2.02°J° Slog• Cvunder 1.9 2554 t 2860 0.21.0% Angled 1. IOU`,'/0 5.5 7 Fast C}~lindcr 20 3061 16 3080 0.519"/0 .Hand Shelled 21 3UOO =1 3004 0.:133°/a Sloe Cylinder 25 3000 4 3004 0.133% Horizontal 2 1()Uoj° t.?.5 lU Fast Cylinder 29 3072 12 3084 0.359°l0 :Hand Shelled 3U 3{}{)4 {) 3t}U4 t).U(}{)% Fast Cvlirxicr 31 3(}14 60 3074 1.95% Angled 3 .1{}()% 9.5 1:1 Slow Cylinder 32 2976 42 3018 1.39°% Hand S:l~elled 33 2966 35 3004 1..2E% Sloe C~°under 40 2976 44 3020 1.46% Angled 3 lUt}% 9.5 14 Hand Shelled 41 2966 36 3002 1.20% Fast CS~lindcr 42 3{}U4 55 3062 1.89% :Hand Shelled 49 299=1 2 2996 O.U67% Horizoltal 2 1(}U% 9.5 17 Fast Cylinder 50 3065 1U 3075 0.325% Slow Cylinder 5:1. 3U 12 4 3U 1 t 0.:133°/a Hand Shelled S2 2994 2 2996 U.U67'/o At~glcd 1 IUU%, 5.5 18 Fast Cylinder 53 306t) 1K 3078 0.585°l0 Sloe Cvlindcr 54 301=1 6 3020 0.199°/°} Fast Cvlindcr 58 3068 lU 30'78 0.325% Horizontal 2 lUU~1° {}.5 2U Sloe° Cylinder 59 3UlU 2 3012 0.066% Hand Shelled fiU 30{)t"i 2 3{)(}g U.()C~f~% Slow' Cylinder 61 21)713 4f) 31)18 1.33"/0 Angled 3 IOUs/a 9.5 21 Fast Cylinder 62 3025 54 3082 1..75% .Hand Shelled C3 296f3 3G 3004 1.20% Slow Cylinder 64 3012 6 3015 0.199% Angled I It}0°I° S.S 22 Fast Cylinder 65 3058 18 3076 0.585% Hand Shelled 66 3000 4 3004 0.133% Hand Shelled 73 2c}7G 28 3004 0.932% Angled 3 1{}()% 11.5 25 Slog{° Cylinder 74 2978 38 3016 1.217% Fast C~•linder 75 3024 55 3(}82 1.58% Hand Shelled 76 2996 0 2990 0.000% Horizontal 2 lO0% 9.5 26 Slog ~°lijlder 77 30:12 4 3016 0.133% .Fast Cyliiuler 75 3070 10 3080 0.325% Slow' Cylinder 85 3OU6 4 3010 U. 1.33°l0 A:ttglod 1 IUU°fa 5.5 29 Fast CS'linder 56 3062 18 3080 0.554% Haiu1 Shelled 57 3(}UO 4 3004 0.133% 124

Table Al2. Airflow test stand calculations fur high moisture data

Total % insert Ai,~1ow~ A_ir[lo~~: :Dint Set # Damage T~fpe Test # UD Bin Net D Bin Net Sample Conti; Speed ~%) Speed (m/s} Sel~aratetl Mass (ul Hand Shelled 7 30()4 ~ 3UU8 0..133% Angled 1 1 UU"/o >.5 3 .Fast C~~linder 8 3U7U 18 3088 U.58;i% l Sloe Cylinder ~ 3U 14 6 3020 0..199°l0 O ..~-.~ ,~ Slow Cylinder 10 2966 50 3(116 1.66% . ,r.~; Angled. :~ lUU% 9.5 4 Hand Shelled 11 2958 44 3UU2 1..47°/a cU Fast Cylinder 12 301.6 74 3()t)0 2.39% Slow Cylinder 1.3 277=} 4 2778 U.144% 43 Horir.,onta:l 2 1U(1`io ~).5 5 Fast Cylinder 14 3082 lU 3U92 0.323°fo Hand Shelled 15 3(1(14 2 3UU6 C1.UG7°~o .Hand Shelled 22 3000 2 3UO2 U.067% ~ Horizontal 2 l0U% }.~ 8 Slow Cylinder 23 3U14 4 3U18 U.I33% :Fast Cylinder 24 3U84 1.2 3U96 0.388% • ~ Fast Cylinder 31 3066 I6 3UK2 0.519% •~ Angled l 10U% 5.5 l 1 Slow Cylinder 32 U1.6 6 :iU22 ().1,1J/°t c ° ~ Ha~Yd Shelled 33 2996 2 2918 t}.Ufi7% Hand Shelled 34 2954 4(3 2994 1.34% ~/ Angled 3 10f)% 9.5 12 Slory C~°linder 35 2978 4() 3U 18 1.33% .Fast Cylinder 36 3U34 62 :3096 2.OU'~o Slow Cylinder =13 298U 36 30.1.6 1.:19% M Angled 3 1(1()°% 9.5 l ~ :Hand Shelled 44 2958 38 2996 1..27% Fast Cylinder =I5 :304() 58 :1098 1.A7% • ►-~ Fast Cylinder 46 3U72 1=# 3U86 0.454%~ Ariglcd 1 1UU°Jo 5.5 16 Hand. Shelled 47 29)6 2 2998 U.Ub7% 4) Slow Cylinder =t8 3U18 fa 3U2=# 0..198% ~" .Fast Cylinder 52 3076 l2 3U88 0.389% 4~ ~/ Horizontal 2 1(}()°l0 9.5 1.8 Hand Shelled 53 26U6 2 26U8 U.U?7°lo Slotr~• Cylinder 54 301U 4 301.4 0.133% .Hand Shelled 55 2}92 2 2994 U.U67% ct" Angled 1 IU(1% 5.S 19 Slow Cylinder G 30U6 6 3U1.2 U.199% Fast C~~linder 57 3U70 18 3088 0.583% ...., Slory Cylinder f> l 3(}UU 4 3UU=1 0.:133°10 ....+-a .~-.~ Horizontal 2 10U% 9,5 2I Fast Cylinder 62 3U84 14 3Ua8 0.452% 4,~ .Hand Shelled 63 2996 2 2998 U.067% Hand Shelled fi7 2950 4U 2990 1.34°% Angled 3 :I.UO% 9.5 23 Fast Cylinder 68 2682 52 2734 1.90°io Slow Cylinder 69 2982 38 :3020 1..26% Hand Shelled 73 2972 34 30U6 i .13% ~ A~lgled 3 lUU°'o 9.5 25 Sloe Cylinder 74 2970 42 3U 1.2 1..39°/a Fast Cylinder 75 a 3()28 64 3092 2.070% ~; Slow Cylinder R2 30U2 6 3U08 U.199% ~, Angled :l 1 UU"/o 5.5 28 Fast C~v°linder 83 3U58 16 3074 0.52U% ~ Hand Shelled 84 3UU6 2 3UU8 U,066°!° ~'~' :Hand Shelled 88 2904 2 2996 O.UC~7% Horizontal 2 TOU% 9,3 3U Fast Cylinder 89 21158 1() 2668 0.375% Slotiy Cylinder 90 3()14 ~ 3(11.8 ().133% 125

APPENDIX B. ADDITIONAL TABLES 126

Table B1. Data summary and Tukey significance comparisons between means for pilot study data

Airflow .Insert Repetition Repetition Repetition Repetition Repetition Standard Tukey Duct Speed Damage Type Mean Config t%) 1 Result 2 Result 3 Result 4 Result ~ Resin# Deviation Significance Hand Shelled 2.03 2.10 1.83 1.76 1.97 1.94 0.140 FC - HS 0% Slow Cylinder 1.76 2.08 196 1.62 1.70 1.82 U.19U FC - SC Fast Cylinder 1.85 1.72 1.92 1.58 1..72 1.76 0.130 SC - HS Hand Shelled 2.3:3 2.39 2.52 2.26 2.79 2.46 0.209 FC - HS Config :1 50% Slow Cylinder. 2.25 2.49 2.40 2.39 2.40 2.39 0.085 FC - SC Fast Cylinder 2.4:1 2.47 2.80 2.48 2.54 2.54 0. l 5:1 SC - HS Hand Shelled 3.37 4.C>6 3.39 3.66 3.52 3.60 0.281 FC -1-[S 1O0%~ Slow Cyluider 3.52 3.92 3.60 3.52 3.66 3.64 O.lb4 FC - SC Fast Cylinder 3.91 3.58 3.77 3.98 3.91 3.83 0.158 SC - HS Hand She.iled (1.(100 O.UOU 0.000 U.OUt) 0.00O 0.0(10 0.000 FC - HS O'%u Sloe= Cylinder 0.000 O.pOU O.UO0 0.000 0.000 0.000 U.t)00 FC - SC Fast Cylinder O.C)UU U.UOt) 0.000 0.000 0.000 O.U(K) O.00U SC -HS Hand Shelled 0.066 0.000 U.U67 U.000 U.U67 0.040 0.036 FC - HS* .Horizontal Config 2 5{)% Slo~~~ Cyl.uider O.t)OO O.U66 0.067 0.067 0.067 t).U53 0.[)30 FC - SC* .Fast. Cyli.nde.r 0.195 0.130 0.130 0.130 (}.1:3{) 0.143 {}.029 SC - HS Hand Shelled (}.00(} U.O0U 0.000 U.Ot)0 (1.066 0.013 0.030 FC - HS* 1.00% Slow Cylinder t).066 0.066 0.066 0.067 0.t)66 O.U66 0.00() FC - SC* Fast Cylinder 1).26:1. 0.195 0.261 1).261 0.327 0.26:1 0.046 SC - HS .Hand Shelled 4.06 3.99 3.78 3.86 4.4? 4.()3 0.266 FC - HS 0%, Slo~r~ Cylinder :3.5(} 4.20 3.92 :3.79 =1.07 3.90 0.269 FC - SC Fast Cylinder :3.50 3.77 3.96 3.84 4.37 3.89 ().320 SC - HS Hand Shelled 6.1.8 6.72 4.72 4.92 5.85 5.68 0.843 FC - HS Config 3 S0~% Slow Cylinder 6.2=1 6.02 5.38 5.25 _5.59 5.70 0.423 FC - SC Fast CSLinder 6.43 5.73 5.79 5.66 6.11 5.94 0.325 SC - .HS Haud Shelled 12.4 8.9 13.0 11.9 9.7 11.2 1.77 FC - HS 1.(}()% Slow Cylinder 12.4 lU.l 11.1 11..8 9.4 11..(l .1.22 FC - SC Fast Cylinder 11.1 9.1 9.4 11..:3 9.1. 1(.).0 .1.11 SC - HS Hand Shelled 0.000 0.000 0.000 0.073 -0.073 O.ODU 0.051 FC - HS U'/° Slow Cylinder 0.00{.) 0.()00 0.000 -0.07:3 0.073 (1.000 0.052 FC - SC Fast C}Jli.nde.r U.O{){.) 0.000 0.000 0.072 {).t}{}{) 0.O 14 0.032 SC - HS Hand Shelled t).Ot)t) O.U70 0,000 0.070 0.t)70 0.042 1).038 FC - HS* Config 1 50~%v Slow Cylinder 1).068 0.070 0.070 0.1.39 0.1.40 0.097 0.039 FC - SC* Fast Cy Linder 0.138 0.138 0.138 U.2U6 U.2U5 0.165 O.U37 SC - HS Hand Shelled 0.000 U.U67 0.067 O.U66 0.066 O.U53 0.030 FC - HS* 1(}0% Slow Cylinder {).t)66 0.133 0.133 0.1.33 0.133 0.1.20 O.U30 FC - SC* Fast Cylinder 0.33(.) 0.458 0.523 0.620 0.456 (}.477 O. lU6 SC - HS Hand S1lelled 2.3:1 2.33 2.55 2.78 2.71. 2.54 0.214 FC - HS 0% Slow Cylinder 2.40 2.48 2.41 2.62 2.33 2.45 U.l 11 FC - SC Fast Cylinder 2.30 2.38 2.51 2.17 2.54 2.38 0.154 SC -.HS Hand Shelled 2.81 3.26 3.29 3.20 3.33 3.18 0.210 FC - HS Angled Config 2 5(}% Slow Cylinder 2.62 3.19 3.07 3.27 3.45 3.12 0.31.(} FC - SC :Fast. C~-Linder 2.9Ei 3.34 3.41 :3.26 3.48 3.29 0.201 SC - HS Hand Shelled 5.05 4.45 4.99 5.2.5 4.98 4.94 0.298 FC - HS 1()[)°/u Slow Cylinder 4.52 4.44 5.31 =1.65 4.65 4.71 0.344 FC - SC Fast. Cylinder 3.91 4.29 5.02 =1.88 5.27 4.68 0.559 SC - HS Hand Shelled 0.728 (}.725 1.095 0.798 (}.509 0.771 0.21.1 FC - HS 0% Slow Cy°finder 0.727 0.651 0.727 0.727 0.729 0.712 0.034 FC - SC Fast Cylinder 0.646 0.839 0._576 0.646 O.T17 0.685 0.100 SC - HS Hand Shelled 0.897 0.913 (1.972 0.839 0.836 0.891 0.(156 FC - HS* Config 3 5()%, Slow Cyliruler 0.945 0.837 0.901 0.839 U9U4 ().885 0.046 FC - SC* Fast Cylinder 1.30 1.17 1.23 0.96 0.96 1.12 0.159 SC - HS Hand Shelled l .2{) 1.40 1.40 l .06 .1.20 l .25 0.144 FC - .HS* 1{)U% Slow Cylinder. 0.995 1.13 1.26 1.13 1..13 1.13 O.O95 FC - SC* Fast Cylinder a.43 1.76 :1.76 :1.24 1..50 1..54 t).224 SC - HS Hand Shelled 0.177 ().U(~ 0.0(}U Phoenix Meter -Fast Flow Rate 0.000 ().1.71 0.07(.) 0.095 FC - HS* Slow Cylinder (Pulsesls) 0.987 1.65 1.13 1.30 1..50 1..31. ().269 FC - SC* .Fast C~- li.nde r 7.64 _5.91 6.72 5.65 6.26 6.44 0.785 SC - HS* Ha.ad Shelled O.OUO 0.000 0.1 l4 U.U58 Phoerux Meter -Slow Flo~ti- Rate 0.117 (}.058 U.U58 FC - HS* Slow Cylinder ().8fi9 0.638 (Pulsesls) 0.74? O.fi95 1..27 0.844 0.253 FC - SC* Fast Cylinder 3.03 3.37 4.66 4.51 5.33 4.18 1).955 SC - HS 127

Table B1. Continued

~rflo~~ Insert :Repetition Repetition Repetition Repetition Repetition Standard Tukey Duct Speed Damage Type Mean Config i Result 2 Result 3 Result 4 Result 3 Result Deviation Significance t /mil Ha.ad Shelled ().(1()0 0.447 0.2(10 0.21.0 0.200 0.212 U.1 S9 FC - HS* BCFIVI (%) Slow Cylinder 0.205 0.579 (1.389 0.388 0.485 0.409 0.139 FC - SC* Fast Cy.li.nder 2.58 2.55 2.62 2.56 2.63 2.59 0.034 SC - HS Hand Shelled U.209 0.409 (}.194 0.202 ().687 0.34{.) 0.214 FC - HS* Visual Damage {%} Slow Cylinder 2.95 S.BI 1.20 2.92 3.2() 3.22 1.66 FC - SC* .Fast. Cylinder .19.8 1.7.3 16.2 26.5 22.1. 20.4 4..1 l SC - HS Hand Shelled 1 1 1 0 1 0.800 0.447 FC - HS* Chowdhuty Test Slow Cylinder 3 2 1 2 2 2.00 U.7U7 FC - SC* Fast Cylinder 6 4 5 6 7 5.60 1.14 SC - H S Hand Shelled 2.19 2.82 3.08 4.00 5.41 3.50 1.25 FC - HS* Green .Dye (%~) Slow Cylinder 13.4 15.6 9.78 15.1 12.1 13.2 2.38 FC - SC* Fast Cylinder 34.(.) 48.3 46.2 52.8 s8.6 48.() 9.17 SC - HS* Hand Shelled 57.7 58.2 58.0 58.2 57.2 57.9 0.422 FC - HS Tcst Weight (lblbu) Slow Cylinder 57.5 57.5 56.8 57.4 57.7 57.4 0.342 FC-SC Fast Cylinder 57.9 57.8 58.3 57.8 56.6 57.7 0.638 SC - HS Hand Shelled 14.3 15.0 I5.3 15.6 15.3 15.1 0.495 FC - HS Moisture Content (%) Slow Cylinder 14.4 14.0 14.4 14.3 1.4.1. 1.4.2 0.182 Fc-sc Fast Cylinder 12.2 12.O 12.5 12.9 1.2.8 1.2.5 0.383 SC - HS

* Indicates a sigiuficant pair

Table B2. Data summary and Tukey significance comparisons between means for low m oisture data

Airt~ow l:nsei-t Repetition Repetition Repetition Repetition :Repetition Standard Tukey :Duct Speed Damage Type Mean Confii; 1 Result 2 Result 3 Result 4 Result g Result Deviation Significance ( /,l HaY~d Shelled U.U67 0.067 0.067 0.067 0.000 0.053 0.030 FC - SC* Horizontal Config 2 I00% Slow Cylinder 0.066 0.133 0.133 0.133 0.067 0.106 0.036 FC - HS* Fast C~Jlinder 0.325 0.194 0.389 0.325 0.392 1).325 0.080 SC - HS Hand Shelled U.(167 0.134 0.133 0.067 0.067 U.U93 0.037 FC -1-S* Config 1 lOt)% Slow Cyliuler 0.265 0.199 0.453 0.199 0.265 0.276 0.104 FC - SC* Fast Cylinder 0.454 0.518 0.443 0.520 0.395 0.466 0.053 SC - HS* Angled Haad Shelled :1.07 1.:13 1.()6 0.878 :1..46 1..12 0.21.4 FC - SC* Coniig 3 1(.l()°/u Slow Cylinder .1..1.9 1.39 1.39 1.32 .1.26 1.3.1 0.()87 FC - HS* Fast. Cylinder 1.94 1.87 2.U1 2.08 2.()7 2.00 0.()88 SC - HS Hand Shelled t).6fi:l. 0.666 o.000 u.665 o.UUo 0.398 0.363 FC - SC* Phoenix Meter -Fast .Flow Rate Sloe Cylinder 1.98 6.28 1.65 3.63 2.32 3.17 1.89 FC - HS* {Pulses/kg) Fast. Cylinder 12.0 27.4 6.11 18.0 8.37 14.4 8.55 SC - HS Hand Shelled 0.665 0.333 0.665 U.UOU 0.332 0.399 0,278 FC - SC* Phoenix :M:eter - Slo~~~ Flow Rate Slow Cylinder =1.62 1.32 2.97 2.31 3.30 2.91 1.22 FC - HS* (Pulseslkg) Fast Cylinder 31.9 7.40 20.0 6.:1.2 1.8.4 16.7 10.5 SC - HS Hand Shelled 0.198 O.U00 o.oao O.00t) 0.()00 O.t)40 {).089 FC - HS* BC:FM (%) Slow Cylunder u.4I4 0.606 0.690 0.489 0.426 O.S25 0.12U FC - SC* Fast Cylinder 2.46 3.02 2.44 2.53 2.46 2.58 0.249 SC - HS* Hand Shelled 0.576 0.554 1.333 0.640 0.888 0.798 0.327 FC - HS* Visual .Damage (%) Slow Cylinder 5.56 5.83 4.72 4.58 7.24 5.59 1.t17 FC - SC* Fast Cylinder 23.5 23.1 2U.7 26.4 28.1 24.4 2.90 SC - HS* Hand Shelled 2 3 3 3 2 2.60 1).548 FC - SC* Clnowdhury Test Slow Cylinder 2 3 6 4 S 4.OU 1.58 FC - HS* Fast C~Tlinder 9 11 lU 13 11 10.80 1.48 SC - HS Hand Shelled 0.(10() 0.832 U.0(i(1 0.830 0.821 0.497 0.=153 FC - HS* Green .Dye (`%) Slow Cylinder 5.38 8.69 6.81 8.43 9.63 7.79 1.68 FC - SC* Fast Cylinder 3O.7 34.8 28.8 27.7 35.1 31.4 3.37 SC - HS* Hand Shelled 53.2 52.9 53.2 52.9 53.4 53.1. 0.217 FC-SC Test. Weight (Ib/bu) Slow Cylinder 51.8 52.5 53.3 52.5 53.5 52.7 0.687 FC - HS* Fast Cylinder NTissing 50.9 52.0 51.8 52.8 51.9 0.780 SC - HS Hand Shelled 19.4 2U.8 21.7 :19.7 a9.7 20.3 ().966 FC - H S Moisture Content (%) Slow Cylinder 20.5 19.9 19.7 21.0 19.8 2U.2 0.554 FC-SC Fast Cylinder 23.3 22.3 21.3 21.6 2U.(1 21.7 1.22 SC - HS

* Indicates a significant pains-ise comparision at 0.05 significance level. FC =Fast Cylinder, SC =Slow Cylinder, HS =Hand Shelled 129

Table B3. Data summary and Tukey significance comparisons between means for mid moisture data

AirtloFv Insert Repetition Repetition Repetition Repetition :Repetition Standard Tukey Duct Speed Damage Type Mean Confi.g 1 Result 2 Result 3 Result 4 Result S Result Deviation Significance { ~„~ Hand Shelled 1).067 0.000 U.U67 U.{)67 0.1}00 {},04{} (},Q37 FC - HS* Horizontal Config 2 i00% Slow Cylinder 0.133 0.133 0.133 0.066 0.133 0.119 0.030 FC - SC* Fast Cylinder 0.325 0.389 ().325 0.325 0.325 0.338 0.()29 SC - HS* Hand Shelled U.()b7 t}.1:33 ().067 0.133 {).1.33 {}.107 0.036 FC - HS* Config 1 1()0% Slow Cyliuler 0.199 0.210 0.199 0.199 0.133 0.188 0.031 FC - SC* Fast Ctilinden 0.4SS 0.520 0.585 0.585 0.584 0.546 0.058 SC - HS* Angled Hand Shelled :1.27 1.27 1.2U 1.20 ().93 1..17 0.139 FC-SC* Config _3 100% Slow Cylinder l ..13 1..39 1.4fi :1.33 .1.26 1.3.1 0.124 FC-HS* Fast Cylinder 2.1)2 1.95 :1.89 :1.75 1..88 1..9{~ ().098 SC-HS Hand Shelled 0.665 1.33 0.000 0.998 1.330 0.864 0.556 FC-SC Phoenix Meter - :Fast Flo~~~ Rate Slow Cylinder 4.30 3.64 5.29 =1.96 4.30 4.50 0.644 FC-HS* (Pulses/kg) Fast Cylinder .11.3 0.332 7.42 13.9 15.2 9.61 5.97 SC-HS Hand Shelled 1.59 2.77 3.32 1.99 2.32 2.4U 0.675 FC - HS* Phoenix Meter - Slo«~ Flow Rate Slow Cylinder 8.64 9.26 6.94 6.95 9.25 8.21 1.18 FC - (Pulseslkg) SC* Fast Cv.linder 29.4 32.6 29.1 38.7 31.3 32.2 3.90 SC - HS* Hand Shelled U.()UU 0.192 0.000 0.000 0.000 U.U38 0.()86 FC - HS* BC:FM (%) Slow Cylinder 0.438 0.610 0.688 0.578 0.647 0.592 0.096 FC - SC* Fast Cylinder 2.50 2.91 2.59 2.24 2.58 2.57 0.240 SC - HS* Hand Shelled 0.699 0.788 0.459 1.502 0.332 0.756 0.455 FC - HS* Visual .Damage ("/°) Slow Cylinder 5.73 6.3() 7.$4 6.39 6.68 6.59 0.780 FC - SC* Fast Cylinder 23.3 22.6 23.9 30.2 28.7 25.8 3.45 SC - HS* Hand Shelled 6 6 4 6 5 S.4U 0.894 FC-SG* Chowdhury Test Slow Cylinder 7 8 8 7 8 7.6U 0.548 FC-HS* Fast Cylinder 10 10 11 Z.1 .14 13.2 4.66 SC-HS Hand Shelled 0.000 0.429 0.855 0.846 0.210 0.468 0.381 FC - HS* Green Dye ('%) Slo~7 Cylinder 7.0=1 9.56 6.81 8. lU 8.23 7.95 1.10 FC - SC* Fast Cylinder 25.3 28.3 23.7 33.:1 29.7 28.11 3.fi9 SC - HS* Hand Shelled 5().2 50.7 51.2 50.3 49.9 5().S 0..503 FC-HS Test. Weight (Ib/bu) Slow Cylinder 50.1 49.6 49.9 =19.8 50.4 50.0 0.305 FC-SC Fast Cylinder =19.3 50.9 5a.4 49.6 50.2 50.3 0.876 SC - HS Hand Shelled 22.2 22.5 22.7 23.2 22.2 22.6 0.416 FC - HS Moisture Content (%) Slow Cylinder 23.3 23.0 22.6 22.5 23.1 22.9 0.339 FC-SC Fast Cylinder 22.6 22.5 21.9 23.7 23.5 22.8 0.747 SC - HS

* Indicates a sigiuficant pain{-ise comparision at 0.05 sigluficance level. FC =Fast C~-linder, SC =Slow Cylinder, T-iS =Hand Shelled 130

Table B4. Data summary and Tukey significance comparisons between means for high moisture data

Airflof~~ l:nsert Repetition Repetition Repetition Repetition Repetition Standard Tukey Duct Speed Damage Type Mean Config 1 Result 2 Result 3 Result 4 Result S Result Deviation Significance t /mil Hand Shelled 0.067 0.067 0.077 0.067 O.U67 0.069 0.004 FC - HS* Horizontal Config 2 l0U% Slow Cylinder 0.144 0.133 0.133 0.133 0.133 0.135 0.005 FC - SC* Fast Cylinder 0.323 1).388 0.389 0.452 0.375 t).385 0.046 SC - HS* Hand Shelled 0.133 0.067 (x.067 0.067 0.067 0.080 U.C130 FC - HS* Colll:lg 1 10()°1a Slaw Cylinder 0.199 0.199 0.198 0.199 U.2()() U.199 0.(}Ot) FC - SC* Fast Cylinder 0.583 0.519 0.454 0.583 t}.521 0.532 0.054 SC - HS* Angled Hand Shelled :1.47 1.34 1.27 1.34 :1..1.3 1,31. 0.122 FC - SC* Config 3 100% Slow Cylinder l .66 1.33 1.19 :1.26 1.39 1.37 0.180 FC - HS* Fast C~`linder 2.39 2.0() 1.87 1.90 2.07 2.05 0.209 SC - HS Hand Shelled 3.98 MISSING 0.000 1.47 0.915 1..59 1..70 FC - SC :Phoenix Meter - :Fast .Flo«~ Rate Slow Cylinder 3.14 4.59 2.1S 5.48 4.66 4.00 1.34 FC - HS* (Pulses/kg) Fast Cylinder 6.54 5.50 7.73 3.42 11.45 6.93 2.98 SC - HS Hand Shelled Phoenix Meter - Slo~~~ Floti~° Rate Slow Cylinder (Pulseslkg) MISSING DATA Fast Cylinder Hand Shelled t).000 0.00() 0,000 O.Ot)0 0.t)00 O.t)t)0 0.0t)t) FC - HS* BC:FM (%) Slotiv Cylinder 0.87:5 0.667 0.625 0.607 0.483 0.651 0.143 FC - SC* Fast C~Tlinder 2.53 2.63 2.97 2.42 3.05 2.72 0.276 SC - HS* Hand Shelled 0.40.1 0.786 (1.234 :1.30 0.207 0.585 0.46:1 FC - HS* Visual .Damage (%) Slow Cylinder 6.72 5.92 5.76 6.62 6.26 6.26 0.422 FC - SC* Fast Cylinder 19.3 21.2 20.2 19.8 21.4 2U.4 0.903 SC - HS* Hand Shelled 5 6 4 4 5 4.8t) 1 FC - HS Chowdhury Test Slow Cylinder 1 2 5 2 1 2.20 2 FC - SC Fast Cylinder 2 2 2 4 8 3.6U 3 SC - HS Haim Shelled ().508 0.119 (1.119 U.96 9 0.380 0.419 ().3 ~ :1 FC - HS* Green Dye (~/°) Slow Cylinder 6.54 5.71 11.OS b.02 6.51 7.17 2.20 FC - SC* Fast Cylinder 2().4 24.7 25.1 21.6 20.9 22.5 2.21 SC - HS* Hand Shelled 49.2 48.5 49.2 48.4 48.4 48.7 0.422 SC - FC* Test. Weight (lb/bu) Slow Cvlilder 50.2 49.5 SU.2 48.8 49.5 49.6 0.586 sc - Hs* Fast Cylinder 48.5 49.3 48.9 48.8 48.4 48.8 0.356 HS - FC Hand Shelled 26.3 26.8 26.6 27.1 27.2 26.8 0.367 FC - HS* Moisture Content (%) Slow Cylinder 29.4 27.4 27.3 28.0 27.6 27.9 0.859 FC - SC* Fast Cylinder 28.5 29.1 29.8 29.9 29.7 29.4 0.592 SC - HS*

* Indicates a sigiuficaut painvise comparision at 0.05 significance level. FC =Fast Cylinder, SC =Slow Cylinder, HS =Hand Shelled 131

Table B5. Correlation coefficients for pilot study data

Airflow Insert Sp`,E,a Standard Repetition 1. Repetition 2 Repetition 3 Repetition 4 R.epetitivn 5 Mean Z Duct Mean R Config (° /°} Test Correlation Correlation Correlation Correlation Correlation Correlation BCFM: -0.238 -1.000 0.247 -0.743 -0.491 -0.445 0.198 Visual -0.294 -0.996 0.302 -().781 -0.541. -0.462 0.213 0~~0 Cho~~dhury -0.397 -0.980 0.405 -0.844 -0.629 -0.489 0.239 Green :~ e -0.366 -0.986 0.374 -().82fi -0.603 -0.481 0.232 BCFM 0,845 0.399 0.924 0.816 -0.234 0.554 0.307 Visual 0.813 0.=#51 U.90U 0.866 -0.290 0.548 U.3UU Config 1. S(}~% Chowdhury 0.744 0.546 0.847 ().t)15 -(.).392 0._532 {).283 Green D~~ e 0.766 0.518 0.864 0.901 -0.361 0.538 0.289 BCFM 0.981 -0.977 0.882 0.932 0.964 O.SS6 {}.310 Visual 0.99:1 -0.988 0.907 0.909 0.978 O.S60 0.31.3 100% Cho«~dliury 1.000 -0.999 0.948 0.859 0.995 0.560 0.314 Green Ih a 0.998 -0.997 0.937 0.875 0.991 0.561. 0.315 BCFM Visual 0% Cha~~~dhury NO RESPONSE Green Dv e .BCFM 0.9 l ~ 0.896 0.997 0.896 0.997 0.940 0.884 Visual 0.890 0.920 0.991 0.920 0.991 0.942 0.888 Horizontal Config 2 50%► Cho~i-dhury ().835 o.95x 0.971 0.957 0.971 0.938 o.88c) Green D~~•e 0.853 0.947 t).978 0.947 0.978 0.941. 0.885 BCFM 0.985 0.965 0.985 0.985 0.997 0.984 0,967 Visl~al 0.993 0.979 0.993 0.993 0.991 0.990 0.980 1()0'% Chowdhury 1.000 0.995 l .o00 l.000 0.971 0.993 0.986 Green D~-e ().999 0.991 0.999 0.999 0.978 0.993 {).987 BCFM -0.574 -0.844 U.75U 0.081 0.208 -0.076 U.0U6 Visual -0.62() -0.811 0.787 ().023 0.1.51 -0.094 0.009 0% Cho~~~dhury -0.702 -0.743 t).8.50 -0.086 0.042 -0.:128 ().0 1.6 Green Dvc -0.678 -0.765 0.832 -0.053 0.075 -0.118 0.014 BCFM 0.085 -0.780 ().836 0.925 0.82:3 0.557 ().311 Visual 0.993 -0.815 0.866 0.945 0.788 0.556 0.309 Config 3 SU% Chowdhury 1..0(}0 -0.874 0.915 0.975 0.71.7 0.547 (}.299 Green D~-e 0.999 -0.857 0.901 0.967 0.740 0..5.50 0.303 BCFM -0.995 -0.282 -0.885 -().998 -0.921 -0.816 0.666 Visual -().988 -0.226 -().911 100% -1.000 -().942 -0.813 0.661 Chor~dhury -0.965 -0.118 -0.951 -0.995 -0.973 -0.800 0.641 Green Dve -0.973 -0.151 -().94() -0.998 -0.9(iS -0.805 {).649 132

Table B5, Continued

Aip Insert °~ Standard Repetition 1 Repetition 2 Repetition 3 Repetition 4 R.epctition 5 Mcan Duct S ccd Conti Tcst Correlation Correlation Correlation Correlation Correlation Correlation Mean RZ g f°lol :BCFM: 0.429 U.U75 0.252 0. U64 Visual 0.376 t).1.:33 0.254 0.065 0`~0 NO RESPQNSE Chowdhury 0.273 0.240 u.256 u. u66 Green Dy e 0.305 0.207 (.).256 t}.066 BCFM 0.905 0.997 0.897 0.896 0.890 0.91.7 0.841 Visual 0.928 0.991 0.921 0.920 0.915 0.935 0.875 Config 1 50%~ Cho«~dhury 0.963 0.971 0.958 ().958 (}.954 0.961 0.923 Green Dve 0.954 0.979 u.948 0.947 0.943 0.954 0.910 .BCFM 0.993 0.997 0.998 0.999 0.99Ei (:).997 0.993 Visual 0.998 1.000 1.000 1..000 1..000 0.999 0.999 100'% C11o«'d1111ry 0.999 0.996 0.994 0.991 0.997 0.995 0.991 Green Dye 1.{>{>{> 0.999 0.997 0.995 t).9~)9 0.998 0.996 BCFM -0.543 -0.124 0.176 -0.985 -O.U16 -0.298 0.089 Visual -0.493 -0.066 0.118 -0.993 -0.074 -U.3U1 U.U91 0%~ Cho~.~'dhury -0.395 0.043 O.UU9 -1.000 -0.182 -0.305 0.093 Green Dye -0.426 0.010 0.043 -0.999 -0.149 -0.304 0.093 BCFM 0.781 0.836 u.729 ().374 u.719 u.68s 0.473 Visual 0.744 0.803 0.688 0.427 ().758 0.684 t}.468 Angled Config 2 50`% Cho~~'dhury 0.666 0.733 0.605 0.524 0.825 0.671) 0.450 Green DyTe 0.691 0.755 0.631 0.495 0.806 0.676 0.456 BCFM: -0.9.17 -0.999 -().356 -0.2(:)6 0.8(}5 -0.335 0.1.12 Visual -0.939 -0.995 -u.3u2 -0.262 0.769 -0.346 0.119 100%► C1loiiidliuty -0.971 -0.978 -0.196 -0.366 O.Ei95 -0.363 (}.1.32 Green Dve -0.962 -o.98s -(}.228 -0.334 0.71.9 -0.3.58 0.128 BCFM -().998 0.889 -0.775 -().915 0.525 -0.255 O.O65 Visual -0.992 0.861 -0.810 -0.937 0.573 -0.261. 0.068 U"/o Cho«'dhury -0.972 0.800 -0.869 -0.970 0.659 -0.270 O.U73 Green Dve -0.979 0.819 -0.852 -().961 0.634 -0.268 0.072 BCFM 0.999 u.95s 0.962 0.997 0.87() 0.957 0.916 Visual 1.000 0.940 0.944 0.991 0.897 0.954 0.911 Config 3 S()% Chowdliuryr 0.991 0.897 0.903 0.971 0.9=10 0.940 0.884 Green Dye 0.995 0.911 0.917 0.978 0.928 0.946 0.894 BCFM: 0.851 0.874 0.944 0.951. 0.97(} 0.91.8 0.843 Visual 0.8:19 0.844 ().923 0.967 0.955 0.902 t).813 100% Chops-dhury 0.751 0.781 0.876 0.989 0.916 0.863 0.744 Green Dye (.).773 0.801 ().892 ().984 ().929 0.876 (}.767 BCFM 1..000 0.980 0.997 ().989 0.991 0.991 0.983 Phoenix Meter -Fast Flow Rate Visual 0.999 0.990 1..000 0.996 0.997 0.997 0.993 (Pulses/s) Cho~vdhury 0.990 1.000 0.996 1.00U 0.999 0.997 0.994 Green Dye 0.994 0.998 0.999 1.()(.}0 1.000 0.998 0.996 BCFM 0.979 0.995 0.999 0.998 0.991 0.992 0.984 Phoenix Meter -Slow Flow Rate Visual 0.989 0.999 1.000 1..000 0.997 0.997 0.994 (Fulses/s} Chowdhury 0.999 0.998 0.994 0.994 1.000 0.997 0.994 Green Dve 0.997 1.000 0.997 0.997 1.000 0.998 ().996 133

Table B6. correlation coefficients for low moisture data

Insert S~O~ Standard Repetition 1 Repetition 2 Repetition 3 Repetition ~# Repetition 5 Mean Duct Contig Test Correlation Correlation Correlation Correlation Correlation Correlation Mean RZ %1 BCFM 0.984 0.934 1..000 (1.998 l..t)OU 0.983 0.966 Visual 0.981 0.938 1.000 0.998 0.999 ().983 0.967 Horizontal Config 2 100%► C11Q~.vdhLll}' 0.987 0.926 ().999 0.996 1.00(} ().982 ().9fi4 Green Dj-e 0.974 0.949 0.999 1..()()0 0.998 0.984 0.968 BCFM 0.937 1.000 0,625 0.994 ().895 0.890 0.792 Visual 0.942 0.999 0.635 0.996 0.9U1 0.894 0.800 Config 1 100%► Choti~dhury 0.93() 1.000 0.609 0.992 0.886 0.883 0.780 Gr+cen Dye 0.953 0.998 0.661 0.998 0.915 0.905 1).819 Angled BCFM 0.999 0.985 0.986 0.982 0.910 0.972 t).946 Visual 0.998 0.987 0.988 0.984 0.904 0.972 0.946 C0I11~1~ 3 100% Chowdhuly 1.000 0.982 0.983 0.978 0.918 0.972 0.9=15 Green D~~•e 0.995 0.992 0.993 0.990 0.x89 0.972 ().945 BCFM 0.998 .1.000 0.997 1..000 0.996 0.998 0.996 Phoenix Meter -Fast :F1o~~- Rate Visilal 0.997 1.000 0.998 0.999 0.997 0.998 0.996 (Pulses/s) Chowdhury 0.999 0.999 0.995 1.000 0.994 0.997 0.995 Gr+cen Dve 0.994 1.000 0.999 0.998 0.999 (.).998 ().996 BCFM 0.998 0.999 0.997 0.979 1..000 0.995 0.989 Phoenix Meter -Slow .Flow .Rate Visual 0.997 0.998 0.997 0.982 0.999 0.995 u.989 (:Pulses/s} ChowdhunT 0.999 1.000 0.999 0.975 1.000 0.994 0.989 Green D1-~e 0.994 0.995 0.993 ().988 0.997 0.993 ().987 134

Table B7. Correlation coefficients for mid moisture data

Airflow In.scrt Standard Repetition 1 Repetition 2 Repetition 3 Rcpetition 4 Repetition 5 Mean Z Duct S i~cd Mcan R Confi P Test Correlation Correlation Correlation Correlation Cor~•elati.on Correlation ~ (%1 BCFM 0.999 0.991. 0.999 0.978 1).978 0.989 0.979 Visual 1.000 0.993 1.000 0.975 0.981 0.990 U.98U Horizontal Config 2 100% Cho~~-dhury 1.000 0.998 1.000 0.9fi2 0.99(} 0.990 0.980 Green D~-e 1.000 0.997 1.000 0.965 0.988 0.990 0.980 BCFM 0.99:1 1.00t) 0.999 (1.997 0.978 0.993 0.986 Visual 0.993 0.999 1.000 0.996 0.975 0.993 0.985 Config 1 100%~ Cho~~Tdhury 0.998 0.996 1.000 0.990 0.962 t:).989 0.978 Green D~- e 0.997 0.997 1..000 0.991 0.965 ().990 0.98() Angled BCFM 0.937 0.999 0.986 1..000 0.99:1 0.983 0.966 Visual 0.932 0.999 0.989 1.00t) 0.993 0.982 0.965 Config 3 100% Cho~~~dhury 0.912 0.995 0.995 0.998 0.998 0.980 0.960 Green D~-e 0.917 0.996 0.994 0.999 0.997 0.980 0.961 BCFM 0.99:1 -0.574 0.850 0.995 1.000 0.652 0,426 Phoenix Meter -Fast Flo~.~~ Rate Visual 0.993 -0.562 0.858 0.997 1.000 0.657 0.432 (Pulses/s) Chowdhury 0.998 -0.518 0.883 1.000 0.997 0.672 0.452 Green D~- e 0.997 -0.528 0.878 0.999 0.998 0.669 ().447 BCFM 0.999 .1.000 0.997 0.996 1..000 0.998 0.997 Phoenix Meter -Slow .Flow .Rate Visual 1.000 1.000 0.995 0.995 1.000 0.998 0.996 (Pulsesls) Chou~dhury 1.000 0.998 0.989 0.988 0.999 0.995 U.99U Green D~-e l..t)Ot) 0.998 0.991 0.990 0.999 0.996 0.991. 135

Table B8. Correlation coefficients for high moisture data

Airflow Insert Standard Repetition 1. Repetition 2 Repetition 3 Repetition 4 Repetition 5 Mean 2 Duct Speed Mean R Contig Test Correlation Correlation Correlation Correlation Correlation Correlation (°~Ql BCFM 0.998 0.999 0.998 (.).998 1..000 0.998 1).997 Visual 1.000 0.996 0.994 0.993 0.997 0.996 0.992 Horizontal Config 2 l0U%, Clio~vdhury -0.251 -0.151 -1).124 -0.118 -0.159 -1).161 t).t:)2Ei Green D~-•e I..00U 0.994 0.991 0.990 ().995 0.994 0.988 BCFM 0.995 0.998 0.994 l..t)00 0.998 0.997 0.994 Visual 0.989 1.000 0.998 0.999 1.000 0.997 0.995 Config 1 100%, Choti~dhury -0.091. -U.24U -0.293 -0.204 -0.242 -f.).214 0.046 Green Dye 0.986 1.000 0.999 0.999 1.000 ().997 0.994 Angled BCFM 0.999 0.970 0.945 0.941 0.999 u.971 ().943 Visual 0.996 0.957 0.928 0.923 1.000 0.961 0.923 Corrfig 3 100% Cho~.i~dhun~ -0.152 0.058 0.145 0.157 -0.229 -0.004 O.00U Green D<<•e ().994 0.951 0.920 0.915 1.00(} 0.956 (}.914 BCFM 0.892 1.000 0.999 0.213 0.992 0.81.9 0.67.1 Phoenix. Meter -Fast :Flow Rate Visual 0.868 1.000 1.000 0.261 0.997 0.825 0.681 (Pulses/s) Chowdliunr 0.279 1.000 -0.227 -1.000 -0.309 -U.U51 U. UO3 Gr+cen Dti~ e 0.857 1.000 1.000 0.281 0.998 0.827 (}.684 BCFM Phoenix. Meter -Slow .Flow Rate Visual (:Pulses/s) Choti~~dhun~ MISSING DATA Green D~-~e