REPORT ON OBJECTIVE RDE QUALITY EVALUATION · the Subjective Ratings (Front Seat) for Bus Run 7 . . . 37 4.2 Listing of Absorbed Power (Six Degrees of Motion) with the Subjective

PTI 7412

REPORT ON

OBJECTIVE RDE QUALITY EVALUATION

Submitted to

NATIONAL AERONAUTICS AND SPACE ADMINISTRATION

by

J. C. Wambold and W. H. Park

March 1974

In Cooperation with the Department of Mechanical Engineering

(NASA-CR-132538) REPORT ON OBJECTIVE N74-34565RIDE QUALITY EVALUATION (PennsylvaniaState Univ.) 244 p HC $15.25 CSCL .05E

UnclasG3/05 17152

https://ntrs.nasa.gov/search.jsp?R=19740026452 2020-07-14T14:11:18+00:00Z

REPORT ON

OBJECTIVE RIDE QUALITY EVALUATION

Submitted to

National Aeronautics and Space Administration

by

J. C. WamboldAssociate Professor of Mechanical Engineering

and

W. H. ParkAssociate Professor of Mechanical Engineering

The Pennsylvania Transportation InstituteThe Pennsylvania State UniversityUniversity Park, Pennsylvania

March 1974

TABLE OF CONTENTS

Page

SUMMARY . .............. .. .. .. ..*...... 1

Objectives . . . . . . . . . . . . . . . . . . . . . . . . 1

Method . . . . . . . . . . .. . . . . . . . . . . . . 1

Conclusion . . . . . . . . . . . . . . . . . . . 2

1. INTRODUCTION . . . . . . . . . . . ....................... . 3

1.1 Problem Statement and Research Objective . . . . . . . 3

1.2 Basic Statistical Measures . . . . . . . . I . . . . . 3

1.3 Historical Review of Comfort Measurement . . . . . . . 4

2. CORRELATION OF OBJECTIVE WITH SUBJECTIVE RIDE RATINGS . . 12

2.1 Objective Ride Criterion . . . . . . . . . . . . . . . 12

2.2 AFD Format for Absorbed Power . . . . . . . . ....... . 13

2.3 Computation of Absorbed Power Using AFD . . . . . . . 13

2.4 Correlation Method for Objective and

Subjective Ride Ratings . . . . . . . . . . . . . . . 17

3. TEST DATA PROCESSING . . . . . . . . . . . . . . . . . . . . 18

3:1 The Two Approaches . . . . . . . . . . . . . . . . . . 18

3.2 The Hybrid Program Method . . . . . . . . . . . . . . 21

3.3 Applied Research Laboratory Program ... .. ...... 25

4. RESULTS OF DATA PROCESSING . . . . . . . . . . . . . . . . 29

4.1 Objective--Bus Data Results . . . . . . . . . . . . . 29

4.2 Subjective Data . ..... ................... . 364.3 Objective--Aircraft Data Results . . . . . . . . . .. 39

5. APPRAISAL OF RESULTS, APPLICATIONS, AND RECOMMENDATIONS . . 46

5.1 Appraisal of Results and Applications . . . . . . . . 46

5.2 Recommendations . . . . . . . . . . . . . . . . . . . 47

REFERENCES . . . . . . . . . . ... . . . . . . . . . . . . . . ..50

APPENDIX A: Human Response to Random Vibration

APPENDIX B: The Amplitude Frequency Distribution (AFD) Method

APPENDIX C: The Hybrid Computer Program

APPENDIX D: Applied Research Laboratory Computer Program

APPENDIX E: Reduced Bus Data

ii

TABLE OF CONTENTS (Continued)

APPENDIX F: Absorbed Power (AP) Bus Correlation Data

APPENDIX G: Bus Seat Transfer Function Data

APPENDIX H: Absorbed Power-ISO Standards Correlation

iii

LIST OF FIGURES

Figure Page

1.1 Basic Elements of AFD, the Amplitude

Frequency Distribution . . . . . ................ . 5

22.1 Absorbed Power Matrix, K.A. , for Run 8, Vertical

Motion . . . . . . . . . I........................ ... 16

22.2 Normalized Absorbed Power Matrix, (K A /M.), for

Run 8, Vertical Motion . . . . . . . . ........... . 16

2.3 Absorbed Power AFD Determined from Experimental

Acceleration for Run 8, Segment 1, Vertical Motion . . . 16

3.1 Digitizing the Data . . . . . . . ................ . . 19

3.2 Determining the Amplitude Frequency Distribution

of a Random Signal: Serial Method . . . . . . . . . . . 19

3.3 Determining Joint Probability Density of a

Random Signal: Parallel Filtering and Digital

Peak Discrimination . . . . . . . . . . . . . . . . . . 20

3.4 Algorithm for Serial Method: General Outline . . . . . 23

3.5 Conversion of Each Filter's Output to Count Peaks

and Store Each Peak's Value . . . . . . . . . . . . . . 24

3.6 Amplitude Discrimination for Each Peak and Counting

AFD . . . . . . . .. . . . . . . . . . • . . . . •26

3.7 Algorithm for Parallel Method . . . . . . . . . . . . .. 27

4.1 Listing for Run 7, Segment 3, Vertical,

Frequency Band 1 ... . . . . . . . . ... . . . . . . 30

4.2 Listing for Run 7, Segment 3, Vertical,

Frequency Band 6 . . . . . . . . . . . . . . . . . . . . 30

4.3 Partial Listing for Run 7, Segment 3, Vertical,

Frequency Band 8 . . . . . . . . . . . . . . . . . . . . 31

4.4 AFD Output, Run 7, Segment 3, Vertical Motion . . . . . 33

4.5 AFD Output, Run 8, Segment 2, Lateral Motion ....... . 34

4.6 Absorbed Power AFD, Run 7, Segment 3, Vertical Motion . 35

4.7 Absorbed Power vs. Subjective Rating for Run 7,

Segment 3, Front Seat of Bus Data . . . . . . . . . . 38

iv

LIST OF FIGURES (Continued)

Figure Page

4.8 Absorbed Power vs. Subjective Ratings for Run 7,Segment 3, Front Seat of Bus with Extreme ValueRemoved . . . . . . . . . . . . . . . . . . . . . . . . 40

4.9 Correlation of Absorbed Power (For Three Degrees ofMotion) with Subjective Bus Ride Data . . . . . . . . . 41

4.10 Composite Plot of Bus Data . . . . . . . . . . . .... 42

4.11 Absorbed Power (For Six Degrees of Motion) vs.

Subjective Aircraft Ride Data .............. . 45

v

LIST OF TABLES

Table Page

2.1 Factors for Absorbed Power Calculation for Run 8,Vdrtical Motion . . . . . . . . . . . . . . . . . . . . 15

4.1 Listing of Absorbed Power (Three-Degree Motion) withthe Subjective Ratings (Front Seat) for Bus Run 7 . . . 37

4.2 Listing of Absorbed Power (Six Degrees of Motion)with the Subjective Ratings for the Three Test Runsof Aircraft Data . . . . . . . . . . . . . . . ....... . 44

5.1 Comparison of the Bus Ride Correlation with the ISOStandard Correlation Using Absorbed Power as theBasis for Comparison . . . . . . . . . . . . . . . . ... 48

vi

SUMMARY

Objectives

This research is concerned with establishing a correlation between

objective and subjective comfort ratings of vehicles. The Absorbed Power

(AP) comfort criterion was used in an Amplitude Frequency Distribution

(AFD) format for the objective measure. The objective ratings were then

correlated with passenger subjective responses.

Method

The method used in this project to reduce analog tape records of

acceleration versus time into a compact and useful form was the Amplitude

Frequency Distribution method. The AFD method, which is a discrete joint

probability of amplitude and frequency, unlike the Power Spectral Density

(PSD) method, retains amplitude distribution data as well as frequency

distribution data.

The Absorbed Power concept of comfort evaluation was then employed

to evaluate ride quality. The Absorbed Power concept uses the power

absorbed by a human body as the measure of discomfort and has been shown to

correlate with subjective response. The acceleration data were put into

AFD format and then transformed into absorbed power, as an objective.ride

measure. This computed objective ride measure was then correlated with the

subjective evaluation for the same ride. Hybrid computer methods were used

to process acceleration and absorbed power data, and for correlation studies.

Correlation studies were based on subjective ride data taken on a city

bus with the objective ride data developed from three-dimensional acceleration-

time histories recorded on the bus. On completion of the correlation of

the bus data, a corresponding six-degree model was developed for future

evaluation of aircraft ride quality.

Conclusion

The correlation of absorbed power as an objective ride measure to

the subjective evaluation for the bus data was successful. For some

individual bus rides the correlations were poor, but when a sufficient

number of rides was used to give reasonable sample base, an excellent

correlation was obtained. The following logarithmical function was

derived:

S = 1.7245 ln (39.6849 AP)

where S = one subjective rating of the ride; and

AP = the absorbed power in watts.

A six-degree-of-freedom method developed for aircraft data was completed

and some preliminary correlations were attempted. However, because of

insufficient data (too small a sample), and since there was no assurance that

the acceleration data were properly matched with the subjective ratings

(exact start-stop times were unknown), the correlation of aircraft data is

not considered to be very exact.

Finally, preliminary correlation of absorbed power with ISO standards

further enhances the bus ride and absorbed power correlation numbers since

the AP's obtained are of the same order of magnitude for both correlations.

While it would then appear that one could just use ISO standards, there is

no way to add the effect of three degrees of freedom. On the other hand, the

absorbed power provides a method of adding the effects due to the three major

directions plus the pitch and roll.

2

1. INTRODUCTION

1.1 Problem Statement and Research Objective

The following is the original work statement from the research

proposal:

It is the object of this research to take vehicle acceleration

versus time data supplied by NASA and perform an objective evaluation

of ride quality for that vehicle/guideway system. The Amplitude

Frequency Distribution (AFD) techniques as applied to the Absorbed Power

method of comfort evaluation previously used on automobile/road roughness

studies by the investigators will be extended to include three degrees

of freedom. This extended method will then be used to evaluate the

subjective ride and acceleration data taken by Old Dominion University

researchers on a city bus. The subjective and objective ride ratings

will then be correlated.

After correlating the above data, work will be initiated to develop

the method to include all six degrees of freedom so that the same or

similar techniques might be applied to aircraft ride data.

1.2 Basic Statistical Measures

Measured records must be recognized as random signals of finite duration

and, as such, they can be viewed and described in terms of three basic

"domains": time, amplitude, and frequency. The time domain description is

the unprocessed signal-versus-time. All types of amplitude domain descriptions

reduce the measured signal to a single number or a table of values which is

mathematically equivalent to computing an amplitude-probability distribution

for the signal. Frequency domain representations of signals are generally

considered to be the most useful. They are based on the concept that any

observed random signal can be reconstructed by adding together a number of

different sine waves.

At first glance, it would appear that the power spectral density con-

tains a complete description of amplitude variations, thus making any

3

amplitude-distribution calculations superfluous. However, the ordinate of

a PSD curve indicates only the average signal amplitude at a particular

frequency. A large PSD value can conceivably be produced by either a few

cycles of large amplitude or a large number with small amplitudes; the dis-

tinction cannot be made from the PSD curve alone. On the other hand, it is

not possible to extract any information about frequency distribution from

amplitude density curves. It is evident from these considerations that the

PSD and amplitude density curves each contain unique information, and a simple

method of combining the two representations is desirable.

An effective method for combining the information contained in both

the PSD and the amplitude representations is to reduce the random time-

history signal to a simple tabular array that displays both the height

and the length features on the random data, as in Figure 1.1. Here the co-

ordinates (linear or logarithmic), amplitude (in feet, g's, etc.) versus

frequency (in Hertz, rpm, cycles per foot, etc.), are divided into a number

of finite bands as shown. Numbers like N are computed and entered at each

window-like intersection of the bands. The numbers express the total number

of signal peaks with the amplitude and frequency of that box in the array.

The complete array of numbers thus identifies the random signal as a com-

bined amplitude and frequency distribution. Thus, the AFD not only gives

the frequency distribution, but also shows the amplitude make-up and

distribution of each frequency band.

1.3 Historical Review of Comfort Measurement

Many experimental investigations concerned with human reaction to

vibration have dealt with the degree of comfort expressed by test subjects.

These individuals were exposed to ride levels associated with various

4

CL10.

N..

__-_Number of CountsE-

Af IFreq. Band

-II I

f.J

Frequency, f

Figure 1.1. Basic Elements of AFD, the Amplitude Frequency Description

5

vibrational frequencies and amplitudes and then were asked to form an

opinion of the ride sensation. For the most part, these experimental

vibrational inputs have been generated in the laboratory, although a few

investigations have been conducted in on-the-road environments. As a re-

sult of these subjective interpretations of the ride environment, several

sets of tolerance curves have been developed to define limits on vibrational

intensity for sinusoidal and random motion.

One of the first studies was conducted in Germany in 1931 by Reiher

and Meister (1). Twenty-five subjects of varying ages were subjected to

horizontal and vertical accelerations while in standing and sitting positions.

After 15 minutes each subject was asked to evaluate his ride and place his

interpretation of roughness into one of six categories, from imperceptible

to intolerable. From these data several tolerance-level curves were

formulated.

In 1933, Jacklin and Liddel (2), using only three ride-level categories

in their study--perceptible, disturbing, and uncomfortable--developed a

mathematical relationship to describe a comfort index. This relationship

utilized both the amplitude and frequency of the vibration.

Several years later, based on a comprehensive review of other tolerance

studies, Janeway (3) developed an equation to describe "comfort level" at

various frequencies due to vertical sinusoidal vibrations. In addition to

vibration amplitude, Janeway considered comfort a function of "jerk," the

first derivative of the acceleration, for frequencies from 1 to 6 Hz, a

function of acceleration between 6 and 20 Hz, and a function of velocity

from 20 to 60 Hz.

Ten Cate (4) also attempted to place different ride levels into

mathematical form, using the principle that a sensation is proportional to

6

the common logarithm to the base 10 of the stimulus intensity. He proposed

a standard vibration intensity unit called a Pal and defined three categories

of comfort from just detectable to troublesome.

Most of the tolerance curves described in the preceding have somewhat

similar shapes. Tolerance generally decreases at very low frequencies,

with a minimum value occurring between 4 and 8 Hz. Above 8 Hz, tolerance

to vibratory intensity increases rapidly. This fact is attributed to the

increased attenuation of the vibration by the human body. Differences

among the comfort criteria, however, are also apparent. The major

difference is due to the definition of ride level by each investigator.

Two particular tests in 1962 warrant mentioning. Snyder (5) reported

the results of a series of studies conducted at the Boeing Company,

Wichita, Kansas. The experiments were designed to establish four levels

of test scores. These scores were to provide a preliminary comparison of

effects of sinusoidal and random vibrations on human performance. Snyder

found "some similarity" in effects on performance for these vibrational

inputs. The most promising relationship between these two vibrations appears

to be a combination of root mean square amplitude, power, and frequency.

Later in the same year, one of the first studies utilizing on-the-

road environments was attempted. To measure "riding comfort," Van Deusen

(6) devised a jury rating system. A group of trained ride-engineers were

asked to assign a number to their impression of the ride on a particular

road. An average number was then assigned to that surface.

Van Deusen then attempted to develop some physical measurement of

ride comfort that would require fewer experimental observations, and, at

the same time, be more objective than jury rating. He measured acceleration

7

at the seat and head of the passenger in three mutually perpendicular

directions. This was done while driving over 38 road sections of a

proving ground course. Measurements of acceleration, velocity, and jerk,

together with subjective jury ratings from the same segment of proving

ground course, were examined for correlation. High correlation was found

for mean square acceleration and mean square jerk in the three directions.

It was also found that the mean square vertical acceleration of the body

correlated 0.815 with jury rating.

In 1965, using the Dynamic Ride Simulator facility at the U. S. Army

Tank-Automotive Center, Holland (7) subjected human subjects to vertical

random vibrations in a systematic manner, testing their ability to perform

simple tasks under vibrational conditions. The experimental results

consisted of their subjective judgments of severity placed on a numerical

scale. He found that direct magnitude estimates provide an effective

method for qualifying the subjective counterpart of random vibratory

motion. The subjective estimates of vibratory roughness depend on the

relative distribution of the frequency spectrum.

In 1966, Butkunas (8), considering all input motion to the passenger

(tactile motion as well as whole-body motion), developed a technique

whereby an overall ride sensation index is formed. He evaluated

acceleration data obtained on 14 different vehicles under four different

road-speed combinations to arrive at his comfort index. These acceleration

measurements were taken on the seat cushion, seat back, and floor pan.

To compute one comfort index from these three measurements, each

measurement was processed through a weighing function--weighing the PSD

spectra with the frequency response of the "man." The resulting weighed

8

spectra were integrated over the frequency range and summed. The square

root of this sum gives the final comfort index.

The techniques of comfort evaluation mentioned above have been

generally restricted to sinusoidal inputs generated in the laboratory.

Since road surface irregularities are random in nature, these investiga-

tions fail to provide an accurate picture of the situation. Moreover, the

investigators who have conducted on-the-road experimentation have relied

on subjective interpretations of ride comfort from trained individuals.

These results have also failed to be adequate. Nevertheless,the results

from the above investigations have been a starting point in comfort

evaluation, even though they fail to produce a numerical ride index with

physical interpretation in regard to passenger response.

In 1966, to overcome the existing research trend of heavy emphasis

on experimental tests to assess the effects of mechanical vibration on

comfort measurement, Pradko and Lee (9, 10, 11) introduced a new comfort

parameter called "absorbed power." Absorbed power is an energy flow rate

dependent on the anatomical properties of the human body and relatable to

passenger subjective responses. It was developed, without prior knowledge

of the frequency spectrum, to describe human dynamics. Absorbed power tech-

niques are discussed in Chapter 2 and in detail in Appendix A.

An International Standards Organization (ISO) standard defining human

tolerance to whole-body vibration has been under development for a number of

years. It is understood that it has received the necessary approval by ISO

member nations and is likely to be published shortly. A Draft International

Standard (ISO/DIS 2631), "Guide for the Evaluation of Human Exposure to

Whole-Body Vibration," was submitted on April 28, 1972, and voted on by

9

August 28, 1972. It seems likely that European countries will incorporate

the ISO document into their own new standards and replace existing

standards of which the most significant is that of the German VDI (12).

Three degrees of disturbance are postulated: reduced comfort, fatigue

decreased proficiency, and an exposure limit above which an acute physical

hazard due to the vibration is considered to exist. The standard suggests

methods of dealing with broad frequency band linear vibration in a given

direction, but does not deal adequately with combined effects of different

directional vibration components or effects of rotational vibration.

The limitations of this standard are well known by its originators,

and it has been stressed that the criteria suggested must be confirmed in

each individual type of vibration environment. There are two further

limitations of the draft standard: first, it deals with vibration only

above 1 Hz, whereas significant amounts of energy even in the vertical

direction exist below 1 Hz; second, two alternative measurement procedures

are specified allowing either (a) third-octave analysis of each vibration

component so that individual frequency components can be compared with the

appropriate limiting criteria for that frequency, or (b) averaging of a

component vibration in a frequency-weighted meter with a total effect

indicated from the weighting.

In relation to the effect of vibration below 1 Hz, recent analysis of

the published data by Allen et al. (13) suggests that the tolerance again

drops, to be no higher than that in the 4 to 8 Hz frequency range.

Experiments to determine the significance of pitch and roll motions have

been reported from Italy (14), but there has been little confirmation of

the tolerance data.

10

More recent work in ride quality was reported at the first symposium

held on vehicle ride quality (15). This symposium was conducted by the

National Aeronautics and Space Administration at the Langley Research

Center. While all of the papers presented at this symposium are pertinent,

one is singled out here. Vinje (16) reported on analytical and experimental

evaluation of proposed ride comfort criteria at United Aircraft Research

Laboratories. He reported a lack of correlation between index and rating

due to human tendency to rate ride relative to average ride rather than

to an absolute standard. He further noted that one must know how the bumps

occur rather than compute their average and that somehow this must be taken

into account to establish an index.

Since the first symposium in Summer 1972, there have been ride quality

workshops held about every six months to allow people in the ride quality

area to exchange ideas. Unfortunately, no formal documentation of these

meetings is available. However, some notes and list of attendees can be

obtained from the VSTOL office at NASA Langley.

In November 1973, the Council for Advanced Transportation Studies,

University of Texas at Austin, published "Literature Survey on Passenger

and Seat Modeling for the Evaluation of Ride Quality" (17) as a research

memo to the Department of Transportation (DOT OS 30093RM8). While this is

not 100 percent complete, it is an excellent working survey for anyone in

the ride quality area.

11

2. CORRELATION OF OBJECTIVE WITH SUBJECTIVE RIDE RATINGS

2.1 Objective Ride Criterion

The objective ride measures used in this study are based on the concept

of absorbed power. This criterion was developed by researchers at the Army

Tank Automotive Command (9, 10, 11) and is based on an energy flow rate

which is dependent on the anatomical properties of the human body. The

human body properties were determined experimentally and the absorbed power

was related to passenger subjective responses. The basic concepts of

absorbed power are given in detail in Appendix A.

The information needed for the determination of absorbed power is the

acceleration at the interface between the passenger and the vehicle. The

experimental data which was used as input had been obtained prior to

initiation of this project and consisted of three-directional accelerations

measured on the floor of a bus using a NASA instrument package. These

accelerations in the vertical, longitudinal, and lateral directions were

measured near the front of the bus and simultaneously near the center of

the bus, and recorded on magnetic analog tape. The accelerations were not

measured at the passenger seat interface, but were used in this initial

project to see if the absorbed power criterion might correlate to subjective

passenger response. Seat transfer characteristics were determined and

proved to be of little consequence. Future work should require that the

accelerations be measured at the proper location or seat transfer character-

istics will have to be determined for every case.

Absorbed power can be computed from the acceleration data in either

the time or frequency domain for each direction. Since power is a scalar

12

quantity, the total power can be obtained by summing the power in all

three directions. For this study, the frequency method was used since

the results would reveal those frequency bands that contribute to the

greatest discomfort. The format for the calculations is shown by Equation

A.6 (Appendix A) as follows:N

Average AP =E K.A. 2

i=o Ii RMS

Where AP = the absorbed power in watts;

, = the root mean square of the acceleration at a given frequency; and

RMSK. = the parameter used to transform the acceleration squared into absorbed

1

power at a given frequency.

Before giving the calculation details, the AFD concept for formatting the data

will be presented.

2.2 AFD Format for Absorbed Power

The AFD method has been found useful in making comfort measurements

because it readily identifies both amplitude and frequency bands of the

acceleration inputs that are causing the discomfort to the vehicle passenger

(18). Details of this method, which can be used on any random data, are

given in Appendix B. The acceleration data for each of the three directions

were filtered into eight frequency bands and peaks were placed in six

amplitude bands.

2.3 Computation of Absorbed Power Using AFD

The seat acceleration AFD is the beginning point for comfort evaluation

by the Absorbed Power method. As indicated above, Equation A.6 shows

that the total absorbed power for a vibration spectrum is the summation of

13

the power at each frequency. The K values are for frequencies in Hz,1

which can be obtained by multiplying the mid-frequency by the vehicle

speed in fps. Since each block of the seat acceleration AFD has a mid-

amplitude and a mid-frequency value, the average absorbed power attributable

to each AFD can be calculated from Equation A.6. Intermediate values for

this calculation are based on run 8, vertical motion, and are shown in

Table 2.1. The resultant absorbed power matrix is shown in Figure 2.1.

This value of absorbed power shown in each block, however, would be the

power absorbed by a passenger subjected totally to an acceleration of that

mid-frequency and mid-amplitude value. To take account of the fact that the

actual acceleration consists of various frequencies and amplitudes, the

absorbed power matrix is normalized by dividing each block by the maximum

number of counts that would be shown by a sine wave of that mid-frequency

for that length of time. For example, the last column has a mid-frequency

of 11.314 Hz. Any amplitude sine wave of that frequency would produce

169.7 counts in that time. These numbers of counts could be termed M. and

are calculated for each frequency. By dividing the absorbed power matrix

by the M. values, a new matrix is obtained which will be called the Normalized1

Absorbed Power Matrix (NAPM). Each block of the NAPM is then K.A. 2 /M. which

isequal to the absorbed power contribution per count of the seat acceleration

AFD. These values are shown on the matrix of Figure 2.2. The NAPM matrix

shows those areas which contribute the most to absorbed power (or discom-

fort) and, thus, gives a picture of the amplitudes and frequencies that

contribute to a comfortable ride.

To determine the absorbed power for a particular ride segment, the NAPM

is multiplied block by block with the seat acceleration AFD to give the

14

Table 2.1. Factors for Absorbed Power Calculationfor Run 8, Vertical Motion

Absorbed PowerMid-Frequency Constant K.

1f/e2)2Hz Watts/(ft/sec2 2

0.088 0.000082

0.177 0.00033

0.354 0.001325

0.707 0.005631

1.414 0.02460

2.828 0.12150

5.657 0.14595

11.314 0.03647

15

0.401 0.00682 0.02746 0.11024 0.46851 2.04678 10.10910 12.14340 3.03440

0.257 0.00281 0.01132 0.04543 0.19309 0.84354 4.16625 5.00465 1.25056

- 0.165 0.00116 0.00466 0.01872 0.07958 0.34765 1.71703 2.06256 0.51539

0.101 0.00048 0.00192 0.00772 0.03280 0.14328 0.70764 0.85004 0.212410

< 0.069 0.00020 0.00079 0.00318 0.01352 0.05905 0.29164 0.35033 0.08754

S0.044 0.00008 0.00033 0.00131 0.00557 0.02434 0.12019 0.14438 0.03608

0.088 0.177 0.354 0.707 1.414 2.828 5.657 11.314Mid-Frequency in Hertz

Figure 2.1. Absorbed Power Matrix, KiA 2 (watts), for Run 8,Vertical Motion

0.401 0.00515 0.01035 0.02079 0.04417 0.09849 0.23827 0.14311 0.01788

0.257 0.00212 0.00427 0.00857 0.01820 0.03976 0.09820 0.05898 0.00737*r

4

4 0.165 0.00087 0.00176 0.00353 0.00750 0.01639 0.04047 0.02431 0.00304

0.101 0.00036 0.00072 0.00146 0.00309 0.00675 0.01668 0.01002 0.00125U

<4 0.069 0.00015 0.00030 0.00060 0.00127 0.00278 0.00687 0.00413 0.00052

0.044 0.00006 0.00012 0.00025 0.00053 0.00115 0.00283 0.00170 0.00021

0.088 0.177 0.354 0.707 1.414 2.828 5.657 11.314

Mid-Frequency in HertzFigure 2.2. Normalized Absorbed Power Matrix (NAPM), (Ki A.2/M ) (watts

per count), for Run 8, Vertical Motion

S0.401 0.000 0.000 0.021 0.044 0.000 0.000 0.000 0.000S0.257 0.000 0.004 0.000 0.000 0.000 0.000 0.000 0.000

S0.165 0.000 0.002 0.004 0.000 0.000 0.000 0.000 0.003

0.101 0.000 0.000 0.000 0.003 0.000 0.000 0.000 0.010

U 0.069 0.000 0.000 0001 0.000 0.008 0.000 0.004 0.023IS0.044 0.000 0.000 o000o 0.001 0.002 0.008 0.017 0.011

0.088 0.177 0.354 0.707 1.414 2.828 5.657 11.314

Mid-Frequency in Hertz

Figure 2.3. Absorbed Power AFD Determined from Experimental Accelerationfor Run 8, Segment 1, Vertical Motion

absorbed power AFD as shown in Figure 2.3 for run 8, segment 1, verti-

calmotion. The absorbed power AFD shows the amount of power attributed

to each frequency and amplitude block for the guideway and vehicle being

examined. The absorbed power for each frequency band can then be

obtained by summing the blocks vertically, or the total absorbed power

can be obtained by summing all the blocks. The absorbed power AFD's and

totals are given in Appendix E.

2.4 Correlation Method for Objective and Subjective Ride Ratings

The subjective ride ratings from the Old Dominion bus study were

given by the two passengers seated directly over each instrument package

used to record the floor accelerations. The correlation simply consisted

of plotting the total absorbed power for all three directions against the

ride rating number assigned by the passenger. The results are shown in

Chapter 4.

17

3. TEST DATA PROCESSING

Programs were developed for two different computers, a hybrid

computer in the Penn State College of Engineering and a Systems 95

digital computer in the Applied Research Laboratory (ARL). However, only

the ARL computer was used to process the data in this investigation.

The first section of this chapter describes the two basic approaches

used, the second describes the hybrid program, and the third describes the

ARL programs. The actual programs are listed in Appendixes C and D.

3.1 The Two Approaches

Once a random signal has been stored--in continuous analog form on FM

tape, or in discrete, digitized form on IBM tape (Figure 3.1)--processing

the signal to determine its amplitude frequency distribution demands per-

formance of two distinguishable but serially connected operations. The

signal must be filtered in each of a number of narrow bandpass filters,

and the amplitude peaks must be discriminated and counted for each filter's

output. The techniques utilized for each of these two operations (Figures

3.2 and 3.3) reflect (a) differing roles assigned to the analog and

digital members of the hybrid team; (b) the inevitable limitations in avail-

able hardware at the particular installation; and (c) tradeoffs between

processing time and the precision required.

To get a fairly precise characterization of the amplitude frequency

distribution of a random signal, quite a few relatively narrow (about an

octave or less) frequency bands will be wanted. This need presses against the

limitations of cost and availability of hardware. Processing time is reduced

18

a Tmer

STeletype

Figure 3.1. Digitizing the Data

Analog Analog Digital:

DAC Bandpass Counting Recording andFilter Circuit Control

[Timer

Teletype

Figure 3.2. Determining the Amplitude Frequency Distributionof a Random Signal: Serial Method

19

IIBM DAC

Timer [Teletype *- -

T Scope I

Figure 3.3. Determining Joint Probability Density of a Random Signal: ParallelFiltering and Digital Peak Discrimination

Filtrs Cntro

dramatically if a random signal can be fed into a parallel set of filters

which yield simultaneously the filtered outputs for all filter bands.

An alternative plan is to use a single filter. The filtering is then

done serially by passing the data through the filter once for each frequency

band required, resetting the two cutoff frequencies of the filter by play-

back speed. This permits almost any number of narrow bandpass filters to

be used. The price, of course, is an increase in processing time. The

processing time will now be the product of the number of filters and the

record length plus a substantial overhead time (mainly tape handling) that

may very well exceed the actual filtering time.

When the output of a bandpass filter is available, the peak discrimination

can be done. For a narrow bandpass filter the output will be a quasi-sinusoidal

signal with fairly uniform frequency but varying amplitude. The function of

peak discrimination is to detect when a peak has occurred, to determine in

which of a spectrum of discrete amplitude levels the signal has peaked, and

to record this event by updating an appropriate counter. In both methods,

the outputs of the several filters are digitized and the peak discrimination

and counting are done by purely digital means.

The single filter method was implemented on the hybrid and the parallel

filter method was used on the Applied Research Laboratory computer facilities.

3.2 The Hybrid Program Method

The purpose of the first hybrid program is to take data in the analog

form from the tapes and convert it to digital form (Figure 3.1) usable by

the subsequent program. The data is converted to digital form using analog-

to-digital converters, one for each degree of freedom (up to six), and output

21

is stored as digital files, also one for each degree of freedom. The

sampling rate (numbers of times per second that the analog value is

converted to a digital number) is set by the user before each run. The

total number of samples taken is determined by the length of the test

run and is set by the user.

The files created by the digitizing program are then used by the AFD

program (Figure 3.4). The AFD program utilizes a single bandpass filter

with fixed frequency levels. The data is taken from the files created

by the digitizing program and converted by digital-to-analog converter to

analog form. This analog data is then bandpass filtered to discriminate

the frequency bands. To obtain the various frequency levels desired, the

data is converted to an analog signal at a rate different from the sampling

rate used in the digitizing program.

For example, to filter a frequency band whose upper and lower frequency

levels are twice those of the bandpass filter, the data is converted to analog

form at a rate one half the sampling rate. This is done for each frequency

bandwanted. The filtered data is then reconverted to digital form by analog-

to-digital converters. Peaks in the amplitude of the data are found by

comparing each digital sample with the sample preceding it and the one

following it, until a maximum in the amplitude is found (Figure 3.5). For

each cycle in the amplitude of the data, the peak value is found and stored

in an array. In addition, the time in seconds (since the beginning of the

test run) at which the peak occurred is also stored in the array. Insignificant

amplitude peaks, down in the noise level, are ignored. The data is then

printed out in a listing as described in Chapter 4. This listing gives

the amplitude of each peak in the data,. the time of the peak occurrence,

22

Start

Data: IF , Np, NF, NA,NS; F ,j=l to NF+I

Ai, i=l to NA; KS

I: Initialization Output: peaks,time, AP's1 j

II: InitializationIV: plitudefor j-th filter IV: Amplitudefor j-th filter discrimination

SFigure 3.6

III: Peak countingFigure 3.5

Output: AFD & APAFD1l Imatrix

j+1 -+ j

T Call scK S >0 display

j > N Froutine

F

Stop

Figure 3.4. Algorithm for Serial Method: General Outline

23

F

T fM <lfN"ff

MA Past largesSvalue of A

F

T t < L

Figure 3.5. Conversion of Each Filter's Output toCount Peaks and Store Each Peak's Value

Legend

Af - Present amplitude of f filter..signal

Mf - Past largest value of Af

If - Peak number of f filter

C if- Minimum amplitude to be discriminated

f - Index of filter band

Nf - Number of filter bands

t - Time

L - Processing time

24

the unadjusted absorbed power, and the absorbed power contributed by the

peak. One such listing is provided for each frequency band of each degree

of freedom. The peaks are now discriminated into the amplitude bands for

the AFD (Figure 3.6) and the value of each peak is compared with the upper

amplitude levels of the amplitude bands, starting with the lowest. Each

amplitude band is tested until the upper level of that band exceeds the

value of the peak. The number in the AFD array whose position is determined

by that amplitude band and the frequency band being processed is then

increased by one. In this way, the number of peaks having each particular

combination of amplitude and frequency can be determined. The unadjusted

Absorbed Power AFD (APAFD) is then calculated by multiplying the number of

peaks in the AFD for each amplitude-frequency combination by the square of

the center amplitude of that amplitude band, and multiplying this by the

proper K factor for that frequency band. The absorbed power AFD is calculated

by dividing each value in the unadjusted APAFD by the maximum number of

counts that could have occurred during the test run by a continuous sine wave

having a frequency equal to the center frequency of the band containing the

value. The AFD, unadjusted absorbed power AFD, and absorbed power AFD are

printed out for each degree of freedom.

3.3 Applied Research Laboratory Program

The digitizing work for the System 95 computer was obtained as a

service from the Applied Research Laboratory. The data was filtered into

eight frequency bands in parallel and recorded on digital tape. In order

to save time and tape, the data was digitized at a low rate of 32 samples/

sec. The digitized data was converted to Fortran compatible form by a

computer program (Figure 3.7), and rewritten in this form on more digital

25

f+1+f .Tf<

fk

i + i,k

Figure 3.6. Amplitude Discrimination for Each Peakand Counting AFD

Legend

N. - Amplitude level1

i - Amplitude level index

N - Number of amplitude levelsa

k - Peak number

thIf - Number of peaks in fth filter

f - Filter band index

N - Number of filter bands

th thCfk - Peak value, kt h peak in fth filter band

26

Start

I: Initialize and

define AFD size

Start FM tape

Convert ADC's. Count peaksfor each filter and storepeak value

Figure 3.5

Output: peaks,

time, AP's

III: Discriminate the amplitudelevel for each peak andupdate AFD

Figure 3.6

scope T Call sc

display ? display

Output: AFD &

APAiD. matrix

Stop

Figure 3.7. Algorithm for Parallel Method

27

tape. This program is listed in Appendix D. After digitizing and

conversion of the data, the AFD program was run. The data was input to

the AFD program from the digital tapes. As the data was already filtered

into the desired frequency bands as written on the tapes, no filtering was

required in the AFD program. Because the sampling rate of 32 samples/sec.

was too low to accurately define the peaks in the higher frequency bands,

Fast Fourier Transforms were used to provide more data between the data

points actually sampled. This gives an effective sampling rate of 256

samples/sec. This was done only for the three highest frequency bands where

the higher sampling rates are needed. The peak identification, data output

listing, AFD, unadjusted absorbed power AFD, and absorbed power AFD parts

of the program are all similar to those of the hybrid program.

28

4. RESULTS OF DATA PROCESSING

This chapter describes the results obtained by processing the NASA

bus ride data and aircraft data. The complete set of results can be found

in Appendixes E and F and typical samples are displayed here. The first and

second sections of this chapter are concerned with the bus data results. The

aircraft results are described in the third and fourth sections.

4.1 Objective--Bus Data Results

The first part of the output listing gives the amplitude and frequency

bands selected. This listing provides band limits and depending on the

scales chosen (linear or log), the center frequencies and amplitudes are

calculated and listed. This listing is not repeated until the next computer

run when a different set of bands can be chosen.

The next part of the computer output consists of eight listings, one

for each frequency band of each segment of bus data. The first column gives

the time in seconds, after the beginning of the segment, at which a peak in

the acceleration amplitude occurs. The second column gives the amplitude of

this peak, and the third column gives the unadjusted absorbed power which is

used as an intermediate step in calculating absorbed power. The fourth column

gives the absorbed power contributed by the amplitude peak. This is the

actual power absorbed by the passenger due to this acceleration peak. This

listing contains only those peaks with an acceleration amplitude of at least

0.02 g's, so that insignificant peaks with small absorbed power values are

igniored. The listing is provided so that the time and amplitude of those

peaks contributing large absorbed power values can be identified. Figures 4.1,

4.2, and 4.3 are typical listings from run 7, segment 3, vertical direction,

29

RUN=7DEGREE=1

SEGMENT= 3FREQ BAND=1

INEW= 2

TIMEO(SEC) AMP(G'S) AP NAP

2.28 0.10 0.000 0.0003

13.03 0.10 0.000 0.0003

Figure 4.1. Listing for Run 7, Segment 3, Vertical, Frequency Band 1

RUN=7DEGREE=1

o SEGMENT= 3

FREQ BAND=6INEW= 8


14.03 0.03 0.047 0.0011

28.84 0.04 0.109 0.0026

31.41 0.05 0.128 0.0030

35.78 0.04 0.083 0.0020

42.12 0.04 0.091 0.0021

45.00 0.06 0.228 0.0054

81.91 0.03 0.047 0.0011

96.03 0.03 0.047 0.0011

Figure 4.2. Listing for Run 7, Segment 3, Vertical, Frequency Band 6

RUN=7DEGREE=1

SEGMENT= 3FREQ BAND=8

INEW= 116


0.38 0.03 0.017 0.0001

1.03 0.05 0.039 0.0002

1.69 0.04 0.024 0.0001

2.31 0.05 0.053 0.0003

3.00 0.06 0.073 0.0004

5.28 0.05 0.039 0.0002

5.97 0.04 0.037 0.0002

6.59 0.03 0.021 0.0001

7.25 0.03 0.019 0.0001

8.44 0.03 0.014 0.0001

9.12 0.05 0.039 0.0002

16.09 0.03 0.014 0.0001

16.81 0.03 0.019 0.0001

17.53 0.03 0.015 0.0001

18.19 0.03 0.018 0.000121.00 0.03 0.019 0.0001

24.34 0.03 0.019 0.0001

25.66 0.06 0.061 0.0004

26.34 0.05 0.048 0.0003

27.06 0.08 0.134 0.0008

27.97 0.07 0.100 0.0006

28.78 0.07 0.081 0.0005

29.31 0.09 0.139 0.0008

30.06 0.15 0.443 0.0026

42.97 0.05 0.057 0.0003

45.12 0.04 0.037 0.0002

45.91 0.06 0.068 0.0004

48.66 0.04 0.030 0.0002

49.25 0.05 0.045 0.0003

49.81 0.03 0.016 0.0001

50.31 0.03 0.017 0.0001

50.94 0.06 0.075 0.0004

51.62 0.06 0.064 0.0004

52.25 0.04 0.030 0.0002

Figure 4.3. Partial Listing for Run 7, Segment 3, Vertical, Frequency Band 8

from front accelerometers. Note that each listing is first identified by

run number, segment number, and frequency band. Figure 4.1 is the listing

for frequency band 1. In most cases, the lower frequency bands contain few

peaks above the minimum, and these peaks have small absorbed power values

due to the small K factors in these bands. Figure 4.2 is the listing for

frequency band 6, and shows that the middle frequency bands generally

contain a moderate number of peaks with large absorbed power values. Figure

4.3 is a partial listing for frequency band 8. There are 116 peaks in the

complete listing. The absorbed power values are small due to small K

factors.

After the eight listings, the amplitude frequency distribution is

printed out; the amplitude frequency distribution shows the number of peaks

that occurred in the segment having any particular amplitude and frequency

combination. A separate amplitude frequency distribution is provided for

each degree of freedom of each segment. Figure 4.4 shows the AFD output

for run 7, segment 3, vertical. This is a typical AFD, showing the

approximate distribution found in most of the runs. Figure 4.5 is the AFD

for run 8, segment 2, lateral, from the center of the bus, and shows that a

few AFD's have counts in the upper amplitude bands, with resulting high

absorbed powers.

The unadjusted absorbed power AFD and absorbed power AFD are then printed

out. These give the unadjusted absorbed power and absorbed power contributed

by each amplitude-frequency combination. The unadjusted absorbed power AFD's

are not shown since they have no meaning; an absorbed power AFD is shown in

Figure 4.6 for run 7, segment 3, vertical.

Finally, the total unadjusted absorbed power and total absorbed power

of the segment are printed. Each of these is simply a single number found

32

Amplitude Levels Are Set At

0.03 0.05 0.08 0.13 0.21 0.32 0.50

Frequency Levels Are Set At

0.06 0.12 0.25 0.50 1.00 2.00 4.00 8.00 16.00

RUN=7DEGREE=1

SEGMENT- 3

AFD OUTPUT

0 0 0 0 0 0 0 00 0 0 0 0 0 0 00 1 0 0 0 0 0 12 0 0 0 0 0 1 70 0 1 1 6 1 5 280 1 0 2 4 4 10 49

Figure 4.4. AFD Output, Run 7, Segment 3, Vertical Motion

33


0.03 0.05 0.08 0.13 0.21 0.32 0.50


0.06 0.12 0.25 0.50 1.00 2.00 4.00 8.00 16.00

RUN=8DEGREE=5

SEGMENT= 2

AFD OUTPUT0 0 2 0 0 0 0 00 2 1 1 0 0 0 01 0 0 0 0 0 0 61 2 3 1 0 0 0 721 0 0 2 1 0 9 810 1 2 2 1 1 34 26

Figure 4.5. AFD Output, Run 8, Segment 2, Lateral Motion

34


0.03 0.05 0.08 0.13 0.21 0.32 0.50


0.06 0.12 0.25 0.50 1.00 2.00 4.00 8.00 16.00

NORMALIZED ABSORBED POWER AFD

0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000

0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000

0.000 0.002 0.000 0.000 0.000 0.000 0.000 0.003

0.001 0.000 0.000 0.000 0.000 0.000 0.010 0.009

0.000 0.000 0.001 0.001 0.017 0.007 0.021 0.014

0.000 0.000 0.000 0.001 0.005 0.011 0.017 0.010

SUMAP= 11.524 SUMNAP= 0.129

Figure 4.6. Absorbed Power AFD, Run 7, Segment 3, Vertical Motion

35

by summing the values in the unadjusted absorbed power AFD and absorbed

power AFD, respectively. Complete listing of the AFD's and the absorbed

power AFD's are given in Appendix E.

4.2 Subjective Data

The bus subjective data used in the correlation studies, taken by

experimenters of old Dominion University and supplied by NASA, are shown

in Appendix F (Tables 1-8). For runs 2 and 6, the subject assigned a

number from 1 to 5 to the quality of the ride, where 1 was the best quality

ride and 5 was the worst. Runs 7 and 8 were similar, except that the scale

ranged from 1 to 6. The subjective data for runs 1, 3, 4, 5 were unusable,

and therefore the objective data for these runs were not processed. The

objective and subjective data were tabulated for the correlation studies.

The first three columns contain total absorbed power of each segment for

the vertical, lateral, and longitudinal directions. The fourth column

contains the sum of the first three columns, which is the total absorbed

power to be correlated to the subjective data. The fifth column gives the

subjective response to the ride quality of each segment. Two tabulations

were made for each run, one for the front accelerometer and another for

the center accelerometer, except for run 8. The tabulation for run 7, front

accelerometer, is shown in Table 4.1.

In a given run, all the absorbed power values corresponding to a

single subjective response number were averaged, and then standard deviation

from this average was calculated. These average values are plotted as in

Figure 4.7, which is from run 7, front accelerometer.

It was noted that a few extremely large acceleration values, especially

in the lateral and longitudinal degrees of freedom, were causing large

36

Table 4.1. Listing of Absorbed Power (Three-Degree Motion)

with the Subjective Ratings (Front Seat) for

Bus Run 7 (AP in Watts).

Segment Vertical Lateral Fore-Aft Sum A -

1 0.022 0.071 0.001 0.094 3

2 0.025 0.002 0.000 0.027 2

3 0.129 0.502 0.004 0.635 4

4 0.005 0.069 0.000 0.074 2

5 0.143 1.060 0.084 i.287 5

6 0.002 0.012 0.016 0.030 2

7 1.165 9.392 8.761 (19.318) 1.165 4

8 0.027 0.071 0.001 0.099 2

9 0.148 (12.482) 0.005 (12.635) 0.153 6

10 0.162 0.189 0.003 0.354 3

11 0.006 0.030 0.000 0.036 4

12 0.019 0.070 0.001 0.090 1

13 0.128 0.349 0.188 0.665 2

14 0.812 3.041 2.534 (6.387) 0.812 3

15 0.043 (5.382) 0.002 (5.427) 0.045 2

16 0.028 0.374 0.001 0.403 2

17 0.184 8.526 0.003 (8.713) 0.187 6

37

16.0-

12.0-

8.0-

4.0-

0oo

030

ci I1 2 3 4 5 6

-4.0 Subjective Rating

Figure 4.7. Absorbed Power vs. Subjective Rating for Run 7,Segment 3, Front Seat of Bus Data

38

absorbed power values where the subjective rating was small. These

absorbed power values were discarded because such accelerations were

large enough to move the passengers from their seats and were unreasonable

since the subjective responses were small.

A second set of correlation plots was made after discarding these

high values, and the absorbed power scale on the plots was reduced

accordingly (Figure 4.8).

A final composite correlation plot, combining the data for all segments

of all runs from both accelerometers, was made. Although in the individual

plots the curve was not always exponential as expected, the composite plot

does show an exponential curve (Figure 4.9).

The composite plot appears as a straight line in a semi-log plot,

Figure 4.10, and fits the equation:

S = 1.7245 In (3.96849AP)

where S = the subjective response; and


4.3 Objective--Aircraft Data Results

The aircraft data consists of four test runs, with each run containing

from eight to fourteen segments. The segments vary in length, but average

about 30 seconds each. As the total time per run is from 16 to 28 minutes,

it can be seen that only about one-third of the information recorded on

the data tape is valid data. Since it cannot be assumed that the test segments

containing the valid data are evenly spaced, some type of timing method is

required to determine the beginning of each segment. Such a timing method

was included on a separate channel of the tape, the NASA time code.

39

2.0 -

1.5-

-e-U)

4J

- 1.0-

o

0.5

0

-0.5 -

Subjective Rating

Figure 4.8. Absorbed Power vs. Subjective Ratings for Run 7,Segment 3, Front Seat of Bus with Extreme ValueRemoved

40

5

4

2

S =1.7245 In (3.96849 AP)

1 /o r AP = 0.252e0 . s 7 9 9 s

0

I I I I I .

S 1.0 2.0 3.0 4.0 5.0

Absorbed Power, Watts

Figure 4.9. Correlation of Absorbed Power (For Three Degreesof Motion) with Subjective Bus Ride Data

41

10.0 -

5.0 -

M

1.0-

0 1 2 3 4 5 6

Subjective Rating

Figure 4.10. Composite Plot of Bus Data

42

Unfortunately, this time code was unusable by the investigators.

Nevertheless, it was decided that the aircraft data investigation would

be carried to completion to show that the technique can be used with data

having up to six degrees of freedom, even though valid results cannot be

expected.

It was assumed that the segments were 30 seconds long, evenly spaced

throughout the test run, and that the first segment began 15 seconds

after the beginning of the test run.

In view of the invalidity of the data and a shortage of available

computer time, only the first five segments of each run were processed.

In runs three and four, the data for the pitch, roll, and yaw were

recorded as velocity instead of acceleration, and were therefore unusable.

Only the three translational degrees of freedom were processed for these

runs. The results are tabulated in Table 4.2 and the correlation plot is

displayed in Figure 4.11.

43

Table 4.2. Listing of Absorbed Power (Six Degrees of Motion)with the Subjective Ratings for the Three TestRuns of Aircraft Data

SEGMENT AP, WATTS SUBJECTIVE RATINGS(2 persons)

TEST 1

1 9.4052 2 22 0.0077 3 33 1.3014 3 24 0.0678 3 35 0.2828 3 3

TEST 2

1 9.5426 3 32 0.0513 4 43 0.0099 5 54 0.0039 4 45 0.0091 4 4

TEST 3

1 0.0196 2 32 0.0201 3 43 0.0039 3 44 0.0103 3 45 0.0674 3 4

TEST 4

1 0.004 1 -2 0.000 1 -3 0.000 2 -4 0.000 2 -5 0.000 2 -

44

.7

.6 -

.5 -

.4

p-45

.3 -.3

0

.2

G

1 2 3 4 5

Subjective Rating

Figure 4.11. Absorbed Power (For Six Degrees of Motion)

vs. Subjective Aircraft Ride Data

45

5. APPRAISAL OF RESULTS, APPLICATIONS, AND RECOMMENDATIONS

5.1 Appraisal of Results and Applications

The correlation results of absorbed power as an objective ride measure

to the subjective evaluation for the NASA bus data was very successful.

Individual segments and rides gave poor correlation since the data base

was too small to give a reasonable random sample. However, when sufficient

numbers of rides are used to give a reasonable sample base, excellent cor-

relation was obtained and the following logarithmical relation was shown by

the data:

S = 1.7245 In (3.96849 AP)

where S = the subjective rating (on a 5-point scale); and


The six-degree-of-freedom computational method for the aircraft data

was completed. A few samples were reduced, but they provided insufficient

data (i.e. too small a sample size). In addition, there was no assurance

that the acceleration data were properly matched with subjective ratings

since exact start-stop times of the segments were not known. For these reasons,

the aircraft data are not considered to be very exact and thus little can be

drawn from the correlation plots.

Since there was a successful correlation of the bus data, a further

correlation of ISO standards and the Absorbed Power (AP) method was started.

Appendix H gives the details of the results of this comparison. It was

found that these two methods do agree rather well. In the whole-body

frequency range, AP is slightly more conservative; in the 10 to 100 Hz,

the two agree; but in the 2 Hz and below range, the AP is not as restrictive

46

as ISO standards. Since AP only accounts for vibration effects and such

things as motion sickness are not included, there is justification for the

harsher requirements of ISO standards in this range.

Since the two methods compare reasonably well, one can use either

method as an overall criterion. However, the AP method has the distinct

advantage that effects due to more than one degree of freedom can be

determined by adding the effect of the individual degrees of freedom. It

thus appears, if the proposed ISO standards are to be -used, a combination of

ISO standards and the AP method would be in order.

Once the bus subjective and ISO standard correlations with AP have

been made, it is useful to compare these two correlations. Table 5.1

shows the AP values for both correlations with the ISO standards for one-

hour exposure.

With the exception of the very good ride, the two correlations give

absorbed power levels that are very similar. Even the very good ride

(subjective rating of 1) is close in terms of overall rating--a .45 AP to

4.57 AP range for the bus data and .15 AP to 5.88 AP range for the ISO

standards.

5.2 Recommendations

Since the bus data and ISO standards were successfully correlated, more

work should be done with the aircraft data. The computer programs are now

operational and the costs of completing the study of aircraft data would

be mainly for computational time.

It is also recommended that a new set of K values for the AP method

be developed from the ISO standards and that both these values and the

47

Table 5.1. Comparison of the Bus Ride Correlation with theISO Standard Correlation Using Absorbed Poweras the Basis for Comparison

Average AP for a AP Level fromSubjective 1-Hr. ISO Standard Bus Ride

Ratings Exposure Correlation

1 .15 .45

2 - .8

3 1.5 1.44

4 - 2.56

5 5.88 4.57

48

original absorbed power K values be tried in the computer programs. Since

the programs accept K values as data, it will be a simple task to compute

AP values based on both sets of values.

In summary, the authors feel that the absorbed power approach has

merits and would like to propose to use the results of this study to run

complete correlations of the University of Virginia aircraft data and any

other NASA ride data that might be available.

49

REFERENCES

1. Reiher, H. and Meister, F. J. "Die Empfindlichkeit des Menschen gegenErschulterungen." Forschung auf dem Ingenieurswesens 22 (1931),pp. 381-386.

2. Jacklin, M. H. and Liddel, G. J. "Riding Comfort Analysis." EngineeringBulletin, Research Series No. 44, Purdue University, Lafayette, Ind.,May 1933.

3. Janeway, R. N. "Ride and Vibration Data." Special Publication SP-6,Society of Automotive Engineers, 1950.

4. Ten Cate, W., translated by Murray, R. D. "Vibration Nuisance."

Royal Aircraft Establishment, Great Britain, Oct. 1957.

5. Snyder, F. W. "Effects of Low Frequency Vertical Vibration on HumanPerformance." Paper read at Aerospace Medical Association, Apr. 1962.

6. Van Deusen, B. D. "Analytical Techniques for Designing Riding Quality."S.A.E. Publication No. 670021, 1967.

7. Holland, Clarence L. "Some Aspects of Human Response to Random Vibration."Technical Report No. 9010 (11 105), Army Tank-Automotive Center, Aug. 1965.

8. Butkunas, Andrius A. "Power Spectral Density and Ride Evaluation." FordMotor Company, S.A.E. Publication No. 660138, 1966.

9. Pradko, Fred and Lee, R. A. "Vibration Comfort Criteria." S.A.E. Publi-cation No. 660139, Jan. 1966.

10. Pradko, Fred and Lee, R. A. "Analytical Analysis of Human Vibration."S.A.E. Publication No. 680091, 1968.

11. Pradko, Fred, Lee, R. A., and Kauluz, V. "Theory of Human VibrationResponse." A.S.M.F. Publication No. 66-WA/BHF-15, 1966.

12. Beurteilung der Einwirkung mechanischer Schwingungen auf den Menschen."(Assessing the Effect of Mechanical Vibrations on the Human Body.)VDI-Richtl. 2057,2. Entwurf, Dec. 1961.

13. Allen, G. R. Private Communication. (R.A.E. Farnborough, England.)

14. Simic, D. "Influenza delle vibrazioni angolari sul corpo umano"(Effect of Pitching Vibration on the Human Body). A.T.A., Vol. 24, No. 7(1971), p. 361.

15. Symposium on Vehicle Ride Quality. NASA TMX-2620, Oct. 1972.

50

16. Vinje, E. W. "Analytical and Experimental Evaluation of Proposed Ride

Comfort Criteria." Symposium on Vehicle Ride Quality, NASA TMX-2620,Oct. 1972, pp. 115-141.

17. Shanahan, B., Stearman, R., Heobez, A. "Literature Survey on Passenger

and Seat Modeling for the Evaluation of Ride Quality." Research Memo

to DOT (DOT OS 30093RM8), Nov. 1973.

18. Brickman, A. D., Park, W. H., and Wambold, J. C. Road Roughness Effects

On Vehicle Performance. Penna. Dept. of Transportation Research ProjectNo. 69-15. TTSC Report 7207, Pennsylvania Transportation and Traffic

Safety Center, The Pennsylvania State University, 1972.

19. Wambold, J. C., Park, W. H., and Vashlishan, R. G. "A New Random Data

Description and Its Use in Transferring Road Roughness to Vehicle

Response." ASME paper 73-DET-26, September 1973; Journal of Engineeringfor Industry, Vol. 96, Series B, No. 2 (May 1974), pp. 676-681.

20. Park, W. H., Wambold, J. C., and Vashlishan, R. G. "Prediction of

Objective Passenger Comfort from Road Profile." ASME paper 73-DET-114,September 1973; Journal of Engineering for Industry, Vol. 96, Series B,

No. 2 (May 1974), pp. 503-508.

21. Brickman, A. D., Wambold, J. C., and Zimmerman, J. D. "An Amplitude-

Frequency Description of Road Roughness." Highway Research RecordNo. 166 (1971).

22. Wambold, J. C. and Zimmerman, J. R. "Hybrid Programs for Calculating

the Joint Probability of Amplitude and Frequency of a Random Signal."ACES Transactions, Vol. 3, No. 7 (July 1971), pp. 133-144.

23. Wambold, J. C. and Park, W. H. "A Data Processing Method Giving a

Better Physical Description of Random Signals." Presented at the20th International Instrumentation Symposium, May 1973, Albuquerque,New Mexico; Proceedings of the 20th International InstrumentationSymposium (1974), pp. 371-375.

24. Wambold, J. C. and Park, W. H. Objective Ride Quality Evaluation.PTI 7412, The Pennsylvania Transportation Institute, The Pennsylvania

State University, March 1974.

51

APPENDIX A

Human Response to Random Vibration

"Iafr ?AGE S pOOR

Transfer Function for Seated Vehicle Passenger

In 1965, Pradko and Lee(9, 10, ll)utilized a transfer function

approach for the analysis of human vibration. The technique. developed

accurately identifies, measures, and predicts whole body response to any

vibrational input, whether sinusoidal, transient, or random.

Figure A.1 illustrates the force and motion quantities of particular

interest in human response dynamics.

Aou

S A.In in

Figure A.l. Response Measurements

There is one transfer function for each combination of output and

input. For example, the transfer function relating the acceleration input

A. to the output acceleration A of the system in Figure A.1 is givenin out

in the equation:

A (f)G (f) = out(f) (A.1)aa A. (f)

in

There also exists a transfer function relating the force of vibration

F. to the output acceleration Ain out

G (f) =F. (f)fa in . (A.2)Aou (f)Aout

Pradko and Lee determined and multiplied the above two transfer functions

together, producing the following transfer function:

F. (f) A (f)In out G (f) (A.3)A out(f) A.in (f) mout in

or

G (f) = Fin(f) (A.4)m in .(A. 4)

A. (f)in

The above transfer function has been termed Effective Mass.

Perhaps a word should be said about the experimental program and

instrumentation used in developing the above transfer function. A known

sinusoidal input acceleration of specified magnitude and frequency was

applied to the seated subject. The steady state output force magnitude

and phase were then recorded. The frequency of the input was then changed

to another value, and again the output was recorded. The entire fre-

quency range considered important was generated. This ratio of output to

input was plotted with the frequency as the abscissa. From this relation-

ship, the transfer function was determined.

Absorbed Power

Although transfer functions allow analytical solutions for the dyna-

mic response of the human body, they do not provide any apparent way for

determining the severity of the vibration. A parameter that will relate

A-2

the vibrational intensity to the subjective response is required.

Extensive testing by Pradko and Lee has shown that the rate of

flow of energy becomes a parameter that characterizes the interaction of

the vibrating human and the environment. The energy flow takes place as

a result of the complex damped elastic properties of the human anatomy.

When vibrational energy distorts the elastic body, dimensional changes

take place, producing reactions that tend to restore the body to the orig-

inal position. The work performed in the process balances the applied

load. Consequently, the body's elasticity produces restoring forces

which are related to displacement. The body's vibratory motion contin-

ues until the energy imparted is dissipated or removed. The time rate at

which this energy is used has been defined by Pradko as absorbed power (AP).

Absorbed power is a parameter relating vibratory input conditions to sub-

jective response and is defined as follows:

Average AP = lim 1 fT F(t) V(t) dt (A.5)T- - T o

where F(t) = Input force; and

V(t) = Input velocity.

In order to evaluate the absorbed power concept in terms of the

passenger's subjective response, Pradko and Lee gathered data from 13

test subjects at the Dynamic Ride Simulator facility at the Army Tank

Automotive Command (ATAC). For each particular test, the frequency was

present and remained fixed. The sinusoidal acceleration amplitude was

increased at a slow rate from zero to a condition of vibration tolerance.

The tolerance condition was a combination of vibration severity and sub-

ject response where pain, loss of physical control, or advanced stages of

A-3

blurred vision were considered by the subject to be unacceptable in the

sense that vehicle control could not be maintained. When tolerance was

reached, the subject actuated a buzzer which began the data .collection

procedure. Results shown in Figure A.2 represent a two-sided interval

which brackets the mean acceleration with 90 percent confidence level

(solid curves). From these tests, mean values of acceleration at corres-

ponding frequencies were used to develop a constant power curve of 290 watts.

This curve was then fitted to the sinusoidal as well as a random vibration

curve. The results indicated that absorbed power displayed the same char-

acteristics as the subjective judgment criterion.

5 I0 I5 2 25 30

co

-J0

FREQUENCY (cps)

Figure A.2. Acceleration: Power Comparison

Since absorbed power is a function of the energy flow rate of the

elastic properties of the human anatomy, it has physical significance and

interpretation. Consequently, it is possible to measure the variation of

A-4

this parameter for different .people and different seating arrangements.

For example, it has been found that a muscular person generally has, for

the same body weight, a lower absorbed power for the same vibration than

a more obese person. The effect of the elastic property of the anatomy

can be shown by using a rigid mass in place of a human test subject. The

resulting energy flow is zero because of its rigid, inelastic properties.

Pradko and Lee have also shown that a contoured seat generally pro-

duces a lower absorbed power than one that is not contoured. This is due

to the larger contact area and resulting reduction in body movement. Un-

der very severe conditions where the man moves relative to the seat, the

assumption of linear equations is no longer valid; consequently, the trans-

fer function and absorbed power results lose their validity as the system

becomes more nonlinear. Pradko has examined this aspect of linearity and

verified that the mechanical response characteristics of man in a seated,

erect position is linear.

Under normal vibration conditions, using absorbed power as a criter-

ion, one can modify the input or seating arrangement and measure directly

the effects on comfort. To examine this sensitivity of absorbed power,

a test was performed using ride forms (composed of 26 random waveforms)

as the experimental inputs. Each ride contained different PSD variation

characteristics in the frequency spectrum of 4 to 36 cps at different

levels of acceleration. The rides were presented in sequence of increas-

ing acceleration magnitude. A group of 10 subjects judged each ride sub-

jectively for comfort and reported only those rides that appeared to be

"out of place." The test subjects reported nine rides out of place. The

absorbed power data which were experimentally measured were compared to

A-5

the acceleration levels of the rides. It was found that absorbed power

closely agreed with the subjective response, indicating that the accelera-

tion sequence was incorrect. The versatility of absorbed power in deter-

mining human discomfort due to vibration is not realized in any other known

methods.

In the time domain, absorbed power can be written for an infinite time

or a finite averaging time. Equation A.5 shows the average absorbed power

function for an infinite averaging time.

Absorbed .power can also be described in the frequency domain. The

2power is computed as the product of the mean squared acceleration (A 2rms)

at each frequency and the parameter (K.), where Ki is a function of fre-

quency, but not amplitude (index i denoting the descrete frequency):

n 2Average AP K. x A. rms (A.6)

1 11=0

Absorbed power is a scalar quantity and, therefore, can be directly ad-

ditive. For multi-degree motion, the individual absorbed power values

are readily summed for a single quantitative measure of human vibrational

comfort. Pradko and Lee have published the K. values for five degrees1

of freedom (verticalfore-aft, lateral, pitch, and roll) as well as for

input to the feet. Typical K. parameters are shown in Table A.l. These1

K values are used to weight the effect of each directional input, and

the total absorbed power is the algebraic sum of the absorbed power at-

tributed to each input. Since.absorbed power is a scaler, phasing informa-

tion between the inputs is not needed for evaluation.

As Equation A.5 indicates, the input force and velocity are needed to

compute absorbed power. However, utilizing Equation A.6, the absorbed power

A-6

Table A.1. Typical Absorbed Power Parameters for Vertical Motion

K.Frequency I(f) Phase Angle

(Hz) watts (slugs) (Radians)(ft/sec)

0.00 0.000000 4.3537 0.000000

0.10 0.000082 4.3557 0.000009

0.30 0.000747 4.3716 0.000237

0.50 0.002113 4.4035 0.001111

1.00 0.009149 4.5553 0.009307

1.50 0.022941 4.8118 0.033143

2.00 0.045576 5.1612 0.081930

5.00 0.198689 5.7092 0.93785

7.50 0.075581 2.7408 1.2811

10.00 0.048340 2.4408 1.1623

20.00 0.010555 1.0568 1.1826

40.00 0.003780 0.73906 1.2470

70.00 0.001390 0.45976 1.3741

100.00 0.000702 0.32860 1.4313

A-7

calculation can be made directly from acceleration data. Hence, it is

possible to determine the absorbed power and, therefore, comfort values

by merely measuring the acceleration input to the passenger for each

direction.

Information in the literature on the effect of long-time vibration is

scarce. However, Pradko and Lee have deduced that a term can be added to

absorbed power that might account for long-term effects. Their empirical

equation becomes:

tAPT ave + A P dt (A.7)

toe Jo avet o

O

where APT = long-term absorbed power;

t = time scale factor approximate onset of fatigue; and0

t = exposure time.

In the frequency domain, it can be shown that the ratio of short-term to

long-term absorbed power can be written as:

APave = 1 Pave 1(A.8)AP 1t/ )AT 1 + (t/t )

which can be used to calculate the degradation of comfort with time.

Figure A.3 is a diagram of how absorbed power can be determined from

the output of an accelerometer mounted at the base of a seated passenger,

utilizing the transfer function to generate the force.

A-8

Accelero- ceeration fTransfer Force Multi-

meter Function

Acceleratior Inte- Velocitygrator

lveraging Average- Absorbed PowerCircuit

Figure A.3. Block Diagram Showing Absorbed Power Determination.

A-9

APPENDIX B

The Amplitude Frequency Distribution (AFD) Method

REPRODUCIBLITY OF THEORIGINAL PAGE IS POOR

Measured records must be recognized as random signals of finite

duration and, as such, they can be viewed and described in terms of

three basic "domains": time, amplitude, and frequency. The time do-

main description is the unprocessed signal-versus-time. All types of

amplitude domain descriptions reduce the measured signal to a single

number or table of values which is mathematically equivalent to com-

puting an amplitude probability distribution for the signal. Frequency

domain representations of signals are generally considered to be the

most useful. They are based on the concept that any observed random signal

can be reconstructed by adding together a number of different sine waves.

At first glance, it would appear that the power spectral density con-

tains a complete description of amplitude variations, thus making any ampli-

tude-distribution calculations superfluous. However, the ordinate of a

PSD curve indicates only the average signal amplitude at a particular fre-

quency. A large PSD value can conceivably be produced either by a few

cycles of large amplitude or a large number with small amplitudes; the

distinction cannot be made from the PSD curve alone. On the other hand,

it is not possible to extract any information about frequency distribution

from amplitude density curves. It is evident from these considerations

that the PSD and amplitude density curves each contain unique information,

and a simple method of combining the two representations is desirable.

An effective method for combining the information contained in both the

PSD and the amplitude representations is to reduce the random time-history

signal to a simple tabular array that displays both the height and the

length features on the random data, as in Figure B.1. Here the coordinates

(linear or logarithmic), amplitude (in feet, g's, etc.) versus frequency

06

C

E

4<

) 1"_Number of Counts

.-

E

-- Freq. Bond

Frequency, I/X ,cpf

Figure B.1. Basic Elements of AFD, the Amplitude Frequency Distribution

B-2

(in Hertz, rpm, cycles per foot, etc.), are divided into a number of

finite bands as shown. Numbers like N are computed and entered at

each window-like intersection of the bands. The numbers express the

total number of signal peaks with the amplitude and frequency of that

box in the array. The complete array of numbers thus identifies the

random signal as a combined amplitude and frequency distribution (AFD).

Thus, the AFD not only gives the frequency distribution, but also shows

the amplitude make-up and distribution of each frequency hand. Further

details of this method and means of computation are given in references

18 through 24.

Research by the authors has shown that the AFD format is useful

when calculating absorbed power. By calculating the absorbed power for

given amplitude and frequency bands it is easily seen what areas contri-

bute to an uncomfortable ride, and make possible design changes to better

the ride. Details of the AFD formatted absorbed power concept are found

in references 19, 20, and 24.

B-3

APPENDIX C

The Hybrid Computer Program

-PAGE 1Sp9R

C ************************A FDGD.F4*************************C THIS IS AN AFD PROGRAM FOR UP TO SIX DEGREES OF FREEDOMC USING AN OCTAVE FILTER WITH THE SERIAL METHOD.C DATA MUST FIRST BE DIGITIZED USING A PROGRAM LIKE DIGTZ.F4C AND THEN STORED ON IBM TAPE.CC************** ************************************************

INTEGER AFD(10,10)EXTERNAL ILTDADIMENSION NADC(5000),TIMEO(5000),A(II),I LA(1) ,AM(11),FM(I1),FL(1I),DELT(II),DATAO(1I0000)LOGICAL STAT

C: *************************************************************C THIS IS THE SET UP SECTION ALLOWING THE OPERATOR TO SPECIFYC THE FOLLOWING:C I.DEGREES OF FREEDOM WANTEDC 2.IF YOU WANT TIME AND ORDER OF EACH PEAK LISTEDC 3.NUMBER OF AMPLITUDE BANDS WANTED AND THE LEVELSC THEY ARE TO B3E SET AT.C 4.NUMDER OF FREQUENCIES BANDS WANTED AND THEC LEVELS THEY ARE TO BE SET AT.C 5.THE DIGITIZING FREQUENCY USED ON THE DATA AND THEC NUM3ER OF SAMPLES.C G.THE DESCRIPTIVE HEADING TO BE PRINTED OUT.C THE COMPUTER THEN RESPONDS AND TYPES OUT WHERE THEC AMPLITUDE LEVELS ARE SET,WHERE THE FREQENCY CUT OFF'S AREC SET,AND WHAT THE CENTER AMPLITUDES AND FREQENCIES ARE.C******************************************************

TYPE 22 FORMAT('0 THIS IS A PROGRAM TO CALCULATE AFDS FOR UP

I TO SIX DEGREES OF FREEDQM USING A SINGLE OCTAVEI FILTER',$)TYPE 3

3 FORMAT('0 TYPE DEGREES OF FREEDOM WANTED, 1 TO 6,:',$)ACCEPT 4,NDEG

4 FORMAT(I I)TYPE 5

5 FORMAT('0 IF YOU WANT ORDER AND TIME OF COUNTS,I TYPE 1, IF NOT TYPE 2,:',$)ACCEPT 4,ICONTTYPE 9

9 FORMAT('0 TYPE NUMBER OF AMPLITUDE BANDS WANTED, UP TO1 10',//,' IF YOU WANT NORMAL AMPLITUDE LEVELS, TYPE 1,I IF NOT TYPE 2,=',$)ACCEPT 6,NAMPLEVEL

6 FORMAT(21)MAMP :NAMP+IIF (LEVEL.LT.2) G TO 22TYPE 10,MAMP

10 FORMAT('O0TYPE',115,'AMPLITUDE LEVELS WANTEDo01 TO .995,:',$)ACCEPT ll,(A(K).,K=l,MAMP)

11 FORMAT(20F)DO 20 K=I,NAMP

20 LA(K)=A(K)*10000GO0 TO 231 REPRODUCIBILITY OF THE

01IGINAL PAGE ISOOR

C HERE THE STANDARD AMPLITUDES ARE CALCULATED

22 EXT:ALOG( 7 0 0 .0)POWER:=(ALOG(1 0000.0)-EXT)/NAMPDO 23 K=I,MAMPB=KDUM =EXP (POWER* (B - . 0)+EXT)LACK)=DUM

23 AM(K) =EXP(POWER* (B-0.5)+EXT)/10000.0236 TYPE 3636 FORMAT('C0 TYPE NUMBER OF FREQUENCY BANDS WANTED, UP

I T10 10',//'TYPE LOWEST FREQUENCY WANTED IN HZ,IN REAL'/',=',$)ACCEPT 8,NFREQ,FMINMFREQ=NFREQ+I

8 FORMAT( lI ,IF)TYPE 37

37 FORMAT(' TYPE LOWER FREQUENCY OF YOUR FILTER HZ,IN REAL'/',=',$)ACCEPT II,FILDO 38 I=1,MFREQY=I-1

38 FL(I) =FMIN*2.0**YTYPE 39

39 FORMAT('0 TYPE IN DIGITIZING RATE (NORMALLY 1000) INI SAMPLES PER SEC',/'NUMBER OF SAMPLES DIGITIZED'/',=',$)ACCEPT 4,NDIG,NSAMPDO 40 NF=I,NFREQDIG:NDIGDEN=FL( NF)RATE=DIG*FIL/DEN

40 DELT(NF)=(1.0/RATE)*1000000*******************************************************

C DELT IS IN MICROSECONDS

DO 15 K=I,MAMPDA:LA(K)

15 A(K) =DA/10000.0

C HERE THE STANDARD FREQENCIES ARE CALCULATEDC***#**** ************ ****** **** ***** *** ** **** ** **** **** ** *** ***

DO 16 K=1,NFREQB=KEXT=ALOG (FMI N)FREQ=NFREQPOWER = (ALOG (FL(MFREQ) ) -EXT)/NFREQ

16 FM(K) =EXP(POWER*(B-.5)+EXT)30 TYPE 3131 FORMAT('C0 TYPE DESCRIPTIVE HEADING FOR CURRENT RUN'/)

ACCEPT 35,HEAD35 FORMAT(14A5)

TYPE 41,(A(K),K=1,MAMP)41 FORMAT('0 AMPLITUDE LEVELS ARE SET AT',//,11F6.2)

TYPE 42 (FL(K),K=1,MFREQ)42 FORMAT( 0 FREQUENCY LEVELS ARE SET AT',//,11FS.2)

IF (LEVEL.GT.1) GO TO 44TYPE 43 (AM(K),K:1,NAMP)

43 FORMAT( 0 CENTER AMPLITUDES ARE',//,10F7.3)44 TYPE 45,(FM(K),K=1,NFREQ)45 FORMAT('0 CENTER FREQUENCIES ARE',//,10IF7.3)

C-2

C HERE THE HYBID IS INITIALIZED

CALL HINITCALL SAMO('SP')CALL STCO('NSEC')CALL SLMO('CLEAR')

C START PROCESSING THE DATA , ONE DEGREE (NDEG) AT A TIMEC OPEN THE APPROPIATE FILE FOR THE NDEG TO BE PROCESSED.

62 DO 999 ID=1,NDEGGO TO (7 1,72,73 9 74,75,76),NDEG

76 CALL IFILE(1,'DATAG')GO TO 777

75 CALL IFILE(I,'DATA5')0 TO 777

74 CALL IFILE(I,'DATA4')GO TO 777

73 CALL IFILE(1,'DATA3')GO 0TO 777

72 CALL IFILE(1,'DATA2)GO 0TO 777

71 CALL IFILE(I,°DATAI-)777 CONTINUE

DO 63 KK=1 910DO 633 JJ:=1,10

63. AFD(JJ ,KK) :0

C NEED TO ZERO FOR EACH DEGREE OF FREEDOM

DO 99 IF:=1,NFREQIADC=OISW=:0INEW:=0IMAX=1 0NSIZE=1 0000IF(NSIZE.GT.NSAMP) NSIZE:NSAMPITEST:NSIZE-NSAMPREAD(1) (DATAO(I) ,I=: 1,NSAMP)CALL STINTCALL SAMOC('IC')CALL SRLT('LINK',0o0)

is5" CALL DTM(DELTERRORILTDADACO,NSIZE,DATAO)CALL INTCNT(NSAMP)

C NEED TO CALL DATA IN FROM DISK HEREC* ****************************** *******************,:r*********66 CALL SLMO('RUN')

CALL SSCL(0)CALL SAMO('OP')

110 CALL CRAC (0,IADC)

C-3

C TEST IF DATA IS LARGER THEN LAST MAX VALUEIF NOTC CHECK NEXT VALUE, IF IT IS CHANGE IMAX TO THE NEWC VALUE AND o ON TO THE NEXT DATA POINT.

IF (IADC.LE.IMAX) rO TO 120ISW=1

77 IMAX:IADCCALL RRLT(TMIN ,SEC)GO TD 110

120 CALL DTMSTA(.FALSE.,STAT,IFREE,IDONE)IF(STAT) GO TO 88

C TEST IF INTERRUPTS ARE THRU AND GO SEE IF ANY MORE DATAC IN THIS SAMPLEC***************************************************************

IF (ISW.LT.1).00 TO 110IF(IADC.GE.0)GO TO 110

C***************************************************************

C COUNT THE PEAK NOW IN INEW, STORE PEAK VALUE IN NADCC ,AND RECORD PEAK TIME IN TIMEO.C***************************************************************

I NEW=I NEW+1NADC(INEW)=:IMAXTIMER=(TMIN*60.0)+(SEC/1000000.0)TIMEO (INEW) =TIMERIMAX=10ISW:=0GO TO 120

88 CALL SAMO('HOLD')CALL SLMO('STOP')NEW=NSIZE+IIF(TEST.EQ.0) GO 0TO 90NSIZE=NSIZE+10000ITEST:NSIZE-NSAMPLIF(ITEST.LT.0)GO To 89NSIZE:NSAMP

89 READ(1)(DATAO (I),I=NEW,NSIZE)GO TO 65

90 END FILE(1)IF(ICONT.GT.1) GO T 95DO 1010 JJ=I1,INEWTYPE 91,NDEGTYPE 92

C TYPE OUT HEADINS IF PEAKS AND TIMES ARE WANTED

92 FORMAT('0 NUMBER',5X,'AMPLITUDE',5X,'TIME')TYPE 93,JJ,NADC(JJ),TIMEO(JJ)

93 FORMAT(0' ,2X,I 4,9X,I5,5X,FG.2)91 FORMAT('I',3X,'COUNTS FOR THE',I,'DEGREE')95 IF (INEW.LT.1) GO T10 99CC COUNT LEVELS FOR AFD NOW,IF A FREQUENCY BAND HAS NOC COUNTS,SKIP TO NEXTC ************* ********* ***

C-4

DO 1010 N=,INEWIFC(NADC(N).LT.LA(1)) (n TO 1010DO 1000 J:2,NAMPIF(NADC(N).G*E.LA(J)) GO TO 1 00JJ :NAMP-J+2GO TO 1005

1000 CONTINUEJJ=:

1005 AFD(JJ,IF) :AFD(JJ,IF)+11010 CONTINUEC

C AFD COUNT NOW COMPLETE FOR CURRENT DEGREE OF FREEDOMC

99 CONTINUETYPE 54,NDEG

54 FORMAT('1 AFD OUTPUT OF THE',I2,'DEGREE OF FREEDOM FOR--'/)TYPE 56,HEAD

CC TYPE OUT AFD HEADINGCC****** **********************************************

56 FORMAT( "' ',14A5)DO 550 K:=1I,NAMP

550 TYPE 400o(AFD(K,I),I:1,NFIL)

C TYPE OUT AFD

400 FORMAT('O' ,1017)999 CONTINUE

STOPEND

C-5

APPENDIX D

Applied Research Laboratory Computer Program

REPRODUCIBMILITY OF THEORIGINAL PAGE IS POOR

C $$$ARL-AFD.F4$$$C THIS IS AN AFD PROGRAM FOR SIX DEGREES OF FREEDOM------C USING 8 OCTAVE FILTERS WITH THE PARALLEL METHODC D)ATA MUST FIRST BE DIGITIZED AND STORED) ON TAPE.--C$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$

COMPLEX ST(256),WtN(32) ,W2N(256),SAVE1DIMENSION X(3840)INTEGER AFD(6,8) .. ----. ----- -----.INTEGER'2 ID,1IFX(480,8)DIMENSION AP(250),LA(7),FM(9),FL(9),AM(10)DIMENSION A(7),NPEAK(250),TIMEO(250)DIMENSION ISEG(19),PEAK(250)DIMENSION APM(6,8),APAFD(6,8),C(8).REAL NAPAFD(6,8),KF(6,8),NAPM(6,8) vNAP(250)ISEC=600P I . = 3 .1 4 1 5 9 2 6 5 3 5 9 - ... .. . ... .... .. ... . . . . . . . . . .N1 = 32N2 = 256 . - - - -.-- -- --- *.. ...- -L2N1 = 5L2N2 = 8-----------...... ......

CALL FFT(ST,W2N,N2,L2N2,0)DO 1020 I = 1,256 ---- ---

WA = REAL(W2N(I))WB = AIMAG(W2N(I)) ------- - - -... ...---- .....--- -- -....... .

1020 W2N(I) = CMPLX(WA,-WB)CALL FF1T ( ST,WIN,N1 ,L2N1,0) ............. .

BB = 0.0C$$$$$$$$$$$$$$$$$$$$$ $$$$$$$$$$$$$$$$$$$$$$$$$$$-$$$-$$$-$$ $$$$C THIS IS THE SET UP SECTION ALLOWING THE USER .TOC SPECIFY THE FOLLOWING (IN DATA CARDS: - ----- -- .C 1. ID NUMBERS, RUN NUMBER, AND DEGREE NUMBERC --- ------ -THAT ARE DESIRED -FOR-THIS RUN-. ......-- . ..--------.. .C 2. ABSORBED POWER K FACTORS WANTEDC$$$$$$$$$$$$ $$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$ $$$$$$$-$$$$$ - .C READ ID NUMBERS, RUN NUMBER, AND DEGREE NUMBER FROM DATA CARDC$$$5$5$$$$$$$$5555$$$$$$$$$$$$$55$$$$$$$$$$$$$$$$$$$$$.-$$$$$$$$$$

READ (5,220)(ISEG(I ),I=1,7)220 FORMAT (19 12 ) . . . . . ... ... .......

KFLE=ISEG(7)C$$55$$$$$$$$5$$$$$$$5$$$$$$$$$$$ 55$$$$4$$$&$$$$$$$$$$$$$$$$$$$$$-$$$......

C READ K FACTORS FROM DATA CARDC$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$-$$$$$$$$$

DU 350 KDEG=1,6IF- (KDEG.EO.2) GO TO 320 ---..........

201 READ(5,301 ) (KF(KDEG, 1), 1=1,8)301- FORMAT(8F6.6)-- - -------- -__ __-_

GO TO0 311320- . READ(-5,302-) (KF (KDEG-,-I-) ,-I-=1-,8-----302 FORMAT(8F6.5)311 -- CUNTINUE -- - - -..... . -. .. .350 CONTINUE Tp.... .DO 800 1--KDOEG= 1,6--- ---------- -.

IF(KDEG.GE.4) CAL=1140.0 X0S RIF(KDEG.LT.4) CAL=200.0 . .. . - . .. .IF(KDEG.EQ.1) CAL=285.0

.TUX =5000.0 ---

IF(KDEG.GE.4) TUX=20000.0C$$ $$$$$ C$$$T L$$$$$$ $$ $$$$$$$$$$$$$$$$$$$$$C CALCULATE CENTER AMPLITUDES

C$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$555 555555555 $$$$$$$$$$$$$555555$$$$$$$$$$$$NAMP=6MAMP=NAMP+1 ..

22 EXT=ALOG(700.0)POWER=(ALOG(1000.0)-EXT)/FLUAT(NAMP)DO 23 K=I,MAMPB=KDUM=EXP(POWER( B-1.0)+EXT)LA(K)=DUM .

23 AM(K)=EXP(POWER*(B-O.5)+EXT)/TUXC$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$5$$5$$$$$$ $$$$$C CALCULATE FREQUENCY LEVELSC$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$

NFREQ=8FMIN=.0625............MFREQ=NFREQ+ 1DO 38 I=1I,MFREQY=I-1

38 FL( I ) =FMIN*2.0-'.Y

C$$$5$$55$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$ss$$$$$$$$$ssC CALCULATE AMPLITUDE LEVELS . ...........

C$$$55$$$555555$$$$$$$$$$$$$$5$$$$$$$$$$$$$$$$$$ $ $ $ $$ $ $ $ $DO 15 K=1,MAMP - -DA=LA(K)

15 A(K)=D[)A/TUX .C$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$

C CALCULATE CENTER FREQUENCIES ..

CS$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$ $$$$$$$$$$$$$$$$$$$$$sssssDO 16 K=1,NFREQ ............ ...........B=KEXT=ALUG(FMIN) ..-........ -

FRE(J=NFREQPOWER=(ALOG(FL(MFREQ))-EXT)/FRE .-.................FM(K)=EXP(POWER;:(B-.5)+EXT)

16 C(K)=FM(K )600.0 - .. .............

WRITE (6,41)(A(K),K=1,MAMP)41 FORMAT( '0 AMPLITUDE LEVELS ARE SET AT-' ,//,T7F6.2)

WRITE (6,42)(FL(K),K=1,MFREQ)42 FORMAT('0 FREQUENCY LEVELS ARE SET AT',//,9F6.2)

WRITE (6,43)(AM(K),K=1,NAMP)43 FORMAT( 0 CENTER AMPLITUDES ARE',//,6F7.-3) ..--

44 WRITE (6,45)(FM(K),K=1,NFREQ)45 FORMAT( '0 CENTER FREQUENCIES ARE',//9F7.3) --....-.--. ..

WRITE (6,46) (C(K),K=1,8)46 FORMAT('0 MAXIMUM POSSIBLE COUNTS PER SEGMENT-,/-/,-9F1O.3)--.....

WRITE (6,605)605 FORMAT('0 UNADJUSTED ABSORBED POWER AFD') .- -

C$5$$$$$$$$$$$$$ss$ $$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$C CALCULATE AND WRITE UNADJUSTED ABSORBED PUWER MATRIXC$$$$$$$$$$5s$$$$$$$$$$$$$$$$$$$$sss$s$$$$$$$$$$$$$$$$$$$$$$$$$$$

DO 600 I=1,6 ..........

DO 601 J=1,8K=7-I ...............- .APM( I ,J)=KF(KDEG,J )*'0.5*( 32.2 AM( K)) "'2NAPM( I ,J)= A,PM( 1, J )/C (.J) . - .

601 CONTINUEWRITE (6,602) (APM( I ,J),J=1,8)

602 FORMAT(IX,9F1O.5)600 CONTINUE .. ...............CU$$$$$$$$$$$$$$$$$$$$$$5$$$$$$$$$$$$$$$$$$ $$$$$$$$$$$$$$$$$$$

C CALCULATE AND WRITE ABSORBED POWER MATRIX

55$$$5555$5$$$$555$$$5555$555$$$$$$$$$$$$$$$$$$$$$$$$$$$5$55555

WRIIE (6,606) ... .

606 FURMAT ('0 ABSORBED POWER AFD ' )

DO 603 I=1,6 - - --- -- .

WRITE (6,602)(NAPM(I, J ) , J= 1,8)'603 CONTINUEC$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$55$$$$$$$$$$$$$$$$$$5$$5$$$C DO LOOP FUR SEGMENTS ..............................---

$$5$$$$$$$$$$$$$$$$555$$5$$$$$$$555$$5$$$$$$$$5$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$5C$$55$$$$$$$555 $5555 5$5555 5 5555 555555555 5555555 555 5 55555 5 5 5 5...............

C WRITE K FACTORS

C$$$$$$$$$$$$$$$$$$$ 5555 5555 $$5$$$$$$$ 555$$$$$..$$$.......

WRITE (6,210)(KF(KDEG, I), I=1,8)210 FORMAT ('0 K FACTORS ARE ',//,8F9.6 ) ..----...........----. .....-.

TIM=0.0ICHK=ISEG(KDEG)

C$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$5$$$$$$$$$$$$$$$$$$$$C ZERO OUT AFD .... ................

$$$$$$$$$$$$$$$$55555$$$$$$$$555$5555$55$$$$$$$$$$$$$$$5$$$$$$$$$$$$$$$$$$$DO 63 KK=1,8 ........

DO 63 JJ=1,663 AFD(JJ,KK)=0O ..... . . - - --. . ..

$$$$$$$$$$55$$$$$$$555$$$5$$$$5$$$5$$5555$$$$$$5$$$$$$$$$$$$$$$$$$$$$$$$555$$$$5C ADVANCE TAPE TO PROPER ID NUMBER ..............

C $$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$5$$$$$$$$$$$$$$$$$$$$KUX=ISEC/15 .......DO 5512 IABC=1,KUXDO 8020 IVQX=1,5000............... --....

READ (OEND=5200,ERR=5100) ID,IFXIF(ID.EQ.ICHK) GO TO 8021 -.... ....

8020 CONTINUE

8021 CONTINUE .--------..

C$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$5$$$$$5$$$$$$$$$$$$$$$$$$$$$$$$$55555$C WRITE ID NUMBER ... - - - ... .. ..C$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$555$$$$$$$$555$$$$$$$

WRITE (6,8888) ICHK -....- -------- -

8888 FORMAT(1X,'ID NUMBER=',I3)C$$$$$$$$$$$$$$$$$$$$$$$ $$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$5$555555$$$$$ --

C DO LOOP FUR FREQUENCY BANDS

C$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$ 55$$$55$55555.............DO 1001 IX=1,8COUNT=0.0DELT=1.0/256.0IF(IX.LE.6) DELT=1.0/32.O -- . .. . ....-----... . .....

KFREQ=IXIs$sss$$$$$ $$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$%$$$ $$$$-$-$$$-$$$-$$C SKIP FFT CALCULATIONS FOR FIRST FIVE FREQUENCY BANDSC$$ s$$$$$$ $$$$$ $ $ $$$$ $$$ $$$$$$$$$ $4 $$-$$$ $$$$ $$$4$-$$$$$ $-$$

IF(I.X.LT.7) GO TO 1003C'$$$$$$$$$$$$$$$$$ $$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$5$5.$$$$$$$$ ...........

C FFT CALCULATIONSC $ $ $ $ $ 5 $ $ $ $ $ $ $$ $ $ $ $ $ $ $ $ $ $$ $ $$$$ $$ -$-$ 5 -- $$ $ -$$-5$ $ -$-$$$-$-$ $5 $ $-

10 0IV = 0 .-DO 1002 JX = 1,480to = X, + X ) - ------ :., REPRODUG] ILITY. -OL

AA = IFX(JX,IX) ORIGINAL PAGE IS POORST(I ) . =- CMPLX(AA BB) -... -

IF(1Q.E0.32) GO T(.) 1019

D-3

GO TO 1002

1019 IQ = 0CALL FFT(ST,W1N,Nl,L2N1,1) ....

CALL FFT(ST,WIN,N1,L2N1,2)DO 1006 I = 17,32IIX = I + 224

1006 ST(IIX) = ST(I)DO 1007 I = 17,240

1007 ST(I) = CMPLX(0.0,O.0)CALL FFT(ST,W2N,N2,L2N2,1)CALL FFT(ST,W2NN2,L2N2,2)NXX = IV'256 + 1NYY = NXX + 255

J = 0DO 1030 I = NXX,NYYJ = J + 1

1030 X(1) = REAL(ST(J))/32.0IV = IV + 1

1002 CONTINUE1003 CONTINUE

IADC=0 ................ ......

ISW=0INEW=O .IMAX=30

C$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$-C NSAMP = NUMBER OF SAMPLES DIGITIZED PER FREQUENCY BAND PER SEGMENTC$$$$5$$$$$$$$$$$$$$$$$$$$$$$$$$$$5$$$$$$$$$$$$$$$$$$$$$$$$$$$

NSAMP=3840IF(IX.LE.6) NSAMP=480 ..

C$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$C BEGIN PEAK DISCRIMINATION .C$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$5$$$$5$$$$$$$$$$$$$$$$$$$$$$$

DO 100 I=1,NSAMP .....

IF(IX.GE.7) GO TO 110IADC=IFX(I,IX) -...........

GO TO 111110 IADC=X(I) ... . - ....

111 COUNT=COUNT+1.OIF (IADC.LE.IMAX) GO TO 120ISW=I

77 IMAX=IADC ...GO TO 100

120 IF(ISW.LT.1) GO TO 100 ...IF(IADC.GE.0) GO TO 100INEW=INEW+1 ...........

NPEAK(INEW)=IMAXTIMEO(INEW)=TIM+(COUNT*DELT) ...IMAX=30ISW=O . . . . . . .. . . . . . . .

100 CONTINUE95 IF (INEW.LT.1) GO TO 99 . ...

C$$$$$$$5$$$$$$$$$$$$$$$$$$$$$$$5$$$$$5$$$$$$$$$$$$$$$$$$$$$$$$$$ssC WRITE HEADING FOR PRINT-OUT - -- .

C$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$WRITE(6,951) KFLE,KDEG,KFREQ .........

951 FORMAT(T7,'RUN=',I1/T12,'DEGREE=',I/T17,'FREQ BAND=',Il).WRITE (6,954) ..... .. ......

954 FORMAT (1H0,T27,10HTIMEO(SEC),T47,8HAMP(G'S),T67,3HAP ,T87,4HNAPC$$$$$$$$sss$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$5$$$5$$$$$$$$C IF NO PEAKS IN THIS FREOUENCY.BAND, SKIP TO NEXT

C$$$$$$sssssssss$sssss$$ss$$$sss$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$

DO 1009 JJ=I,INEWC$$$5$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$ $$$$$$$$$$$$5$$$.......

C CALCULATE UNADJUSTED ABSORBED POWER AND ABSORBED POWER

C$$$$$$$$$$5$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$5$$$$$$$$$$$$XPEAK=NPEAK(JJ)PEAK(JJ)=XPEAK/CAL .--

BPEAK=32.2*PEAK(JJ)AP(JJ)=KF(KDEG,KFRE()*0.5*BPEAK**2 -. . . . .. .

NAP ( JJ ) =AP(JJ)/C(KFREO)C$$$$$$$$$$$5$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$5$5$$$$$$$$$$$$$........

C PRINT OUT TIME OF PEAK OCCURANCE, AMPLITUDE OF PEAK, UNADJUSTED

C ABSORBED PUWER AND ABSORBED POWER OF PEAK .................-C$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$

WRITE (6,93) TIMEO(JJ),PEAK(JJ),AP(JJ),NAP(JJ) --- ....

93 FURMAT( T30,F7.2,T50,F7.2,T65,F!2.3,T85,FIO.4)1009 CONTINUE .... . . . . .

C$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$

C COUNT PEAKS FOR AFO AMPLITUDE BANDS .. . ... .. . .

C$$$$$$$$$$$$$$$$$$$$$$$ $$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$DO 1010 N=1,INEW . .- ---..-...................

IF(PEAK(N).LT.A(1)) GO TO 1010DO 1000 J=2,6 .............. .

IF(PEAK(N).GE.A(J).) GO TO 1000

JJ=8-J ------

GO TO 10051000 CONTINUE

JJ=1

1005 AFD(JJ, IX )=AFD(JJ, IX)+1 . ... ..... -------.. . .

1010 CONTINUE9 9 C O N T I N U E -.. . . .- -.. . .. . .- - - -- --.. . . . . .. .. . .

1001 CONTINUETIM=T IM+ (COUNT*DELT )----------

5512 CONTINUE

C$$$$ $$ $$$5$$$$$$ $$$$$$ $$$$$$$$$ $$$$$$$-$$$-$$$$$$$...........$-C AFD COUNT NOW COMPLETE FOR CURRENT DEGREE OF FREEDOM & FREOUENCY

C HEADING FOR AFD PRINT-OUT - - -- . . ------ . --------.. ...

C$$$$$$$$$$$$$$$$$$$5$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$WRITE(6,951) KFLE,KDEG - - - -...--- ----------------

WRITE (6,54)54 FORMAT(1HO,T25,'AFD OUTPUT') --- -... ..---- -------

C$$$$$$$$$$$$$$$5$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$

C CALCULATE UNADJUSTED ABSORBED POWER AFD, ABSORBED POWER AFD-, TOTAL-C UNADJUSTED ABSORBED POWER, AND TOTAL ABSORBED POWERC$$5$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$-$$$$$$......

SUMAP=OSUMNAPO = .0-..-.- - --------.. .--- ------- -

DO 550 I=1,6

SDO 551-J=1,8 - --- -------XYZ=AFD( I ,J)

- A P A F D ( I , J ) = X Y Z A P M ( I , J ) .. ... .. .. . .. .... ... . ... ..

NAPAFD(I,J)=XYZ'"NAPM(I,J)SUMAP=SUMAP+APAFD ( I., J ---- -

SUMNAP=SUMNAP+NAPAFD(I,J) .

Cssss$$$$$$$$$$$$$$$$$$$$$$ $$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$------C PRINT OUT AFD, TOTAL UNADJUSTED ABSORBED POWER, TOTAL ABSORBED POWER,C UNADJUSTED ABSORBED--PUWER .AFD,- AND-ABSORBED--POWER--AFD---------------- ---C$$$ $$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$551 - CONTINUE -- - - --- - --- --------

WRITE (6,400)(AFD(I,J),J=1,8)

D-5

400 FURAT ( 10 t7)

5tO CUNTINUEWRITE(6,801) SUMAP,SUMNAP

801 FORMAT(IHO,T12,'SUMAP=',F7.3,T35,'SUMNAP=',F7.3)S WRITE (6,654)

654 FURMAT ('0 UNADJUSTED ABSURBED POWER MATRIX')

DO 650 I=1,6WRITE (6,651)(APAFD(I,J),J=1,8)

651 FORMAT (8F9.3) ...

650 CONTINUEWRIIE (6,653)

653 FORMAT ('0 ABSORBED POWER AFD')

DO 652 I=1,6WRITE (6,651)(NAPAFD(I,J),J=1,8)

652 CONTINUE .....

8001 CONTINUESTOP

5200 WRITE (6,5201)

5201 FORMAT (1HI,'END OF TAPE') ...STOP

5100 WRITE (6,5101) .. ........

5101 FORMAT (1H1,'ERROR ON TAPE')

STOPEND

CA$$$$$$$$$$$$$$$$$$$'$$$$$$$$$$$$$$$$5$$$$$$$$$$$5$$$$$$$

C SUBROUTINE FFT $$

C IHIS IS THE FAST F(JUkRIER TRANSFORM SUBROUNTINE USED

C TO DEVELOP DATA POINTS FOR THE HIGHER FREQUENCIES WERE

C THE SAMPLING RATE WAS NUT ADEQUATEC$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$$

SUBROUTINE FFT(Z,WXW,NXN,L2NX,NCX) ...............

COMPLEX Z(256),WXW(256),CMM,DMMIF(NCX-1)10,1.2,11 ---- ..........

10 DUl I = 1,NXNTWP 1M=-6.2831854A = FLOAT(I-1)*TWPIMv/FLOAT(NXN)

1 WXW(I) = CMPLX(COS(A)tSIN(A))RETURN

11 DO 2 I = 1,L2NX .....

K=24;-( I-I)K2=K42 . . .. ....... -----.-.. . ... -.. .

KK = NXN/K2

DO- 2 II=1,KK ................................................M= ( I I-1)"K2D00 2 III=1,K ....... ...

J = (1 1-1)*KK+1L= I I+MLL=L+KCMM=Z(L) . . . .... ......-

DMM = WXW(J):=Z(LL)Z(L )=Z(L)+DMM

2 Z(LL )=CMM-DMMRETURN ...............

12 DO 4 I = 2,NXNK=I-1 - - -..... .. .... .

KK=0DO b L= 1,L2NX ..................

J = 2**(L2NX-L)JJ=K/J -..IF(JJ) 5,5,6

n) A

6 KK=KK+2-* (L-1)

K=K-J5 CONTINUE .

IF(KK-I+1) 4,4,77 CMM=Z(I) .. . - ... .... .. ...

Z(I) = Z(KK+1)Z(KK+1 )=CMM

4 CONTINUERETURN .........END

D-7

APPENDIX E

Reduced Bus Data

REPRODUCIBILITY OF THEORIGINAL PAGE IS POOR

RUN 2, DEGREE 1

(Note: Degrees 1, 2, 3 are degrees 1, 2, 3 for front seat;degrees 3, 4, 5 are degrees 1, 2, 3 for center seat.)

Frequency and Amplitude Bands are set as follows:

FACIORbS AP,

O 000082 0.P003() 0.00132, 0 )jL- 3j 0.j ,4r..1£1 i. . + [.9. o0 ,,3t+70

I,,c LI U E I.LFVELS ARL SEI .,-Io.~ t) . iI C,, ()J, o

7 0.11 .17 i.26 Oosi ,Jb i,

U h, j i 01F kLUUEt-NiCY L-VF-LS fRE SET -f

.06 0.1? . 5 .. 50 1. o - .U2 u o. ou0 1 ,.) ,

.'bo7 0 , -136 .212 .3,30 0. f 1 3 .

.TEr FRFOUL.iC I S i HRE

0.0 b8 U. 177 ,o354 Ol7 1, ( i 4 2. .70:- 1 . 31 .

,,IMUM POSSIdt_ L COUNTS PER b)Ly,-LT

1.3) 2,652 503 o3 10.uJ/ ?I .?13 42 .42 o ,4. 5 lo9, t05

, -SU.),hED! POWE,'R: , A,: RIXU.02729 001'9 3 0o4,,, 9/ 1.4( Io ,.-.- 711 4 0 .. 36,-3 4a 130tJ 12.1.37

. .. . . - 9 ... 7' 1 4 o, :3'.3 48 d 513, 4 I . :37 9

0.01125 0 0 4bdu 0.1bl 0.7/2 0 3o3i4b 16 0 b6501 2.0185v IV121}. 125 C, !. ! c 14 1) cf I D ,3 ,, f/:: 3, .i 25J o61 ('. . ],61b 74- , t) . I"

0.00464 i. )163 C . UY490 0 390591 ,-t- I .o2"5 - *, .1 70.00191 0 .0 C7 19 .030 0.. ti o :5-3 ]. 0 -0 0 3.4o J 3 1 1 ? - 3U0 U0079 C.i 17 (:V? 0 .o: 0 0 0 -19 4.166 5 1 :ijo 0.35C1uI U0032 .0 131 u. "+ . ;,+0u 3 0 7+8CY7 0.5 /52 0.1,4-4+31

O 'i, AL I ZEI) ,bS --- P U . I AS * 0P5 - . 0 . 061 . 1.. U. 3 0. "24,5 0 (. b / I0.0( ,+8 0 . 17e 1 / , .c U . ic. ' . 9 1 , 0 .392 30 ) 3.2.5 2 U. )2"1 oi.UU3i ) u.u J;3 u. 1-+12 (.03J, * '5 03.10168 ). 97c23 0.01215

0 . 0 4 0 1 el 7 0 0 i.0.300 t4 C I0. 0 U (:;6t+u 0.1 1 * K'?1' . U. ud7,l 0. U12'Y1 U. 0u I

Co JO 1)0&4 0.U49 j0.0 U.C:dJ . )J+49 U.x11-33 U

REPRODUCIBILITY OF THEORIGINAL PAGE IS POOR

E-1

RUN0e. HUN-A

IEGOEF - rEGHFF= IbtoMCNT. I SEuMEN1* 3

AFU LUIPUI At0 OUIPUT0 0 0 0 e 0 1 0 0 h

0 0 0 1 a , 15 1 1 0 u 4 j I /0 0 0 1 3 1 4', 1 0 U 0 10 0 3 101 0 0 0 7 h 48 0 0 2 4 7 0 17 9'0 0 0 1 I 4 2 2 1 / 6 13 t 12U3 24 0 0 0 3 e 10 10 6

SUMAP=43A.087 SUMNA.P 0. 160 SUMAP=SO.939 sU tp. .3

Adhok0b POwER A.0 ASO4E0 potwk AFL)0.000 0.000 0.000 0.0U b16.31. 4 .. 436 0.00U 24,7 0.000 0.110 0.000 0.00t 0 0.0 '.oO 0000 72.b2

0.000 0.000 0.0ou U.7e .3*. I. n1 0.000 75.01 4 0.011 0.044 0.000 .. 000 13 ~. 7 .ou ?0.019 J39U.I/b0.000 U.000 U.uU U 0.410 4i I -1 ;.oUOU h. •b 8_.40j 0.005 0.00n 0.00 . 0 .000 l 3* 00 2 ... 1 14 *.J IU0.002 0.000 0.000 0.0U00 4.Ql 11.3j 20.401 40. 13 U. 0000 0.000 U.0600 . 50db 4.1. 2 uou t77 .t3 3.1.ob

0.000 0.000 J.0ou U.054 0.14 - I. I. 14.013 15.0/ 0.002 0.0.16 .013 o o.31 .4117 15b.h 35.03 .3 .O

0.000 0.0A U.00u U.17o 4.504 3.Jb5 1.0 V J.Uuo 0.000 0.000 0. U U.UV .08 .195 4..4, 1b..1', 0.Ub0

tJORMAL 1ZFD AS(0SdF0 P3ot.. AFU0.000 0.000 0.o000 0.0 GU J.7/ . bj 0.v0 0.143v.000 0.000 0.000 U.073 . . rtb 0.000 0.4,.40.000 0.000 0.000 0.03 .1,7 O. 0t:u 0.097 , 0.'d6O.I001 0.000ru 0.000 0.000U 0.1 .y ./ .024U 0.o.du0.000 0.000 0.O0v 0. U1 v.b. t .35/ 0.65 0.091

SU.000 0.000 0.00U2 0.U17 ;.ved .0/9 L75 0.2l

NUWMALIZED AbbURtBEU PUW AFUU.0n 0.04I 0.000 0. 0 0.0 0 *. JUU 0.000" 0.42v

0.008 0.017 0.00O 0.000 0.63 0.000 n.236 7.099

0.003 0.'000n U.000 0.000 .046 0t;. 04 o.dO v. oS'

0.000 0.000 .012 t). 049 0.149 0.iI00 0.6A _ U.t .I

0.001 0.00 0 0.002 0.u36 .0.0 7 U.J.4 0.413 0.02-

0.000 U.000 0.00u 0.006 pt.u. . 113 .19 0.33

-UN=2o ... kF..IHUN=2 O rSFmt 4

StEo tN1= 2 AU UU

AFU 00 UrutO 0 0 0 0 0 ' ' 0

0 0 0 0 0 4 0 0 u U 0 . 0

I 0 0 0 0 b 0 0 ) U U 0 U

0i .. 1 0 0 0 0 1 3'

1 0 1 1I1 40 0 1 0 0 1 by 1 6

0 I 1 4 0 1 1 t 1 e

0 1 SU4APs,4 1 .365 bUsiNAPt 1.762

StiMAP.713. 659 SuoAPe o.(.'0 ,1~[ . Oc1'1q.4L1 q AbSUNO1F 00 003'kfl

ASOHUo0 PowFR AFt. 0.000 0.000 0.000 0.004 0.-00 .0., 0.000 0.0nU

0.000 0.0,00 0.000 4.(00 .,: .10 0.ono 8.55u .0U011 0.000 0.004j 0.LOu 3... ... t. Jr. .2 V. 'u

0.00i 0.000 0.000 0.3J u.90u i ., , . 0. 100 ,I.o0.000 u.000o 0.000u 0. o, . j ' .10 .. u .. , e.oU 000 . 0.003 0.000 0 00 1 1) Q I ., 1 (. 1 4. b1010.000 0.001 U.00J v.111 .ol o 1. 74 1.UoL

NUIOOLIZJ&D o'uOk0LU P'Ot AFu1 0U.000 0.0,0O 0.000 0.00 '.0 .0 .v00 0.0000.01:8 0.000 U.000 U0OU '.r0 *, -. : 0.000 o.I0v

0.01) 0.001 0.000 0.U0 t, . 7-', C 0 * 0.01 1, .1 010 U*.00U0 0.000 0.uOO .0: "0, ' U.tQU0 0.000 U.0

u.000 U.000 0.000 0.00 0.ouJ . .vou d.O40 IN.J.f 0.000 0.0n00u 0.(00 0. 00t ..1,I .0 00 .o .10

0.002 0.000 0.031 0.131 .804 2.01l 57.03 3 o.03 0.000 . 001 t . u -. .0.100 2..,t, ".,.j 0.)17 0.1, 00.001 0.003 0.013 0.18 0I h"., 2.aJ3 . 0 0.00 o Soo.Uo U.0o00 U.uou 0.1. o.0oJ_ L.'Uu 0.1,4 0.C.b0.000 0 .oI 0.005 0.11 1 . v.1 0. 08 10.9,3 0.144

NOkMALILEI) AdSOROEv PUAL. a0.000 0.000 0.0o00 0.000 . .0:0U u.U0n U.deO .0.00 0.014 0 .000 Q.v .10 ... 0 " 0.00 1 .'50

0.000 0.070 0.000 0.0o j..i I . 0 0.UO 1.U5U.001 0.000 0.0V6 5.01 ' J, V'.oh? o.001 ,. .JO

(.001 0.01 .?u0 4.011 ,.0 . .4', 0.*0 t.to0.000 0.000 .001 )0.011n .0 l .iJ 0.1 0 v .o I

0 0 0 0 0 0 0 11 fu..... F OUTPUT

1 0 0 0 0 u v 35 0 0 0 0 0 0 0 S15

0 0 0 0 4 0 2 53 1 0 u 0 0 b6

0 ' 0 0 0 5 1 5 0 0 0 1 .b

0 1 u 3 7 J J1 25 0 0 o 3 11 u I - 00 1 1 * 3 Jb 7 I 1 2 , 3 o 0 14

0 1 4 5 .0 17 10v 4SUIAP 585.545 SUMI4IP- 4.b5i

'AtiAP=14.704 .SUMNAP. ot

ASHEDPO.EW IkO 5f l ISMP78.704q0.000 0.000n 0.000 0.000 .000 0.o00 0.000 133.1I. AU.SOO1I) 'oE1 AF

0.011 0.000 0.000 0.000 .*0 : . 0.000 175. 0 0.000 0.0on0 0.000 0.000 .V 0> .ll00 0.t. 2 .1 Un40.000 0.000 0.000uuu 0.000 b0. "; .0 u 1.)0 1. . . 3 U0.011 U.00 0.00U0 0.000 Q . * 'U ).,onU edu0.0

0.000 .0 .0 .000 9.000 2. u6 .dU31 20.01 3J.23 j3 U.0 0 0.000 0.000 0.316 1 1*-'- .2000 51.757 90.'7f

0.000 0.003 0.000 0.102 1.003 3.t00 43.440 1.144 0.000 0.010 U.000 0.394 0.30. .1,10 47.000 13. 70.000 0.001 0.0QS 0.134 U.73 1.442 Z0.791 1.010 0.001 0.003 0.025 0.3e4 u .7I.v A.000 3. 23t 4.VU2

0.000 0.001 0.0o I 0V.111 I.105 e.17 3 91073 0.b7NO0MALII) ASOl U.E0 POw..O A0t N L

0..000 0.000 0.)00 0.000 0.1', . ,J 00 0.00 0.MF . ... NOOMALIZEOO AUSR2.O POowE AF,

0.000 0.000 0.00 0.000 J.,l0 .. v7 0.07,0 1.03l 0.000 0.0,0 0.000 0.0 00 ,.00 1.v 0.oO l of 3.000 0.0.0 0. 00 0.000 2.Oo? 0.040 0.194 0.644 0.000 1.0011 0.000. 0.000 0.700 1..000 0. 0ou I0l

0.000 0.000 0.000 0.000 ".130 .00? 0.240 '.005 0.000 0.000 0.00 ) 0 0.030 0.(00 0.0,1 0... ?0.000 0.001 0.000 0.015 ol'd A 0.000 0.A t' O.5! 0.000 0.000 0.000 U.037 ,0.,v .0V')0 0.41 O.LU0

0.000 0.000 .01 0.013 ., ,0 ,j1 (04 0.00 U.001 0.0l1 2.Uub 0.031 .., ... 01b 0.404 0./'?0.000 U.010 0.0U4 0.11 .,"00 .,.1 3 0.1 9 U.UUJ

RUNL2 . RUN2

SFGMLt o F.(iL 0

AFU 0 01,0T "AFU OUTPU.0 3 m 0 0 0 0 0 0 0 0 0 0

2 0 0 0 0 0 Q 00 0 1 0 0 I 0 u

Ad I 01 62 1 2 A 9 0 2 310 1 , 0 S . 2 30091 5 5U3r;5P

SUMAP. 29.0 SUMN.,P 0.522

ASURdED POWER AFD , 0 350 I 0 0 0 0 . u2 II 0 u 0, 2 0

-- 1 1 0 0 0 07

2 a I A, O "'

I U 3 3 7 0 5'

0 1 0 3 7 2 1e 4d

SOMAP. o0.010, 5"1NAP- 0.06

AdSUktFD 0o,,fW AFO '

0.000 0.329 0.000 0. 100 .)) ,.0 01') 0.000 oo 000 0.000 .110 o 0.0u u.000 , .O 0 . nO 0.000

0.027 U. (.u U.o u. Ob ,l ' ;0..0000. 0.1u 0 (0 0. U(tI .us1 0.045 . 0. .U0 u,000U

L $.,

0 ' .000 0.000 0.000n

0.000 0.000 U.07b 0.000 0.:00 1.0v)0 0.n000 u.0u0 0.00O v0.nu U, 0.0. ."0 .., o j.-r.1 -e,

0.002 [.00 0.0b A.000 0.Q73 .0n0 0.000 6 V7 0.00? O.(nl 0."31 U.000 1.I.. .0 0 . UO ?)0.J31l

0.002 0.0,13 0.025 0.054 '.i2b 7.2od O.no0. 0 1f.0*. 5 O.001 0.000 2.030 lb *. I . (.11, j. J2u 1 n .eo

S 0.000 0.001 0.1)00 0.0045 .*o l .1.e 1 *. 1S5 5-1,4 0.00)0 0.01A1 0.000 0.06? 0.70 1 2.000 1 .30 o.'.0

% NOKMALIZLI) AMS(R.V Pw AFU NUO:MALIZED Au f)Ru : J 0' v .LN -t A, ,

t.005 0..14 U0. o ).Ou .,IV 0 0 00 V.000 000U 0.000 0(.041 0.000 U. 00 v. ) V .0O0t) 9 * o000 U o.000

0.017 0.0n0 0.01 0 U.070 U . 0,0 :.bu 0.000 (1.0(U0 0.00 0 0.117 0.00. 0.*10 . ,- .1 0 r, ,. 11) U.0,00

U. 0 C ,0A)0 0.1114 0 .0 U 1. O 1. , 0:1) 00u0 ,uU . U. U7 U.000 U. N f.UUU A, .0 .') V *U OU 0.000 U.('*?o~oo) O.N ,3 O.O~d O. o}u - u. tH r :..0ch' A -~~h An 3,* 0. 0 ov : .. O (*.) U ,Ou 1. UbW b O U 4O , *(

0. 00 : ,,: 3 ,.l, 0 0,0.. , 2001 01.003 . 0 0. .10 1.4 L .0.0 1 0 O.uoU 6. L0

S 0.001 .01) 1 0.), ) .'.. A 0.I 1 0. ....0 0.0010 U - 0.001 0.0f 0 0.00/ 0.00 s .') .011V 0.".-

0 ,.101

0 .. .01)1 .11).00 . 0.000. . 0.0+..0.. ... 014 .0.0 . . . .00. .. 0.100 0.000....U14.0....10 0...t L .0.U .JL2L...*L4L.

HUN.2 UN= 2

OEGRFF.=1 DEn,EF=

SEOMEN. 9 S,MENT= 1

APU OUTPUT AFO OUTPUTo 4 6 2 .3 ..t (3 ' 0 0 0 0 1 30 U t

0 v 1 0 3 0 0 0 0 u

1 0 1 0 2 3 2 49 0 0 0 1 5 0 0 5

2 0 2 1 6 2 1 56 I 0 2 3 e 0 2m

0 0 0 4 5 7 19 20 1 1 3 10 4 ,2 1 to

1 0 2 3 . 1" 1o 1 1 0 1 2 I 19 34

iAP62.7 SUMNaP3 9.M6 - SUMAP.130.U3 SUMNAP- 2.606

AUSOtI4ED POWEH AFU AHSOWH0 0) P3WEH AI1

0.000 0.439 2.205 3.78 ?.,l I.a 3 o I I 0.0 0 646S0 0.00U0 0.220 U.0000 0.000 0.1t 0.0(U 0.000 0*000.000 0.091 0.000 0.772 1 -bf60 60.0b o.V 0.02? n. n4s 0.000 0. 0,J 3.3.. 0.000 0.000 0.,I

0.000 0.000 V.0 09 0.31 b .45 60.000 6.0oU I .OU

0.00? 0.000 0.062 - 0..)94 S 15$ 5.1 .. e( 3. 1.0u

0.001 0.0 3 0. 3d O.6 41 0.4 5 1 s o 9 1.n1 . .. 11

0.000o 0.0n1 .000 0.02 e . .1 *173 10.97j3 4.4 * ,0

NONMALIZED AUSORbEO P0 AFU .000 0. 000 U.0.000 0.003 O.UO 0.000 .309 0. 0.000 0.000

0.005 0.000 0.015 0.000 2.11 . bo.904 16.500 4.o032

0.004 0.000 0.U 0.13j1 2.036 5.661 3u.bol -47.579

0.000 0.000 0.000 U.216 1.fdj B.1"6 2b..hS 9.o0'

0.000 0.000 0.010 0.060 0.4d7 -. 404 10.395 2.3Jq09

NORMALIZEII AHSUREU( POWLM AFUU.000 0.166 0.41l 0.353 1.1,0 2.od9 O.n000 0.6.

0.000 0.034 0.000 U.073 O.00u 2.3,93 0.10d 0.JS,4 0.017 0.017 0.000 0.000 0*1 0.001: 0.000 0.00

0.003 0.000 0.014 0.000 0.131 ,.40*6 0.194 0.059 . 0.000 0.000 0.000U U.0jU ,.3b .0*u'3 0.000 0.0910.003 0.000 0.12 UO.012 v. 33 0.133 0.J.1 . u 0.001 0.000 U.012 0.037 0.2 3 0.133 0.000 U. 34

0.000 0.0000 00000 " U.020 t0.3 :. I 0.to4 0.u :.001 0.01 0.0? U.051 e. * 0.30 0.01 . 1

0.00 " .0 ) .3 ? 0.1.00 '0.,,: .0l 0. 3 .01' , ,,n r n, , , ,, . , 1 1

"UN=.? WUN2IDEGREE1 DIEGHFF=I

SEG L NT- I n SF w'tul l

=12

AFU OUTPUT AFU OUTPUT0 0o ouo'ut ou 00 00

0 0 U 0 3 3 2 0 0 4, 0 0 , I

1 0 0 0 £ 1 0 0 0

0 0 0U 0 J3 0 0 1 0 30 o 0 2 II 1 3.. 0 0 0 0 b | 6

' I 1 0 5 5 1' 20 . 0 U '0 I 1 1 51

0 0 0 10 eo 23 U U 4J 49

StUMaP=305. I I IIN.P 4. JV' SUMAP- 66*ieJ2 SUmNAP- O.Y72).A 0 14 1 4V 3 .- ; .3

000 . '30F U.000 0 00 . 0.1,10 (.000 ?4.75 O00.nO 0.000 0.000 ,j0 1 oo.O p.U e. 1

0.Oil 0.000 0.000 0.000 0.3 0 .0 0.000 9.043 0 (.011 0 o .U U .UOU V .00.

0.001 0.00 0.000 ,000 o. 1=0 3*.(9 0.000 95.043 0.011 0.000 0.000 0.000 V. ,0, (.00- "0 2o. o'0.000 0.000 .000 0.P) 00', " 1.3 o' J.0 70.b5 0.000 0.000 0.000 0.000 1.39 .U . 1,30

0.00O 0.203 0 u.00 U dl U .. J l , . 1-4.1oh3 31. 3 .J 0.000 0.0(0 .00 0.00 3.34 .. uU 3.o'0 *.0. jd

0.001 0 0..03 V'.000 .270 -. 0 *1...0 3o.236 I.. 300 0.oo 0.006 0.000 0.1064 3.3 1.13,7 1 .. I I I.0,0

OMAL I1ZE11 10SORmEU P(wk J u NORMAL IZL ABS5RbE0 POh U0 0 . U 140.00o0 U.000 0.000 U.000 UC 0. 00 0.000 0.13. 0NU.300(10 O.OnOU. 0.000 0.000 .tb . 0 0.

0. 00 0.0 0..000 . U * i41 .100 ,.Ono .00 .008 0 0 000 .o 0.000 3*) ".(3 o.o00 0. 1o

0.000 U.3(30 0.000 0.u3 V .. : .. j IV ,.un u 0.6b 0.000 0.n000 .3o0U u.000 ', 0 00 .. 0.

0.000 0.00O 0.000 0.o0 ) , ?5 . 97 *03 0.041 (.0 0.000 0.000 O.000 .30 (.100 (.030.000 0.000. 0.000 0.02 0 . 1 !..7. .462 0.10b 0.00 .Ow2 0.000 0.30'0 *0... .0 . 0. 0 -. _

UN2 DEGREE Aft OUITPUT

5VGl!tNIT13 j 1

AFU0 2 0 1 1 9

o 0 ' s0 0 s

AF 0 0- 0 2 1 0 A I 3

0 0 0 1 9 e 0 1 j 10 1 1 *

0 0 0 44 4 3 2

0~F 0 Q U IT

o 0 0 0 U .:O 1 :100 0 0 O 00 0 091

) o5 U . 3 . 3 1 4 0 V

AHSOR"FiO pjowEW( AFII 0.n00 -. . 011U 0,0n0 ~0 .0 .o 3b e 1H.ol 0.,~ 1-ni 1%,-Ob

0, 0 , no . 1,0. 1, 01. o0 0o~0 ,V5, 1 .) ono U. 0 .00 u.13 1U - -6," 01. 1

0.000 to.OU0 O.OO u . 0O 0V.1" U OU 0.equ 162 .bt, U.00? U .(ou v.013 U. 162 e. j,, 5.+ t-01) O 9.t'

0,00O 0 "0 0 UOu .0t0"'t I I.O'/ 3 , 3 6 ,JO 0.000 0.000 0.Ul O 0.O09 21 l I*, "

0 0* l

o h j1.

0 00 003U

O

3

.

0, 0 0,0"10 1 141 4 30 0. 12e I 0n 0

UOE .UU .,1 . 1 ",,

RUNA12

1S001 004) F e-. U.000IlO S1 OI2.4

OQ 00.000 0.091 0.000 0.t 12 3.0.. 3l.3l I001 41

0.000 0.000 Q. 0 . n0. O ton 0.'n0 1 .0 71 .001 0.100 .000 ).1 U I .1i0 0U133 0.240

U 10

AF Ono U It0OU 00lU. 133 0.001 O.0 0 0 .v 1 , i- 3. A 0 4 V.1Ie. 00 . 0.00 0.000 ... . ; .Ul.0 000 00 0.0 1 0 . 0,0 10. .0 0.00 0.3 0. 0 ..

0.0 0.0 .0006 0 2AioUD n n 000 000 .. ry 000 *

0.0 0 000 . . 00 .0011 0.00 00 ,*o .0 U.00

0.U000 0.00 0 0 0.0 00 t.oi), I.... 0.000 * .P I ' .e.O00 0.000 O 0 . 5 .. / 1 .AU2 .... ---...----

A0 0 P E A0.000 0.000 0 0.o1n

3

00 v w'-13 0.17

0.000 to 0.U0 U3. 0 ..000 0.( to 1 6..60 *

0.000 0.001 0.000 0.010 0.010 .*jo0 3.131

1.240 4.113

0.0LL 0 6 "~ 0 1 10.0 0.4 5 0.03 0.1 00.SEGMtEN = 0

0.000 0.000 0.0000 0.000 0. 0 0.1300

AU OUTPUT

0.00 0.00 Po s .0 1.. 1 01 0 0 2" t ,

0, 000 00 010 0 .11,11 . 00.000 1*. 1 U

0.01 0.00 0 uou 0.0 1.0' S', 0. I 0 .000 0 .1 d1 2 1 5 1 0 1

0 00 0.000 0.0 U.u ,0 .* 1 0 .01 . , 0.000.0 0.* fl11 (. 0 '..11 .11 0' 1.S .1

0.0 .0 .12 UOQ 0 0 .00 0.1 0 0 .00 __ __ _ __ __-

0 .000 o .oo 0.000 o .llt ______u

, 7 e a o a 0 5 o s s

0.000 0.000 0.000 0.00 0.00 1 o 35

,10 7 = 00

A I 0 0 0 2 0 0 1 * J *

0 0 0 .1 0 0 0 1. 0 0. 1 0 0 0 0 0 o

o 0 0 U10 0.o . 03:o l**8 B i

14.90 - " 0.1 0.01.RUN-2

IlNI)~ 1i91 I" I

SI-',04 N I lI

1U U1 01 1 b0 II ) n 0 0 0 A

00 400 0 , U10 Q0111 . 4 L0 o 35 .lb

.. 0 1 0 0 2 10 2 30

. 0 0 1 o 0 . U000000 1.0910o .0 0 .. l *0 1

00 0 00 0

U .1

1=11 " 0 0 0I 1 0, 0 4

0 0 2 4 1 3 30 1 0.0 0. 000 0.0 0.0t, .11'i' ., V1 4 1.1 aI

0. .00 O .000 o0.0U 0.100 0.,O0 0,U(10 3.010

O.00 O 0.000 0.U00 vO U .'11 0.0U0 O.0o0 72. ISb

0.001 1S b.0.00 0.060 0.00), V.000 I.9.h 0,.b 10.414 1,4.101

* 0.000 AL.0001 0.000 0 .tv U 4'0. ; 1.0 13.01 . bI

NIMOL 1 Ui0.0 OLU 3.O L0 Pl'o1- 110F)

0 .00 0 (. 10 0.. 0 0 . -. 7 t 0 .0 1lJ 1 . (o If.il

1 h

07 .,b 0

0.000 0.0110 0.000 0.000 U0'11. 0.000 0.000 e4t 310

00U0 0.000 0.000

00000 ll0lO21b

1-11 vti0U 40..06 0.300

..... 00 "-741. 13 S *,100 0. 0 0.0)1, 0. 01,0 b 00010 U.10 1i) i. ¢0,. .tii,0 0.01.0 11o31

0. 0 01.001

0.001 0.000 jU OoO

..4? 17.,3.2i

.1 0- .l

NA~~LZ E0 OFO UjR F)FUaTU

U.000 0.70,3 (. 1 V .0.1 0 V.1i ,1 0.U010 0.000 .000 0.001 0.000 0.000 0o lO . .10) ,113 0.107 0.000

0.020 O0 .O 000 0 0 0 .0 3.3/4 .OOU 0.0 0 3o 0. 100 __ T,. ,,l1 1 2-' 1- 10

0.1000 0.000 0.3)71 0.000 I3."J 00 .. ll ') 0.0 107 iM.603 ________________________________

u.0 0 0 .10 0. 0 t .00o 41,ll? I .010 0 3.0I01 3.1.1 00l 1J 11

0.001 0.0 0 0.OO 0.21 , . 7 . 46U 0.3 1 U 1 590 n1

0.000 o ,O0 . .110 (.109 0l.J'1 V..1)" 01 .j U, .0 .11 1 0 0 1 4 1 2 4

NOO8MOLIEO 0 110R 0 P01.1 " 0 1' 4

0 . 0 0 0 1 . 0 0 3

0.0 0

1. U , 0 0 .1t0 0 .4

1 0

.0 OI

0 . 0 1 0 . 0 0 0

U. 0 .0

t

00,)' .0 .! .

0 .0 0 0 3.1

2 0 1 0 v 1

0 . 0

0 .0 0 0 0 .000 0. ,1 0 .0 0 0 .u 1 u01,1 -t 0 .

. 06 .0

1 .11t 1 1 2 1 0 1 0 10

0.001 0. 00 0.1112 0. gO0 11. 10" 0.

,0 0.10 0.00 0 0 0 0 . 4. 5 o0

.001 0.002 0.000 0. 00 1 .110 0r7 .01, 11. 79 0.010 0 0 I 3 i . 3 O 1

0 .000 Uo.00U0 J 0 . O ,. Z.O 1 o ..

U00 o-.O1'.1U Q 0 0 4k 1 2U 0

0 .008 0.110 0.1000 0.0 )Q.3i . 000 Il

0.1) 0.C0 ,0 , 0. 0 .,00

0.000 (1 . n .0 v 4 ,)3l 0U. u v . 0.1 l.101 o0.000 0.11119 0.000) 0.'2l 0..0', 4 .ho 01, 11U 33.ll l.13

ir

O .UOO~ ~~ ~~ . L(¢ b.O ' . ti2 to . 'tr' 1, :'uIe. i+ .,.>U.00o0 0 o 0 13 01 1 * Iv) 10.3 J 1().103 1 .• "t5e '

0U0O0 0.000 u.0Uu U.11 to .o00 .. 0'v 0 3.1

N OOLI 3 i)OSIII1 0.11 ~ o °/ '

°U 0o0 U.0

0. 1100 0.0o00 0.0 {, o .oo ,. 139 1.11 l,,) . L'0 0.01,1

o0,o)3 0.007 t1, .,b 0.030 . .02 '. * 1,0 ) (0 0j .101

0 .0 00 0 .003 0.110 0 00 o.O o5 16i . o 3

* 1l ,l10 U

0 .030

0.0(00 0010 0).1100 (I.013 0.030 j 3. li, U o.3 I 1)0

0.00 0"000 U .1100 t0oi| t ,1v I $ , 11 &).1I10 0.034

RUN 2, DEGREE 2

(Note: Degrees 1, 2, 3 are degrees 1, 2, 3 for front seat;

degrees 3, 4, 5 are degrees 1, 2, 3 for center seat.)


KtFACTORS APE.

.015740 0.n64070 0.3148H50 o.785920 0.6j2Q0 0.1?b625 0.022900 0.003500

AMPLITUDE LEVELS ARL SE' AV

0.03 0.05 0.08 0.13 0.l 0.3? U.bu

FRLUJENCY LEVELS AiE SET AT

0.06 0,1? 0.25 0.50 1.u00 2.00 4. 8 .10 16.',.

CEI41ER AMPIIUPES ARE

0.044 0.068 0.106 0.1b It U.257 0.401

CTER FREQU ,INCIES AHE

0. 0 8 0.177 0.354 0.707 1.414 2.r 5; . 3b7 11.314

MAXIbUM POSSI;LF COUNTS PEP SEuIEN1

1.326 2.652 b.303 10.607 21.213 42.+2o 84.853 109.705

ABSURBED POWER M ,'Tk1A1.30961 5.33070t 26.19881 65.3v051 ~i 1'oi i0. 432 1. J053, 0 291210.53973 2.1697 10.797?b e6.9493: dI . ? '4d ( 4.3291 J 0.7'5 2 4 0.12 00?0.22244 0.905 4 4+.44981 .i.,Ob6u A.75:52 1./ 54io 0.32302 0.0,+9 4b0.09167 0.37316 1.43392 4.5773 3.h039 U./3530 0.13337 0.o2OjoU.03778 0.15379 0 . 15H 1. *8 65 1. 062? 0.*30304 0.0 b49Y 0. 008+00U.01557 0.06338 0.31 149 0.7174t 1. 15 . 0.124W9 0.02205 0.0034b

N1OU MALIZEi) ABSOkUo - 'U ,.,ER vI HlIA0.98777 2.01036 4.9t0O'o 6.1 0U 2. 12 8o.3 0.247b9 0.0224 0.001/2v.q0709 0.28?653 2.03b95 2.5b40 i .. t 91 0.1t0204 .009e5 0.000710.16777 0.34 14b 0.3906 1.041.14 0i. ; I2 0.04205 0).003d1 0.0J00290.06914 0.])4013 0.345 61 0.4315o 0.J/U' 9 0.01733 0,00157 0.000120.02850 0.u5oJ 0.14252 G.1/7ob ) . 7u U.1 1'14 .00 0 b 0.u,00050.0117 4 0.0239.: 0.05874 ,.0/33u L.:;; ,82 0.00?9q 0.0002/ , 0.0000?

E-6

AFU. 011110 1 0 0 0 I

o 0 0 o 0 0 0 0 0 11 0 1 u a)0 0 11 11 0 11 u) u. 11 U1 11 L 1

0 V (1 ( 1 11 0 I) 11 u t- 7 3V1 oi to 01 LI I 0 0 0 Q1 I) 11 0

V1 I 0 1 0i II L 5SLOOP. 9. 1 10, S0J.l.,A o 1.20.

SOOP. 2.0116 Su0lll.p- I 0. e3LI d Id PWRA;

-t~I(E AOSE, A(IUOOO( P13.II> 1)09 O Q- v .( .o .

11.000 1.0r11 1.001 11.0010 V . ll I110. V U.11110 0. 11 00.11110 000 0.,1111 0.0111) V 11.12t1a 1.01 Ono .040 3.0l1L

0 :1101 0 1. 010 U o 111, 11.-0111 1..1 "'.01110 1.Li0 0,11L vo 0.000I 1). V100 U 3.10 0 J 0.11 U H J, ) . Oli11 L . V19 3.,0111

20 NO M LILI LOIOO I 00110 . 1 .u )- . .Oi01)O u. f)10 0 ? 0.1)00 .o t ~ l- 1:w I.lOU 1 A, I. .

0.00DC 11.111(1 11.1111 0.1(3o -101 V.0110 0.0011 0.111)0QGo .ou %.ui :'j 1" .(, Ve

0 3 .10 1.004i 11.1100 1011 :.21 1.01 0.000O 1..001U0 0.6 .1i ~ v -u n

0.11 .1111 0310 0.~ (1 U.06 1.13V 0.11 0.0 110.1vU.00

11.11 11.:1 11. 111 U. 1 1 0 ,. l ' 1 , l l " 10 11

)1.) 10

0 0 ) 0 ' 0 1 1 bl'Ono tlvl'

0 2 0 11 3, 11 1 111:cl . ,, - 0

0 a0 .11 1 0o 11 V1 114 0Q 0 no v . 00 0 0 0N114 11 1-. AUI0 L VU it- .40 0 1 0 I

01 000 11 no 0 0 3o 7 ll- 0i 0 ol V 11 0.:Of U11t 0.0113 1 I

Q11 0 0 1,0 0 -00 1). 11u J 01

U . 09 0= 1.311 0.009.AP 1)1.111t111." u"'

0.1100.02 0.0119 311.301 13.'4 -13.000 0.0101.00 11011

0.1 0. ol 0.11( 1110 e.Il 5.1196 1.0110 41100 -

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HUN-?

SEumENr 50a00015 S. SE(. T= B

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2 1 0 0 0 U u 0 0 0 0 U 0 u0 0 0 0 0 1 0 0 00 0000 10 0 0 t u s

0 0 0 U 0 0 U 0 0 1 el

SUMAP. 9.131 .UMNAP,= 1.7?2 0 U . 0 U 47

SUMAP. 0.598 5U1I0 .0bd0.

AtiSORBED PowE0 AFD

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7( IoIMiO. I 0.012 0.000 0.1100 Uo.000 1.v 0 Vo (. oO 0.1l)I

RUN=2

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SEGMENT= 6

AFu ojPuT0 0 0 0 0 0 0 00 0 .3 0 0 0 0 0

2 0 0 0 0 0 0 14

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NORMALIZE,) AIISsR11..) PUo.L AFj0.00 0 .00 v.100 0.900 .000 .,. 0 v. U0 .000U.000 0.090 0.000 U.000 0.* ' , 0 .uJl U. 01 OU0.000 0.000 V.0 .0 0..)0 n*.,in) J .J1 . 10U*U.69 0.0U00 .0.000 U.000 , . v 0) 0 U0' 0 . U .Ou0 0000 0.116 0.1.3 0.000 .000 3Uu.000 0.000 0.000ouV.021 0.,00 ".1u' 0.uJ '.,si ,, .1,0 1.0 v.01u0 U 0, 19

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UN 2. 0 1 2 0 0 e 0 b3

DEGRFre SIIMAP. 4. 51r(,I= 1014,

SkOMtNl . 7AB800k1)U PUwE AFo)

0 0 ,t U U .1 1 .000 4.3 4 0.000 0.000 0.0 1.001 0.000 0. 00C

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0 1 1 2 0 1 ) 19 AFU 1000,00 0 0 0 0 0 0

0,A0 ;*360 SUM4N,.Ps 1.IJl 0 1 0 It 0 0 U C0 1 0 0 u 0 o 0

AHSO)ED POwE0 A0) 2 2 U 0 U v v /

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U0.000 0.On0 (.000 0.000 U . . 1' l'*0'l I 0.000 0.000 2 0. 0 u 0 0 11

0.22? 0.905 U.o00 .n00 0." 0 U0L00 . i 0 ('.00U

0.002 0.373 0.000 0.000 L 0.l 0 .,U 0.000 0.000 SUMAP 5.912 SUMNAV* t.9d6

v.03 0.000 0. fbo 0.000 0.010 .;.33 00oS5 o.1( I o

0.000 0.o;;3 0.311 b.Sbs 1)00 5.3)0 1.136 0.066 AtSORBE3 P,)-r AFOI0.000 0.6"0 0.0U0 Q.Uou U.1).) (.00. J.,U .011

1O01MALIZEI) ASOEL PowER AFU U.000 2.197 0.000 . U.0 1 ..V00 0.000 0. 'j

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U. 106 o.341 0.000 0.000 ,.'j Q di j 1,0 0.0n0 0.0,10 U.030 0.134 1.S10 U.00 a'.0' J(3.030 0.000 0.0U6U.0b9 0.141 v. 0)0 U.oUu -. V, ".0 ''0 U. 000 0.0)0 0.031 U.000 0.100 0. 0 .(") it,) J . 000 U.K3 . i

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11 NUM14FW ?4 0.000 0.000 0.000 0.1m) 0. I7' 0.401) 0.00n 0.0000.000 0o.09 0.000 0 .() U.,0Q 0.010 0.000 0.000

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0.003 0.000 0.000 0.oU0 .~ .,.000, 0.000 0.00AFU OUIPUT

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AFO oUTPUl SEGMENI-160 0 0 0 0 0 00 0 0 0 0 0 0 1 AFU uUIPUI

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1 0 0 1 U 1 0 1Ub 0 1 I U 0 0 0 h

0 0 0v u . 61 0 3 0 0 0 0 0 43o 2 0 0 U 0 1 10 2 0 0 0 0 0 U 56

I o 0 U 0 3d

SUMAP0 4.406 SUMNAIN 0.1U 1 0 0 1 0 1 35

4A0SUR000 POWER AFO SMAP= 5 .b09 SUk.N.P 10.o7(

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0.183 0.000 0.300 9.1 1 .. l .0 00 0.000U 1.l.d

0.030 0.154 1.512 0.000 . 0.000 0.000 0. V .Jl

0.Ol6 0.000 0.311 0.71 0.00o, 0.12 5 0.000 0. 1ei1

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NORMALIZED AbSOREO P0OwEN AFU 0.012 0.000 0.059 0.013 U. O 3.;J03 0.000 0.0L1U.000 0.000 0.000 0.000 1.0v1 0.000 u.00on0 0.000 .. -

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RUN=.2 UN-nEOREE=2 DEGk F.

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AFU OUIPl11 AFO OUIPUT

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0 0 0 0 0 ' 0 49 1 u l .1 2 31 0 G 0 0 0 1' 1 2 1 2 j1 0 0 0 30 V0 1 ) 0 I 1

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SUMAP 8.9eb So1mr.aP 1.1.'9 Sl 0"." 3.326 btUWN"P. e1. 3h7

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0.092 0.746 3.668 4.51t 7. 13 J.'ll. 0.bh0 0.110.038 (1.00O0 1, I . ,1;, 12 1.4 ). ('011 p,. (,nh () .Oq oc,) .4, 70.016 0.063 10.311 0. tO ;1.1,1:; L. Io 0.0,Uh U 0.61.

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SUMA 60.443 .. ...P.---... .... - -

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K FACTORS YE

0.015740 0.Oh4070 O .3. , '..-, , w,' 9,I-. C 0.0229n (U03 uO

AMPLITUDE LFVELS m-WE St T AT

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M4AIMUM POSSWIt.E COUNTS PtW bn i,.I T

1.326 .652 5o.3 3 u.0,) 21.213 .4+o20 -. b3 1 jb9,705

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___________-___---__ DEGREE-2

SE(,4ENT 10 SEGMENT.12

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0 00 U.0 0.. . .. 0Q..

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s. 0P, . o 0.2- vie

A SI-BED POVE- AFu

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G t E k' P I. I L S : '

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0 r) 8 0.1.77 3 , -+ I.7u 1[ 16 2 , _ 11.314

IVA U]. M '.S S LE Cu r S A- IM SL P'.'1 I

1.3?b 2'652 5 3. 1u, . -1 o.3 9t. 4?O 8'.ob3 1097 0 4o

U 0066? 0.(,27 4- 0.1 02 0. t>:. r o<:t L0 1 9 0 1 . 4J+ . 3+

..3 o :. Z- J, U'?ljsP F i)U ) ,r b{ ,Ar iI AI

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U.00,Ub U.t0. 3 U;ll1 l .o, t) .+ (I21]'9 0.14'+J5 D.;360d

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0 0 021 .'042 7 * . 0

U 00",871- u c 1 7f- (.L I .. , . j k ,l eav Cus ..2' . 10.U036 0o0;.Y& U 0l Ish 0 (; 1 '87' 071l od .01 U 0 ;j

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E-62

HUN.7. ........ ; "-----" --- RUN- E E

SEGMENT I SEGMENT- 3

AFU OUTCPf' 0 UT0- 0 T00 0 0 0 0 .0 0 0 0 0 0 0 0 0 0 0

0~ C 0 0 .0 0 0 ~-0 0 0 0 0 0 2 0 0 0 u 0 1 7

o _ 0 .0 0 II 0 0 1 1 6 1,)0 2 44 0 2 0 4 4.. .. . 4+

SUMAP 2913 . SUMNAP. 0.002 . _SUMAP 11. 4 SUIMNAP 0.129.

ABSORBIED POWEF . ABSORBED ROWER AFD0.000 . AnO0 0.00 0.000 0.000 0.000 0. 0.000 0.0AF0 0.000 .0.00.000 0*• 0 0.o 0.000

O.000 0.000 .00O 0.000 - 0.0 T.O . 0o 0.000 0.000 .0000 0.000 0.000 0.000 0.00 o.000 o.000 0.0000.000 0.000 0.000 0.000 - 0.000 0.000 0.000 0.00 0.000 0.005 0.000 0.000 0.000 0.000 0.085.

. 0 .00.0 00 0.. 000 0.00o 0.000 V o 0oo o oo- o.oo O.o o.J . 0.0 0..00. o00o .00 0.000. 0.000 .0 0.000 0. 00 o 0.00000 0.010 0.00 0.Ono 0.000 0..

0.000 0.000 0.000. 0.000 0.000 Q.000 0.000 . 000 0 0.000 0.003 0.01 0 0.144 ).19 2 10,2 2. bl1.37 0.000 0.000 0.000 0.011 0.097 0.441 1.444 1.Ira

NORNAL!ZED ASORiE PO EA A70.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000

0. 0 00 0.000 o T oo o .;5-000 -0000.000 00 0N(OoMAIECAHONI 0.000 0.0 .00 000 .uo 00 0.0000.0 0.0 oo 0.0 000 0.0 0000.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0 .000 0.000 0 .0 0 0.000- 0.000 0.000 0oo ,0.TO0.0 _9"0. 0-.000 0.00 0.000 .oo0? _o.oo o0oo . ., n o0n0 0.0 09.003 __

. o 0.oo o0. u u.,Cuo 0.000 0 0.090 0.000 0.000nu 0.001 0.000 O 0.000 D.no 0o. 000 0. 00 ) 0,0)0 0.00V0.000 0.0)o0 0.00 C 0.000 OUUO u 1.00 0.000O 0.00 . 0.000 0.000 0.00ol 0.001 0.07 0.0u0o 0.021 0.0140.00 0.000 0.00 0. 400 O.O O , O.OO . .000 0.0O 0 .00 _ _ 0.01 O*I 0 0. L ". 0. .1 . 0.019. . .

HUN-

SEGMtNT= 4HUN.?

SEGHE.E=I AFU OUTPUT. . EGMN 0 0 0 U 0 0 0 .00E,~ I _ _ _ _ ~ ~~~~.~ ~ ~ ~~~~_ _ _ 0 .... 0 .... 0u. .. . . .. . O..........

AFU OUTPUI 0 1 o _0 0 )

.0~~~ 0..00 00 ) -

. 0 00 v 0 .... ...... _ 0 .-- I- I u 0 0 0 0 00 0 0 0 1 C C_ 0 0 0 0 --- -- 0-0

0 ) C ) 00 0 --- ---- o 0 0 0. 0 110 0 3 0 0 0 0 00 0 0 0 3 0 0 3 ' SUMAP. 0.406 SUMAP 0 0005C 0 0 0 1 3 0 2 3b I -- UCOrPC.HF

. . . ... Z . I USS u WHE D P O W E R A F O" o- o 0 )'. 2.00 OUCNo P. C.uo *'.1 0.000 0.000 m0.000 0o.00 0.000 0.000 0.000 .. 0o

0 o -- 00 0...00 --- 0.000 0 0000 0.000 0o, O 0.000 000

0000.0000.000 0.000 0.000 0.000 0 0 06o_ n _o A o ____,HoSo~ p 9 _ u ~ __ _ _ 00 0 6F 0,I) D O O 0.000 c, 0 o. 0 0.000 0,U. . . . ... .. . . . .. . .. . . . . .. . .. . . . ... . . . . .. ..

0.000 00.000 0.000 0.000 0.010 0.000 0.000 0.-

NORMeALIZED AU SnRtEU PO*EF{ AFU

9.000 0.oo o .coo 9.co o.c o uu, .,o o. ou.0 - o.ooo U.noo o.ooo o.oo o.00o 0.coo o.ono o.0000.000 0.000 0.000 0.000 0.000 0.00 0.000 O.00 0.000 0.000 0.000 .000 O. O- - --- ---.-000 0.000 ... 0-

0.000 0.000 0 .0 0000 0 000 0000 .00 0.00 .0.. .00 0 00 0 0000:.0.000 0.000 0 .. 0.000 00 0.)) 0.000 0.000 Oo.

C)_o 000 -. _ po9oo _co .. 00. 0 0 0 * 1 c1 - . 0 j!)00 0.000 0 .000 0.0000 4 0.00U17 c.000 0.Qn9 O.099

.0.000 0.000 0.000 0.000 .000 0C006 03 00 0.0200NORMALIZED At!Sn00E U P .Ek AFt

. o~ooo 0... .o000o 0.000 ..00-- 0.000 0-00.0-0--.00.o0.00. .00 0.000 0.0-00.000 0.000 0.000 0.000 0.000 0.O0o0 OOO 0.000

0.000 0.000 0.0.o 0..00'o 0.0000.oo0 . 0.00000.Cu 0 Jo0o 0-0uo

0.00 . 0 0 0 0.000 0 0000Co 0.0 0.0000-000 __ 000000 0.000 Q.000 0.0000 0.000 0.00 0.000 0.-0

0.000 0.000 0.000 O .0)00 0.00" 0.000 0.000 0.0oQ

0.000 0.00.0 0.000 0.000 0.03000 0.000 0000.000 0.000 0.00 0.000 -0.00 UCQ.C~0 .0.0o00.to0.000 0.000 0.000 U.000 -U.000 '.0 .0 .0

HUN?7 RUN-7?....... OE I- - - .o-,- -- - EG'Fr.1 _o I

1 0 0 0 0 001 .. S G 1.T .....

UAF O UTPUT . . . . . .. . ." - All.)OUTPUT 1 I

0 0 _0 1 _0 I 0 0 0 0 0 0 0 1 2 1 3 1 .

I . 0 0 0 0 U 0 0 0 0 0 0? "2 4 33. .. . . .

0 0 1 1 2 1 3 40 0 0 1 2 1 4 10 49o o . 1__ _3 4. 4 0 0 0 1 ...... 4 . 15 .4 .. .... . ..36.

StJMAPs 11.00F SUMNAP. 0.143 SURMAP. 72.506 SUMNP a 1.165

A-vtI OeO 'E) POw R AFO -..- AbSURE O POWER AF0 . .- - ------ - - - --- - ---0 0 0.. . ..00.000 0.000 0.110 0.000 0.000 000 0.000 0.001 0.000 0.000 0.000 0.4609 0.000 10. 109 1 I.143 3.034

0.0 0.. -O- 0. - - - .n 0.000 0.011 0.091 0.193 Z.531 4. L 56_50o S1. 5l 1_0___ .000 0.00 o 0.00 ._ . 00 0 0.0.0 n0. 0000 00 000.0,. 0.000 000o0._._4 1 205.)00 7.0?0...0.000 00o5 0.000 0.000 O03 O.000 0.000 0.000 .340 3.43 ..0o3 3.09

0.u00 0.000 0.0o . 0.0(o 0.000 O.Ouo 0.0n0 1.b99 0.000o o.oo 0.o00 0.oOo 9.000 .'.), 3.400 7.00,S0.o0o 0.0.n 0.003 .0.014 U. 11 0.29e 1'051 3.5102 0.000 0.000 0.003 0.o.7 I.05Y 1.101 3.503 4.'Cl0.000o 0.002 0 .000 0.000 0. 3 9I) -_.01 . 0 .... .o 0 .. o..0 oo 0 .00. .0 .po 2.1 . o , ...

N ORMALIZED aHSnOFV PO'E R AFO -".0.000 0.000 0.020 0.000 0.00 0. 9) 0.000 0.000 "0.000 0.004 0.000 0.000 0.000) 0.000 0.000 0.000

____-.0o __0.002 .0.00 o.o00 0.016 )1.voo _.Ooo .000

0.000 0.000 0.001 0.001 0.006 0.007 0.012 0.0210.000 0.000 u.00 o 0. 0o.0I0 o. 0r,0 ......

S0.000 0.000 0.0 0.00I 0.003 0_ . O 0.0. 0.009

NOMALIZED ABSOROUEO POEH AF)0UN__ . .... 000 0.0110 0.000 0.044 0..00 0.216 0.143 0.01

-____U' G0 -~-_RN7-,-O-- 0-00 )4 -. 0i7 0.06I 0.119 0.090 0.059 * 0.00DEGREE - - --- - -- 6- - - -V

SEGMEtJ 6 0.000 0.002 0.000 0.000 )0.0b16 0. 01 0.0?4 0.010.900 __._0.000 6-. ..OU 00 0* -0_0_ - 000.033-0 00 -0.04. _

OFu OUTPUT 0.000 0.010 0.01 0.1OJ .663 0.017 0.041 J.025

0 0 0 0 0 0 0. 0 0.000 0.000 0.000 0.001 0.005 0.0'J 0.026 0.00V. ... 0. . 0 . 0 ----- 0-. -. ' . .... ... .....

0 0 0 0 0 0 0 HUN=70 0 0 0 0 0 0 0 ) II IU , 0 0 0 0 0 0 2 .. SFENT* .

. . . 0 , 0 0 0 0 v u 3 F N H

II AFU OUTPUT .0 0__)00 ._ 0 3.... ... - .

S-MAP- 0.283 SkMNAPQ.002

0.000 0. 0.0.000 0.000 0.000 0 0 0 0 0 0 0 0A850RHEO) POWtR AFO1 . . 0 0 0 0 0 0 u 0

0.000 0.000 0.000 0.000 0.000 0000 .0 0.0 00 0 0 0 2 J 2 6-- 0 0.000 0.000 0.1)00 ._ 0.000 (. :00 0.0o0 _ 0.000 . . . . ..

0.000 U .)00 0.000 0.00 0.o.,0 0*o 0.00p0 0.10b SIJ.AP= 2.oSl SUMNA'. 0.0070.000 0.000 .0 0.0 0 .U 0 .000 0.00 0 0. .n 10

NORMALI.EO ABSOR13E6 POWER 0.000F P A) 0.000 0.010 .0 ).Oo0 0.0on 0.0000.000 0.000 0.0000 0. 0.000 0. 000 0. 00 V.000 00 0.0 0 . v.0. 1 0.0 )00. 0.000 0.0000.000 0.000 0 00 .000. 00 0.00 o. 000 .000000 0.0 0.000 0.000 U.I 0.0, C0., 0.000 0 *. 00

0. 0 0O no0 0.- u 0 .i t-.) t . ( 00 0 0.(.o If.000 0.0n0 0.00v V. 0 0 0 0.0oo 0.000 0.0000.000 0.00 0.000 0.00 .01 10 0.00 0.0 0.000 0.00 0.000 0.000 0.0.0 0.1*00 0.000 0.000

000 0 0 0 00.000 0.000 0.000 0 0 - . 0.000 0.000 0 . 00 11I 0 0 1U 0. 30 0 0.4 .'0.000 0.000 000 0.1100 0'0r00 .I00 _ _0.100 ... 0.00.1 0 1.000 0.0)10 "0.0O0O 0.0)10 .040.U +---0.301 '--.04 . .39 ..00000 0.000 0.000 0.00 0.000 0.000 0.000 0.001.u .4 .0 . 0.

- 0.000 .0,10 .30 .0t0 . .0)0 000l 0 .060 . -0.000 0.000 0.000 . Oo 0.0 00 '.000 0.000 0.0.1)

0.000 -.. 0.00 0.•0 0 0.010 o.0 .') u __0. 0 - .0 0.o

0.000 0.000 0.000 0.00 0.000 0.000 0.004 0.000 3

0.000 0.000 0.000 0.000 0.002 0.008 0.003 0.006

N -? RUN.? -

........ -....-R- -E- -1 .... DEGRE-bE-l1

SUM041 9 SEbOm4Ol.! I

AFO OUroUT AF TUiTPUT0 0 0 0 0 0 0 '0 0 0 0 0 0 0 0

0 0 0 0 0 0 0 0 -__ __

S0 0 0 0 0 0 00

0 0 0 0 0 0 0 044 ! 0 0 0 V 0 0 O " O O O O ______ ____Oq . 0 O o 0 0 0 0 0 0 0L 0 0 0 0 Lo 6 25 0 0 0 0 0 11 0 o 0 ,. • 6l 35 ...... ...... 01 0 ......_o...0 ;t

° "o ..... j

0 0 1 0 2 4 10 35 _u_____ -

SUMAP. 16.063 SUMAAP. 0.14d SUMAP.= .557 SUlN P4. 4.4,06

_.A~oSH ooEDe.W AF-............. 0.000 .01 0.000 0.000 __ 'o OR 0.9400.000 0.000 0.000 0,300 0,.000 0.000 0.000 0.00 0.0 0 0.000 0.000 .oU 00, 00 0000.000 . 000 0.000 0.0 0 0.00 C*000 00 .1 .000 0.0 0.00 0. o.0 0.0,0 0.000 0.0000U. 00 V0 0,0n$ 0 I _ _ o .UO 9. D00 _ .0J0c 4.1( O 2 3_

. _ __! .0 000 O.Dn Q3f .UUv Oo v)u 0o 0.009u 0.I10 0.000

0.000 0.O o o 0. 00u 0.000 0.58 2.1 4. 0.000 .c o o. 0.Q 00 u. o 0.0 J 00 ".Oo - o0.0 .

I 10.000 U000 0.00. 0.00 0.0I9 . 1 .,_ 3

.000 0.000 oo 0 .000 0.0073 0,00 0.0,0 0.397___ 0. _ 0.000 0:006 0:000 0.oOO 0.000 2:404 0.000 0.000 0.000 0.1.00 0~0o 0.00 o.ooo 0.000

0~o .0 .004 _.0 .0 .00 000 0 0.049.''"4.'.'.o 0.o0 *n 4.00 0.,0 ____ 00 0.04o-1NO0HMAL IZ E dSUktIrU'k PbWER APU. I NOHMALIZEO-AHSOl,'IdI -.PO,,E-4AFI) __L

.00 .0 0 0 .000 0.0000 00 0.000_ 0.00 0 ........ *0.000 0.000 0 0.000 0000 .073 0 0.000 0.0000_U0. 00,0 4j4U09 QJloo v U0 . ,) )

0 .U (10 0.0u

0.000 0.000 0.000 0.000* 0.00 0.0U0 0.00 0.013 0.000. 0.o0 0.001

. ,60 . 000 0*00 0*000 6.001

0.000 U00 00 0.004 0.0'402 0.0110 0.007 u.007 0.000 0.0000 0.00 00.0 0.003 O.000 0.Ono 0.002

RiUN*7FOT f RUIN-7

SE~tfaoSE LiME 14T -12

AFU UUIPUT AFU uUTPUT

0.00 .. .06 .000 0.. U ,_....00 0 UY. . 000-_ .... -0.0 .... 0*.00 0.00. '-. . O.000o- 0.0€0 .00') 0.,O0 - 0,400 ... 00,4h f0 '0 _0 0.0.0...........

.00 .O 0.0 0.00 0o 011 0017. 007 ..... 0 .... 0 0. 0 .0 0 0 003 000 0 0 0.002

Q . U N - O _ -- - 9 _. .... . . ........ ..... ...... ...._ _ . 0 . .0 _

1 0 0 . 29 _5 I00 -10 .20l -090* 0. 0 0 0 0 1

Sk)MAP. 11.411 SUJMNAP- 0.11,2 SUmAP- .J40 .,S~UMNAV -

Ad50RBED POWEP AF0 AHSumoFf P%.fR AFn

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.0 0 0. . . 4 2I0 0 10 05 1.14 0 o 0.000 oo . A0 -, 0 0*d

400 0 0 6 . . 0 o2 3 1 0 9t) .10 I .J13 0 00o 0.000 0 0 0.44 o 0t40 Q

0 0 0 U . O 054.,4400.p iI111 1J'No44g 0,. "' I 54.. .... S .'.P ..1.J.q _____..SUMN0I oy.Q10 .. ...... .. .. . .

U5.000 0.000 0. 0 0.011 0 49 0.6 1 1.444 1.04A00U00) o 0 000 0.0 .144 .

NTi;I4MAL_1ZEDi -AHORttB f'wtli'k AFUNOWMALIZED A8SOP Eb WowEN AFbU_

0.000 0.0o0 0.000 .O ).on0 *000 0.On 0.000 0 0.000 0.01 4 .000 0.0 r 0. 0 V U0 V 0.000 .OO

- 0- o -_ n __U_ C 00 0 .U. 0-0 U 0 10 0 0 _ onn : -

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0.000 0.0440 0.04444 0.014 '.03, 7I, :.00 0.11 43 G,00 0.00 0.000 0.40 0.00 44.440 0.0(0 0.000 0..003

0.00 u0o Uo 0)O,4 0a.1411 44.(49 0.4.T1 1,401 l.0l] : ' 0.000 0.nU 0.000 U.4400 .4,. 44.44, 0.Ugo 0.s4

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. 0.000 0.000 0.000 0.000 0.00 0.000 0.0000 000 0000 00 10 . .0 00 .

_ _ 900o0, o10 0.000 U.o00 U(.V4)00.0Q4 0 240-o00 0.003 __

0.0.000_0.060 0.00 0.44440 0.,400 044044 4.000 0.00.

0000 0.00 0.000 0.000 0.014 00.40414 0010 0.

00000 0.000 0.000 0.001 U .11 ..021 0.008 0.000.0

0.000 0.0

0.00I0 0.000 0.0440 0.000 0.400 0.000 0.O000 0.0000.0o_ 0 o n_ 9.00O0 o _ . 40...u .S. 0 -(4 .2.2 ---04.0 o 0...e._. , 04 ? 0 ....... O 0 .. ..O000 0. 61(0 0.000 0.000 0.O14* 0.04, 0.010 C.OO00.000 0,000 0.000 0.001 0,011 0 ~ .0 0.000 0.0000.000 _ .- , n . ..0000 .JfL_-- .) -- , 1q .. .@ (l__ _i. - - - "

DE , F . .---- --- - -1.- - .. I -

I SEGMENT=15

OU'.7. *'- *-- --- -- .A ------- *- FUi OufPU I'UN7 0 0 0 0 0 00... .; - EGUEET0 - 0 0 0 0 0 0 0SEGMLNI- 1 . . . . . . . . . . . .. ..3 0 "u-' . . 6.. . . . . . . . . .

0 0 0 0 0AFU OUTPUT 0 U 0 = = 0 tI! 7o -~ f _______...__-_.....__.. .- o -% ...3 -. . .! 0 0

SUMAP. 4.064 SUMNAP= VU3

ABSOROED POEP AFD

0.000 0.00 0.000 0.00 0.000 '.000 .o000 U_.01

0.000 0.000 0.000 0.000 0.000 0.000 (1.000 0.o000000 0.000 0.000 0.00 0.000 0.000 0.000 U.,00u.0 000 .0 00- 0.0 0000 0. 000 0 .059 011 9 _0.000 _ 0. 12

0 1 1 0 0 0 0 0 0.000 0.000 0.000 0.006 0.146 V9 10n 0.86000 1.00 20.000 0.000 0.000 0.000 0.146 O,.0n0 0.800 1.000

0 1 0 ! 21 0 0 3 L D S _0 1 .31 N___LI__- 3~kiE- OE

0 0 1 1 3 1 4 75 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000

S J-AP. . 0.018 SUMNA- U.128

ABS00 EO P1ERE AFP- __U.000 0.000 V. .4t U.o o 0C0 T 0o i 000.000 0.0100 0.04 0.000 0.000 0.01,0 0 n.0 0 0.000.000 0.005 .9.019 0.000 0.000 0.000 - .0.000 - 0.000 -0.000 0.002 0.000 0.033 0.1. t 0.00 0.000O 0.03?0.000 U. 000 0.000 0. 00 .11d V.010 0.350 2.114 0.000 0.000 0.0000 0 .000 . Q.On Q.00 0 0.000 0.0000.Oo_ _ 0.000 0.001 0.006 0.013 0.120 0.578 0.106 0.000 0.000 0.000 0.000. 11 .00 .000 9 ...

0.000 0.000 0.00o 0.000 0.0V0 0.00 0.000 0.001NORMALIZED ABSORBED POWER AFU 0.000 0.000 U.00 0.000 0.003 0.007 0.000 0.000. 0 0.000 O.0n _ 0.000 - 0." 04_ , 0.001 - 0.A00 0.000 0.0 0.007 l.7l .0

"0LOO,00 -

0 .0 00 o .n n n 0 .0 0_ 0 .0 .)0 .0 ). . . 0 r 0.0 0 .0n U .*- - -. . -OU . ......0.000 0.00? 0.004 0.000 U.000 0.00 p 0.0,U 0.000 RUN7 .0.000 0.0fil 0".000 0.003 0.007 0.000 0.000 -0,.O _DEGREE "0.000 0.00(0 o.oo O .ao o0o 0 (Oc 0.004 0.016 . S OLNI .. --0.000 0.000 0.000 0.001 0.003 .0.003 .007 0.0 V6

, o ~o " .- s""6 o o o no.. . . ..- . ---- 0113001,0

S 0 0o 0 6 0I 0 0

0G 0 O 0 0 0

AFD OUIPUT S11MAP= 3.693 SUMNAP= 0.0i'

0 0 k I - 2 u AUSURbED PO E AF ..0 1 0 0 Q I 1 0 0.000 .no0 0.000 0.0)0 0.000 0.0r0 0.0n0 0.040

IU . 0 , 06000 0.00 0.00 0 " 0 0 1. 0.00 0.0100 0 1I 0.000 0.n0 0.000 V.000 0.000 0.01o0 O.unO 1. lj

U. . 0 0, ---_ 00A 0 0 one U 0 U. 0 Q 0 .I ,) 0 U 0 IJ i I

SUIiAP 40,Jb bUMNA,. .t i 0.000 0.00 0.vu 0.11 0.u 0.000 . 0.07 o

AS BS H ( POWEP AFO NO MALIZED AHSORHME P(),EM AF)0.000 0.000 0.000 0.469 2.(4 7 0.0 0 2.143 3.03 0.000 0.000 U.0 t 0.Un 11 .900 .0).0 0.000 0o010

0.000 0.00 0.091 01193 1.687 b333 oo 00 .uI 0.000 0.000 0.000 0.000 0.000 0.00v 0.000 0.,000.000 0.05 0.0 0 .00 0 2. 0 0 0.I 20063 00 .00 . 0.000 0r) t.0 vU. 000 VO . ,00V V. 00 0.,0U .00 0 0.0 " U0.001 ,33 v 00 * Q 123 1.7nU ).215 .000 0.n .000 0.00 0. 01 0.00i) 0 .0 U.000 , * ,01l0.000 0.00 0 0.000 0.01 2.051

; C 0 2 2.41l 0.175 3 3 3 0.000 n0.0 0 .UOU 0.000 .000 , 000 0.000 0.(0

U.000 0.0r, 0 0.0v1 0.0(0 ,1,97 .12 1 . 00 0.019. 0.000 0,00 0000 .000 . 01 00 V (00 0.00 7 0o 9

NOkMALIZE0 A6SOPOED POwEk iFU I i ...70.000 0.000 0.000 U 4 U.u00 4 .0 u _0.143 _0.0 -- - . .1 .. -..0.000 0.000 U.U 0 .0- 0.03 0 . , 0.1 .000 00.00 .. 0 SE1M.N0e700.000 0.002 0.000 0.01V 0.00n -. 040 n.U41 0. 0 0 0 0.000

0.000 0. 11 00 .lui0t

0.11013 . 112.0 0.000 0.00 _ 00 0 . .. 000 -. F UT T.0.000 0.000 0 0.00 0.1G, 1 0.003 0.n007 0.017 0.001 0 0 0 0 0 0 0 00.000 0.000 0.0 0.070 0.001 0.1.00 0.000_ 0.1003 00'L07

0.00 .0 . - ._1 .90L- - -..0o .V .. 0 o 5 .... . . 0 u . 0 0 . . .

0.00 0.00 0.00 .00 000 0.01 0.11 0.00-0 -.0 0)01311300 1 .0-----0 -.00-.

0 00 0 0 0 0 0 0

0.00 . 111 - 11000 .010 9~U0~~173.01 _0.o, _0 -0 0 0 -.0 S .00 .0 0 G** 000 **6

0,_ 0 Q0 0 U 0 1 0 271 0 0 0 1 5 1 5 J4-0 6 6- , - -- 6 4

SUMA.= 16.0 __ SUMNAP_ U. .4

0.000 0.000 0.0110 0.000U 0.000 0 .11O 0.00 0.000

I 0U.001 0.000 0.000 0.000 o3430 o, 0 0.000 0.oL.b0. 00)0 0.000 0 .000 __ 0.00__ 0.000 - 0.1t,0.. 0.000 -.46. _ _.0.000 0.01100 010 I U 07'. 3. 1? '. /112 1.000 ?.V0

0.000 0.tfO1 0 0. out) 0 .1).140 ./;1 2.30 0 1.040I~ MA 5301I 2EIOOOIO0 P1,,-,71-l FI

0.000 0.000 0. 0 0.001 0.000 0.00 0.001 ).0010 .1 Qt 07 0 0 13

0+00 000 0£00 {t.)0 ,.0t o.0l1 0.000. 0.006

0.00 O.O~O o00 . 01 'So0I _ 0. 1 0 001 0.010,

RUN 7, DEGREE 2




K FACIORS aR E

I 015 7+o 0.064070 O.314 iJ. .. (5"? 0 ,, .t'4 , a ,.12u250 0o022900 0.003Lu0o

I.LI IUDE LEVELS t\-E SFI AF

0.03 0.05 0. 0 13 ..C1 :.32 0o3 o

IQUELNCY. EvLLS fHE SFT iT

0.V6 0o12 0.25 ". I. 0 Z..' " .. 0 10. C

IEN; E AM PL I IUE S AR

I. . 0 06 . 0 bDo i 5 0 57 "

C I E F< EQOE-.IR I S AHN

.088 0. 177 -o354 0.970 1..14 c , t' 8.o 57 1 4.31,

MvAAIMUM!P POSS 'ILE CU)UN1S Fta, br.,i tT

I 1.326 2.652 5.30)3 10.6') 21.2103 4 1 5 105

I bSORBE) PO,' Mh;T('IA30961 5.33u73 26.1 ( 1 h 53t 35 1 I . 532 L.)3 0.292

. 53973 2. 19697 10.79720 ,., : -32,.7 +.32913 .) 7?524 U . ?00?Z'.2?44 0.044 4.44,7 1 1. ' 4 4 I o I I D2 1 1 4i 0 .323b;? Q. U49)4I 091 1.37316 1. 339 2 +. A 3 .634 . /3530 .133 I . D'i03

10 3 17 0.15379 0. 5 i I.8,. 1." ,b ( 0.1 103 . 3. 05. 6 0 4 3 40

0.01557 0..h633-36 0.311, .7i "4, .51 5-4 A.12,c9 0.022_j 0.00346

10U <4LIZEDf AdS 3E-) P "eF 0 -ikR.i A

.9.777 2 1: 3) 4. . 4 ?.', ,J . 4' b9 0. d, :+?o 00 172L.+ 0709 . 2 5 o 3 9 5 .u.- ,. 91 ) .1 204 0. W. t5 0o .u 71i

0.1 b777 0. 4 o.3 1o t o .3 .'41"51 ,. ,04205 .00 1 0 .* k)C 9S* 06. 1 4 t. 14 73 .3t 5 i . I o . 7 0 , 01 i 3 G 4 A.' 3. U o I '. 2

0.02850 7. 5.5 0. 1 42c U.7 / . ' 0.00 14 Uoc0b U.101I50.0117+ C.I ?39. . .... / . . V 0 . 9 4 0I,.:c7 VU C 0

E-67

.. .. . ... . 2U ,2f .. .... . . . . .. .... .... .... .. ..SRUN?7 * EGREF2

0 00(0 0 0 0(0 001 233_

OEGIFE=, . .. ... . .... SFGMENT-_3

... SEGMENT-. I ... . ... . . . ......AFU OUTPUT

AFU pUIPUT 0 . 0 _- 0. O 0. .00 0 00 0 0 00 0 0_ 0 0 0 0 0 0 0- 0

0 0 0 0 .o 0 .. . .. 0 v. C . 1 0 0 It 0 0 3.0 0 (. 0 0 _ 0 0 01 0 0 0 0 0. 0 023 . . ... 0 0. 0 _ _._ .__ . ___ _ _0 0 00 0 0 0 0 0 040 0 0 0 0 0 0 0 oo 0 1 1 0 0 0 0 660 0 0 0 0 0 (1 60

ABSO RHE SPOWER A 3 FA k.A LSOPHE POWE'R AF2.-- 0.000 0.000 0.000 0.000 0.000 0.000 -- 0.0 0.DOU

0 .C000o 0.0(0o 0.000 0.n,. 0 . ..0 0. 0 (,no , . .. 00 0.0oo 0.00000 0.000 0.000 .0.000 . 0.000uo 0.0o000.0n0 0.nn000 0.uo 0. o O.( o .0 0.0o00 0.00 0.0 0.000 0..ooo 0.000 000 0.000 . 000.. 0 .000 0. 0 . .0. 0.

0 000.000 0.000 0.000 0.020 0.0(2 0 0.0(20 0.000 o __ _0.009 0.9000 0.000 0,000 0.003 0.2220 0.000 - . 0 '.

(.1.00 0 0 P00 _ .200 . ) .0- .20 A L .22.. .0U0 o . ,h0 0.092 0.2120 (.UOU O.00 2.2(00 0.L'00 Q. 9ili0.09 0.000 0.000 U.000 0.00_ 0.00 0 0. 0 .000 0.000 0.000 0.000 0.000 0.000 0 0 0.00 0 0.0 .0t200.000 0.000 0.000 0.000 0.000 0.000 0.000 0.1od .00 0 .003 _ 0.311 0.00nu0 0.000 0000 0.000 0.0'0 ._. .U0.000o . - 0.)(0 .00 __0.00 ,00.0 0.000 0.000 0.000 0.20d NOIM.L.Z0 00020 POE AU

.......AF 0 0o o 0 0,00 0 0.000 OW_ AUN0 0 0010702 2S2 'UP.1 .0 0.00 0.000 ___ 0.000 0 0 .00 0 .. 0.000 . 0.00 0 ____0.00. 0.00 _ .. . 0.00 0.0O . _0 .000 0.00 .00 0.(0 0.00U 0.000 U.000 0.2 U 0.000" 0.0U00. 0 0000 0. 000 0. 0.00 0.000 0.000 0.0O0 0.000 0.000 0.341 0.000 .000 . . .00 0.00 1. 0.00 *n *0.000 0.000 0.00 . .000 0.00 0.(00 0.000 0..00 . .0 9 - . o 0000, 0.000_ o .0 .00 2.0p00 0.000 0.0039.06 0.0o _. 0.000 ___ o.00 0.0 0 o .. 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 000 . 0 0.000 0.0000.000 0.000 0.000 0U.10 .. 020 0.00 0.1100 0 .12 0.000 0.024 0.009 0.000 0.000 0.000 0.000 0.0c,0.000 0.000 U .,000 Q0.000.000 .(fo0 0Un0 - 0.01, 1

-IF (;PFC- 2 SEGMENT-. 4

00MLZDASOHD04 F

0.000 0.00 0.00 0.00 0.000 0.000 0.0 0.0

U.o0 0.0 0 0. - - -- ----- P... 0 ...... _ Coo

Co -o -o .---- o o-----o-o-o--o-O --

', 00 0 0 0 0 0Q 0 0 0 0 0

0 0 0 0 0 0 0 0 0.00 00 0 0 0 . 0--- 0 0 0 0 0 0 0 0 0. 0.. . 2 " - 0 0. . . . 0 . ..0 - - 0' . . .. .. . . . .. 0 0. 0 " ". . ". . . .. . .

0 0 0 0 0 Is 0 C 140 A 0 0 u 0 56

022...... S 00:, 24. = " 0.3200 -- 022P= 0.002 2 S 0IMAP= 0 140 SUMNAP. 0.069

S AbSOH,3ED POWE[R AFD

A0SR0b2ED PO2WE.-R AO -_ __--0.000 00.000 .000 o.o0 0.000 0. 000 ... 00 0 o.000_ O0.000 - 0.0'.0 LD,0(l 0.22(1(1 0 .20 .2Q 2 00 0.0n0 00 20022 0.000. 0.00o 0.200 0Q.(00 .0,0 2. "lq 0. 0 n0 0.,00U0.000 0.200 (I n L'..22)v0 .0 0:)V 0.02 22k . 0 0.U0 0.00 2 0.00 0.00n0 0.000 0.000 r.000 0.000 0.000 0 .0000.000 -_ 0.000 C2.000 ., V 0 0. ....- 00 O - u00__ U . ..oo . .. __ 0.0009 _ 0.00n0 0.000 0.0n0 0.(I (2,0 . 0 0.O000" .0- u( ., 0 k.. m

ll? C. .on(: - t.0tr (11) * 0.V00 0.00 0.000 .nn 0.0 0 . .. )- .(0 - 0.

00 0.0o020

0.Ono 0.Ono 0.000 0.2O20 0.2000 3.u0 O O.U0 O " 0.120 2 0.000 0.000 0.000 0.000 0.000 " 0.010 O.Ooo 0 O0toO.Oo (I 0 o 0 0. 2 NN .000 2.2 0.200 0.0nO 0.19 - -

NORMALIZEn 0H0,)R0E PO0R AFO0.000 0.000 _ 0 0.02l 9.000 10.u - 0.00 .0.000 .0.000 0: .to0 0.0 0 0{.020 I. UIV 0.000 0.000)0.000 0.030 (0. 000 0.0 -o 0.000 0.000 0.00O 0.0000.0n 2.000 0,02 q. , ( , 0.9,( ;.UO 0.022 0.0000.000 U.000 0.000 0.22 00 2-.000 2.3220 0.000 0.001 20.000 0.000 0.020 -" 0.000 0.000 -0.000 0.000 0.001

0000 On 0 22 A1o 002 ____

.... . ...... . . . ..... .. ,*... .. . . . . .. .. . . . OR AL 00 A SOOHE 22 P0,010 022"U __ _ _ _ _ _ _ _ __ _ _ _0.000 0.000 0. 00 0. 000 0.000 ' 0.0A0 0.00 . 0.000-" 0.000 0.000 0.000 0.000 0.2o00 002 0 .'00 0.0200

__O_ _ 00 0o 0 0.000 0. 000 22.00 -. Qu 9,9£ U 0. O 0 O., oQ u-- 0.U09 0.000 0.000 U.000 9.001 0.020 0.,00 0.000

S 0.0200 0.000 0.00 0.000 0.000 .u0 0.0nu 0.020_0.. 0.0n 0.n00 .00 0.000 .v 00,0 0.00 _0.000 .... 0.000 0.000 _ .

HUN.7I ________ E00'0

F..-2 .....SEGMENT. 7

0 0 0 0 0 0" 0 0 2 1 1 0 0 3

§..7 0 0 1 . 201 0 0 0 2 41

OEGRFE-2 0 0 I 2 0 1 I 55.. .. SEGMENT.5 0 0 0 0 1 1 1

AFD OUTPUT 0 0 0 0 SOMAP. 91.527 SUMNAP.. 9.39e0 1 0 0 0 0 0 0 ASOUBF.0 POWER AFO0 0 0 0 0 0 0 3 0.000 0.00 0.00 0 0 0.000 0000 0o000 0.000 0.000

-0--.- .0 0.- -- 0.000 0.000 21.595 26. 949 ?1.3,? 0. 1.0n 0.00o 0.36,- ,o.ooo . . 1 . . ,0 . .. -1,o o 1.8 11.... e0r 7 - . 0 .6 0.9 . . .0 1 1 0 0 0 2 0.092 0.000 0.000 0.000 O.o000 0.135 0.2A? 0.636

SUMA s 4.468SUMNA.46.0!0 0.000 0.000 0.756 3.3 0.000 0.303 0.005 0.5 03

- - .. €4.468 SUPMNAP 1.060 . 0.000 0.010 0. 000 0 . . 0 v .0 ) . 073 n.142

0,000 0.000 0.000 0,"l0 0.000 .0n0 0.000 0.00 0.000 0.000 0.000 _ ... o _ o 0 _000 0.000-.. 0.00 -

j~fS~3DPqRAUNORMALIZED AHSORbED POWER AFU

0.000 2.197 0.000 0.0)0 0000 0.000 0.000 0.0001.001 0.000 0 020.000 . o0 0.000 (1.1n00 0.000 . . .... . 0.000 0.003 000 . .00|.1 0.042 0.000_ 0.006U. 183 0. - . ..o 0.00 ) 101 0.000 0.0n0 0.0000 . 0.00 .........__

0.000 0.000 : 0.000 0.00on0 0.000 0.000 0.00 0. 30 0.0 0 0 0 6 . .000 0,001 0.001 0.0030,00O .- 0,063~ -0.311 0.000 00 ,0. L 0.000 o.noo 0.003 0. o C . 00o0 0..0c? OOn 0.003

NORMALIZED AASOR0E POWER AFF

0.00E 0.000 0.0 .- t 0. 00-0 0.000 0.6.000 .00') U00.000 0.029 0.000 0o0oo0 0.000 .O(,O 0.000 0.000 DEGRFE'20.000 0.000 0.000 0.000 O.OOn 0.0000 0.0010 0.001 SEGMENT. 80.139 0.000 0.000 0 .00 -0 0..0055_-0_ 0_0 -- - - 00- - __ ..0.00 0 0 -- 0 c-- -- 0 - 000 1, V 0 .)n0 0 .00•3 AFU FVI Pu

0.000 0. 0 ,0590 0 ooo .0o0 0. 00 0,001 0 0 0 1 0 0 0 0 00 0. . . 0. 00. .0 0 0.. 0 0 0 01 u 0 00- ----- o o o 0 0 _ 0 0

0 0 0 0 0 0 0 0

0.000 .one _ 0.000 .coo .000o0.oo o -0 0 .. 00

0.000 0 .- 0..... O_ ... 0 .3 0.0.

0,00 0. 0.0 (0 0130 1.007 ~~~~ ~ ~ UNA._ 7 __ _ __ Z 7; .0

RUN 7nEGRFF-2 AHSORHEn POWFR AFU

.00 N . . . 000 0 . . 0.00 . 000 0.00) 00 .)0 0.00 ....

- - . . .... .. 000 0.000 -- ..

0:0 0E Q.00O 0.000 0.000 L0.000 t.000 .. 009 0.0nu. 0 . 0 0 0 . 00 00 .0 0.0 0.900 0. 0 0.000 0 ,1V 0.0 0 P.U 0. 100 0 0 ) 0 0 0 n.. . 0 .0. . .... .... ......... . .. ... . . . . . . . ... . . ... . . .... ... . .... ...

0 0 0 000 0 0. 0 0 000 0000 0,000 0 0010 0000 0n0 0.00 0 10

0 0 0 0 o 0AU PO . F ( I

0.000 0.000 0 .000 0.000 0.00 1.0o 0.0S .... 0 . . .. .. ......0.0..0..000 0.000 .0.00 L0,. 0 000 0.0 - ). 000 0.000U

000 n o 09 0.000 v.. . 100 0)v V.00. 0.7000 0,00

005090.0 10110 001--- -- ~-- - --- - ----- 0 -0-.2-0.000 0.000 .70 0.000o Q .001 0.00 boa

000. 0 0 00 0.000 0 '0.000 000. 0 0. 0.00 0 .006 0.001 -

0.000 0.000 0,O 0.000 0.000 .( 00n 0.ono 0.000 0.000 .00 1 0.009 , .01 0.0 0.000 00 .1l

0.000 o0.0,0 ,no voo 0. 8 0at ~ o___0.00 -0.00 -0.100 . .00-0.00..1(~0 .00 0.00 - .- ___________________________.________.___o_____.______________o___o__

0.001 0.0n _ 0.00 .. 0. 100 . ... 0, .0 . 0 '. .000 0.000 00.000 00 0N0 1' U O. 0.000 o Ono .000U i ( UN E.7

. 0.000 0.00 .00(0000, 0.01111 (..1 0. 010 0.00 ; 9I N0 9, .

0.--- -0.010 05 90 0_ 0 _. ____0 30.02

..0..9.O61 2E0 0.090 9011 At . . . . .... ...)0 0 Q .k! 1 O.U 0 • 0.U00 -- - ....- -%l~ -h T -9 . ... .. . ............... . ... :-----------*

0.0o 0.00 a.o00 0.00 (1 . , ..... 00.'_ 0.00 _.. . -- 2... ..... 0 . .- - .....-0.•00) . 000 ... 0.000- 0.0)00 C*,o'o' .0" 0 .oO 1.OoO 2 1 3 1 1 5

0.00 0 0.000 . o00. 0.0 , ,. 0 0 0 u 0.0 0 0 . ..... n .. . .0__ ___0.00 ooO 0O. 1 0 0 1 0 2 e 19

0.000 0.0m0 0.000 0.000 0.000 M .OtO 0.U00 0.000 0 0 0 0 0 1 A0.012 0.0., O..ok 0.300 0.000 0.0t.0 0.000 0.000 --. - _ 0 I 1 . .... 4 _

SUMAP.156.91A , SUMNAP. 12.482

~~~~1~~ --- (-.----.--' HURE 0000000 9110 -11--- -- ---- ---0.000 0.000 0.000 0.000 0.000 l0.S,14 IY .ns 0.2'10.00 . 0. 00 _a S. 5 ._ 10.4 9 _ '.09 _ 0.31 ___ 0.1 . U.OO . .0 000 1. 11 000 11.107 0.000 3.5 i .0. 47 0.o',, 10.092 0.000 0.000 4.477 '.G00 - 1.471 .2 0 (,. -8 I

0.000 - 0.000 0.000 __ .. 000 ... o.. 0 C. J03 .. 0.165 0.19 .3

0.01. 0.0n0 0.311 0.000 (.o13 0.170 .15 M 0.1U0

_....tNUHMAL [ZE 0MS0 1t4EU POWER AFUI 0.0000 0.000 o.o0 - . .. - .... 0.o 0.oe0.000 0.000 " 4.072 2.041 3.003 0.• h.A 0150 0.004

0.000 0 3 0, e00 1 4047 0.000 00 84 0,008 . 0.001- ..0 9 0.000 0 00 0 . 3 ? o.u(; P .03 5 0. 0 3 0 .(0o2

0.000 0.000 0.000 0.000 0.06,0 ('07 0.002 0.0(oI001 OOqO _0 p_59___.k000 o ,29 .003 .02 .1

. . =,. . -. . .. ... . . .. . . . . . . . .. ( ... .. . ...

p

NUNs7

-E SEGMENT-10

_00U.UT 0 . .. ___- -.-----.. ..

0 0 0 0 0 '.1) 0 RUN-7

0 0 0 0 0 0 0 0 1FRFE=2

0 0 _0 SEMENT )2I--. -Q.. . . .. . . . . . 0 R o 12

0 1 0 0 0 s 3 Z5 AF. QUT.__ _.0 0 0 0 0 5 6 0 0 0 0 0 0

0 0 A 0 0 0 0 0

SIt11AP- 3.63A SUMNAP. 0.189 0 0 0 _ 0 0 0!_ 0 0 0 0 o I

:SbfiBE POwER F 0 0 0 0 0 0 0 30.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0 0 0 0___ 0 . . . 0 20

SUHAP= 0.207 SUMNAP= 0.070

AOSORBED POwER AD.0.000 0.n000 0.000 0.f000 0.000 0.000( 0.000 0.0000.000 0.00 .0.00 0.00 .000 _ .000 0.00000 0.000 _.

0.000 U.00 0.1,00 V..00 0.001 0.000 0.000 0.000

0.092 0.070 0.000 0.000 0.000 0 .000 0.000 0.020

0.000 0.000 0.000 0.000 0.00o0 U.000 0.000 0.000 0.000 0.000 0.00 . 0.000 0. Oo_ .. 0 0.00 .0.025 _ ..

0000 0.000- 0.000 _000. .00 0.00 0.32 .0..49 . 0.00( i .ooo 0. .000 0 .000 0.000 0.000 0.V69

0.092 0.000 0.00 0.000 0.000 0.00 0.000 0.45

0.000 0.154 0.000 0.0110 0.000 1.b15 0.165 0.010 NOWMALIZE 1 ABSORBE0 POWER AFL.

0po00 0.000 0.000 0.000 .000 . .6. _..136.. 0.12 0.000 U0.100 0.000 0.o01 0.000 0.0n 0.000 0.00oo0.000 0.000 0.000 0.000 0.000 0.0,,) 0.000 0.000

NORMALIZED AHSOwRE) POWER AFU 0.000 0.000 0.00,_ 0,00)) .0 _0.000 0 .. 0.09 ..

_ 0.000 .0.000 0.000 0 0.000 ,0. 00000 000. 0.000. _ 0.000 0.069 0.00 0.000 0.000 0.000 0.0t,0 0.00o0 0.o000.000 0000 0.000 0.000 . u.o000 0.0n0 0.000 0.000 0.00 0.000 0. 000 0.0000 0.000 0.00 0 0.000 0 ..00 0.u

0.000 0.000 0.000 0.000 0.00 . 0.000 .00o 0.)n00 0.00. . 0 00 0.000 0,00 __ 5 0.00 0.000 '. _ _

.0,069 . 0 000 0.000 _ 0.000 0.000 000 0.000 .. 0.001. -- NI = -

0.000 .05" 0.0011 0.000 V. tct 0. -o. 0.0oe 0.001n

0.000 0.0n00 0.000 0.000 0. 000 0.0 0.00 0.001

; .. . .. ...- - -.--- --- -"--"- U - 7 u '*" -=-.. . . . . .. . . . . .. . . . .. . .. . ..

,UN.7 OEGREE 2

)ECPF00-2 - - - __ - -07-5GETh13

SEGMENT-I.S EAFD OUTPUI

AF OUTPUT ..... o o " - - --. . .b .. .3". . .- .. . . . . ..

0 0 0 0 0. 0 3

0 0 0 0 00 L0 0 0 0 0 0 10 0 0 0 0 0 1 6

. 00, 0 . 0 0 .. 0 . ...... 0_ . ... .2 0 . . . ...... 0

S0)0AP.00 1.1081 sUNAP0 = 0.030 0 0 0 0 0 0 0• .... ... .. . . .. .. . .. .. .. .. . ' .,_ .0 . . 0 . 0 __ 9 . .. . . .. BSOR F D .00 - -- - -- -- .. .

0.000 0.000 0.A00 0.00 0.00 0.0n 0.00 0.091 1 1 0 0 0 .0 0 330.000___ 0.000. 0.000 .. 0o 0.000 0.00 . 0.00 0.0 . .

0.000 0.000 6.00 0.10 0~.0' 0.000 0.374 0.198 . .0 0 2 0 0 0 0 2

0.000 0.0110 0.000 0. ( () ..000 "1°0 0.11 3 0.010 1'0 I0 0 000..000 1.000 0.000 0.01), 0 000 . ..0U 0.01 0.7 00,)

. ... 00 .0.0 . . 0" 0. . 0.00 00 0 . .. 0 . 0.0.5 -0.05. . ... ..

0.011 0 006 o . 00 o 0.e14ABOR)0LED POWkR AFU.. ... . ...-... . -0.000 0.00o0 0.000 _ .000 - .000.. 0.00). . 0.000 0.00o

(;

0.000 0.010 1.000 0.000 0.')0 Q . 0 .0 ') j.O000 0.0 Ij)00.000 0 .1no0 0.000 0.000 0'). (, .000 0.0n .0.600.. 0.00 . n.373 0 ).000 .0.000 v .'.00 G.0' . 0.0n o 0*0b7.

0.000 0.000 0, .. 0 , 0 0.000 0GU ).D.V r ) .70)

0o.016 0.0 .0 0.623 0.0 0. 0.0 0.0,)0 0.0 0.0 o

)"NO.AALIZEP AH50RhE0 0 PUE-0f. H....

NORMALIZED ASO0EU POwEk AFU 100 002 0.000 0. 000 .000 C.000 0.000 (. Ou 0.000 0.000

0.000 0.1)00 0.000 ____0.oO 0.103 0.00n 0 0 0.000 0.000 U.000 1.01 ,)olp I * 00)) 0 .Oo 0.00"

0 .000 o.oO 0.000 0.000 Q00 C 0. 010 0.00 0.00. 0.OC 0.000 0.000 0.000 1. t00 (.000 0.00,0 0.000

0.000 0.0nQ 0.000 0.0n0 0.000 0.000 0.004 0.001 0.069 0.141 0.000 0.000 0.00A C.000 v.vn3 0.03.

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NORMALIZED Ab0S04E, PoWER AFU0,000 16.083 54.2081 49,321 36,b8H 3.9fr 0,o?.9 oi UUNORMAIZ ,00 U0SI9 PUE U:11f0. J .34 8.144 40.6J 0.U00 1.P. 0.111 0.i05 0.00 000oo 0.000 U .000 0.000 0 U .000 0.0U480.071 2.3J2 )0. 000 . 000 0.092 0.0 0.000 . 0.000 0.u 0(000I 0.000 0000 0.001 0Z3 --0o- Q.000 . 0. 00 0 00 0 ,) D V.00 0.000 0.061 o.-..u.-0.27 0.000 0.000 0.000 0.000 0.069 0.044 0.025 0.277 0.00 0.000 0.000 .000 .0O 0.0 0.69 .006 0.090*000 0.464 1.710 2.134 0.280 C.08b6 0.011 0.003 0.000 0.00n 0.000 0.000 .0c0 0.029 0.003 0.0070.047 0.096 0.940 0.00 0. 116 _.0. 4 - .01 . .0.000 0.007 0.0 0 0.000 0.000 0 .0 0.0O 0.00 . 0.000.047 0.096 Os?35 _.0 000.000 0.044 O.U01

RUN_7RUN

00 ". " 0E(;N7F -5

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,, + AFU OUfPUl07( 0080So~olUIPUr

0 0 0 0 U 0 0 20 0 0 0 0 0 0 20 1 0 u 0 0 0 0. 00 u0 0 0 I00 0. . . '. . .. 0 0-0 .0 .0 *

0 .50 030 0 0 0 0. 8, 0 0 0 0 2 1 32- - 1 0 0 1. 0 0 0 440 0 9 72 0 0 0 0 1 0 0 1 J6.1. 2 0 3 1. 0 19 2. 1 0 2 3 1 1 0 d 40I 0 1 2 3 23 * 22 8. .. .. . . .I " S1AP 56.186 SUNAP. _.-754.SU..00.l80.941 SUP.NAP- %C05000 OWR 737

OAHSOA D P SOFR AFIOwE. ABSORED POWER AF POwE. AFLI00000.000 U. 000 0.100 0.000 V.O " 00.000 0.000 0 ooJ0.000 Vo.0O 0.000 0.oouu .000 0.000 0.00 23,297 . 21.059 0.000 0000 0000o .000 0.000 0.0oo 2.4000.0On 0.o000 0.000 0.000 0.000 0.000 3.041 1.521 ... 0.000 0000 0.000000 00 0 . 00 .000 0.000 0.no 00.890 0.000 0.00-1 0.110 0 .090 14.073 .?94 L.131 0.367 0.000 0.000 19.309 0.000 0.000 0.000 3.5-41

-- 0.000 _ 1.493 0.000. 10.309 - 0.303 26.471 - 4.068 2.04 . 0.000 0.000 0.000 7.546 0.000 .010 0. 20 1.I00.051 1.230 3.003 22.630 11 f45 9.607 4.:078 1.004 0.000 0.507 3. 730j 3.110 2.450 0 .000) 0.181 0.00.0:.62 0.0254 0.,244 6.220) 7.30 1.99d 2.V84 v.305~ ORLZD0010080001C- :"N AIE HSPE OE ~ . .... !! NRAIE ASSORUEU POWER AFUCh 80,000 0o050o60 PO0,2 . . .o 0.00 0.000 o.0oo 0.0u0 . U.ooo 2.0o 0.000 0.01. .0.000 0.000 0.000 V.000 3.000 3.Oo 0.000 0.137 . 1.629 0.000 0.000 0.000 0.000 1.00 0.O4O 0.014

0.000 -- o00 - 0.000 9.000 - 0.020 0.000 0.037 0.068 0~ . 0.00 000 0. 00 0 0. 0 00 0'.000 0.000 0.000 0.040 --.- OO 00 0 0000 0,000o 0,000 0,.On0 0.000 0,044S0.671 0. O 0.060 0 000 (..o00 .. 33o 0.015 0.037 .. 0.277 0.000 0.000 1.2o U.000 0.000 o0.0o0 0.021 -0.000 -. 0.563 0.000 1!726 0.000 ).62o 0.050 0.013 0.000 O.0o0 0.000 0.711 0.060 0.000 0.003 0.010,1- 0.114 n.464 0.570 2.134 .0.oo0 0.229 -0.049 0.006 . 0.000 0.191 0.705 0. 13 0.01106 .000 0.002 0.0030047 0.096 0.235 0.56bb 0.J347 Q.047 0.0;5 0.002 ..-- D NUM8ER 53 - . 7 ..

SEGMENTaI3

AFU OUTPUT0 0 1 0 0. 0 0 000 2 1 0 0 0 0 801 1 0 0 0 0 0 300 0 I 0 0 0 0 0

0 0 1 1 0 0 1? 02 1 0 1 0 0 40 0

SUMAP=338.603 SUMNAP . -.95

2,9 RUNOY

ABSORBED POWFR AFT )-. . DEGREE=5

0.000 0.000 104.795 0.000 t.0 0.000 U.J90 95.b17 SEGMENT.16

0.000 17.576 43.189 0.000 0.000 0.000 0.000 38.4050.890 3.622 0.000 u,000 0.030 0.Uou 0.000 5.935 0 PT0.307 .00nn0 7.330 0.00 V. nO 0.000 0.000 0 .652 0 0 0 0 0 0 0 13

0.000 0.000 3.7023 7.546 0.0t0 0 .0 p2.b38 0.000 0 1 0 0 0 0 0 59

0.125 0.2594 0.00 3.110 0.O000 .OnO0 3.bS 0.0o0O 0 0 0 0 0 0 67

NORMALIZED AdSOPHEU POER AFU 0 2 1 0 0 0 e 16

.0.000 0.0(10 19.760 0.000 .-u000 .o0u 0.010 0.93 . 0 0 3 U 0 0 S b

0.000 6.628 8.144 0.000 0.vto 0.000 0.000 0.0260.671 1.366 0.000 0.000 0.,00 (.700 0.00 0.035 SUMAP= 81.959 SUMNAP . T

0.277 0.000 1.383 0.000 0.000 0.000 0.000 0.004 -6,O -0.000 0.000 0.570 0.711 0.U00 0.00 0.011 0.000 ASORE POWER AFo10.094 0.096 0.000 0.293 0.0(0 0.000 0.043 0.000 0.000 0.000 0.00u 0000 ,1000 0.000 0.00 19.3

OEGR 5 0.000 0000 0000 0000 8.700 0.00000 00.000 2.3.RUN.7 -0.890 3 . 6;2 0.0100 0 .000 ).l .00 Onoo000 0.00 .56DEGREE-5 0 .000 O.Oo o o. oo 0 . 00 0 o. 0 o 0.000 9 .000 2..46

SEGMENTIl - 0.000 1.230 3.023 0.000 U.U000 0.U00 U.440 U.36

0.000 0.000 3.730 0.000 0.00 0.070 .- 53 0.0,9

AFO OUTPUT,0 . 1 1 0 0 0 0 11

0 1 1 1 0 1 0 650 1 1 0 0 0 0 70I ] 11 4 1 0 0 340 1 1 3 1 1 19 180 0 1 2 0 0 SI 2

51"SMAP532.456 SUMNAP. 9

Af A NORMALIZED AbSORHED POWER AFUAISUROFO POwfR AF) _ -. 0.000 0.000 0.000 0.000 0.000 (,000 0.000 0.Udv

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1in0.000 9.788 43.19b 10 7.797 0.000 17.317 0.000 31.204 0.671 1.366 0.000 0.U00 0.000 ('.000 .000 0.0780.000 3.b82 17.799 0.000 U.000 0.000 0.U0 . 13.849 - 0.000 0000 0000 0.00 .000 0000 0.000 0 .000 0.010.367 * 1.493 7.336 73.238 14.4?5 0.000 0.000 2.772 0.000 0.464 0.570 0.000 0.000 (.0"0 0.005 0.0un30.000 0.615 3.0U23 22.637 5.945 I.eI2 4.178 0."05 0.000 0.00 0.705 U.000 0.ot 0.000 0.005 0.000

- 0.000 0.000 1.246 6.220 0.000 0.000 4.0l1 0.028 - _,-,-

NORMALIZED ASORBE0 PUoER AFT)0 --. 0.000 . 8.041 19.760 .0.00.0 0.00 £C.000 0. 0.000 0.07 .. 6

0* 0.000 3.314 8.144 10.163 0.000 0.40b 0.000 0.184 RUN0.000 1.306 3.356 0.000 0.00 0000 .0 0.000. 0.082 - U=

OEGRFE=5SEGMENT=17

AFO OUTPUT

0 0 0 0 0 0 0 5680 , 0 0 0 0 0 0 371 0 0 0 0 0 9 37

0.277 0.563 1.303 6.905 0.60 0.000O 0.000 0.016 - 0 2 0 0 0 0 17 6.0.000 0.232 0.570 2.134 . 0.2 . 0.029 . 0.049 0.004. 0 0 2 0 0 3 26 5

,000 0.90. _ t. 35 0.586 0. 00 O.OAU o4 0.000 SU 121.94 Su P

RUN.7 . . o,(f1DEGREF5, ASSORHEO P0ER AFD

*EGMENT=I5 0.000. 0.000 0.000 0.000 U.000 0.000 0.O00 67.5bu, .00 1 0.000 0.000 0.000 0 , 01 .(0 0 n.0 0 3 . 44

AFU OUPUT 0.:890 0.(0l 0:100 U,0t10 0: a . C 0.000 (.32v0 - 0 3 2 0 0 6 27 .. ... 0.000 0.000 ..00 0 0.000 0.00 .00 000 0.0v0ou 1.74 ...0 7 I 2 1 0 0 77 0.000 1.230 0.000 0.000 0.000 0.000 3.7~8 0..)?j0 0 0 1 0 0 4 0.000 0.000 n 2.492 0.000 0.000 1.4 9 2.356 0.069| ? 2 0 0 1 2 .9I 0 1 2 0 1 5 14 . NORMALlIZED A RE0 POE9 AFD0 0 3 5 0 I 4 I 0.000 0. 00 0.000 0.000 0.U0 0.000 0.000 0.394

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... 0 0... 3 6 5 0 . 0 . 0.000 0.000 0.0 7 0.000 0.00 0.00 0.000 0.152

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, --.000 0.000 0.0 .000 4.42b 3.00? 0.0010 0.000 0.7050.3607 2.9 1 1.67 0 0.0 0.000 2.9,1 0.000 0.JoL0.151 0.000 3.0n3 19.09 V 0111 1.12 1.0.9 0.4700.000 0.000 3.730 15.549 2.450 0.1(00 2.2h5 0.05$

NO.MALIZED ASO00EU P(. AL)FU-- 0.000 0.000 59.281 49.321 OUv 0.0,10 * 0.000 0.105

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RUN 7, DEGREE 6




SFACTIORS ARE

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MAAINUM POSS1J I LE CoUiTS PEI, 6 r- T

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6 BSOk4ED PO,,ER 'PT ki X

0,00000 0.000 0 0.0000 0 02 o 4 ).921 1 .1. 266 2.9120 0.19137

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0.000 0000 0 .0000 0.( (1i01 1.401' 0.6 4U8 0.08401 0,o0552* .,0000 U.OO00o 0.0fl0i0 0.33634 0s.5935'- (.2s720 U.(+462 U.002i8

0.00000 0.00gc ', 00 0 0 .453 1 .3497 0.i 600 0. C U.00019

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AH0SO4SED POWER AF 4 BSOBEO POW AFO

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A.SORHED PO0W0 AF0 NO0i0ML IZE ASOPHEU Pow AFU 0.000 0.000

0.000 0.000 0.000 0.000 61.727 17.31 1.200 0.37 I 0.000 0.000o 0.000 0.000 0.000 0.0o0 0.000 0.000

0.000 0.1o0 0.01 9.0l| ( !.•*00 7.3.i4 I .4 ____1.0 0.6 000 0.000 .0o UU . 0.000 - .0 . 0. 00 0.Oo0.000 0.000 040.000 10 .O U 0. 0

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0.000 0.000 0.000 0.330 ....o . 187 _ 9. 5 0. 13 _. 0.0215._ _-._.. . . . ...

NORMALIZED AHSOPBE0 POWER

AF I0.000 o0.00n 0.u00- 5,334 0. 1.0 - .510 ___ 0034 0.001 . .....

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0.000 0.000 o.1O0 0.107 0.0 o .0 0 . _ 0.002 0.000.

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AFU OUTPUT F U0 0 0 OUPUT 0 0

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0 " 0 0 0 0 0 0 u 0 .

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1 ci 1 0 0 0 0 2 1 0 1 0 0 0 0 1

0 1 0 0 0 0 0 7 I 1 1 1 0 0 0 30

SUMAP 0.094 5JUMNAP- 0.001 OSUmAP 0.410 SU-INP 0.032

AqsU EI PO.EO AFD AbSORFIED POWER AFO)

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"UNRMALIZED ABSORBE 7

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SEMENT 14

AFD OUIPUT AFU uUTPUT

0 0 0 0 0 0 0 0 0 1 0 0 0 0 0

0 0 0 0 u 0 00 _1_ 0 0 0 .

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SEGMENT 15

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0.000 0.00 0.000 0.000 0.000 0*0 .. 0. o0 0.010 0.000 0.000 0.000 .00O 0. 0I: _ 0 00 0.0n0 0 *v1

0.001 C 0.000 0.00 _ 00 I ' Q .01__000__000 ____i,____ .0 _ 0.000 .0 0.( .000 ,o 0q lC0 0.0 ,o , L 0

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0.000~ ~ ~ ~~~~., V. 0.0 000 000 .90 .00 0.7'.3 1.00t,0LZOlSROI 00 00 ____ . . .

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0.000 u.00 0.001 0 . 000 . 000 0.0 0 0.0?b00 0.0130 . 0.000 0.000 0.000 0.000 0.000 0.000 0.012 0.0".4

0.00n 0.000 0.0u 0.0o10 O.000 0.1j(o 0.002 0.0,l3

HUN.AR . . ... RUN ._ .... .r OEGREE. .EG t~

$SEGMENT 10 SEGMENT=1 2

. -_ -AF) OUrIP0T

0 0 0 0 0 0 0 00o 3 0 0 0 0 0

o 0 0 0 0U 00 0 0 0 0 0 0 4

AFD ouTPuT

0 0 0 0 0 0 0 0"0 0 0 0 0 0 o O - -

.0 0 0 G 1 0 0 01 0 , _ _ _

0 0 0 1 7 3 4 52 0 0 0 0 2 0 0 3

0 1 0 3 6 8 19 39 0 0 0 4 U 17

SUMAPs .0 SUNA 0.2 o SUMAP 2.601 SUMNAP- 0.025

_A IISORHED. POWER9 AF -A50RHED) PO6WER AF 0D

0. O000n 0.000 0.00 00 . 0.00 0.000 . 0 n0l 0.000 0.000 0.000 0.000 0.00 0.000 0.000 O.o0n 0.000.000 . 0.00 0.000 . 0.000 .0 0.000 0.000 0.000 . .0.00o o. 0 __ 0.ooo __0 . 0 0.00 . 0,000 . 0. . 0.000 .

0.OOf 0.000 . 0 0.00 _ 3 ) .-- 0 -0,00 0 0 0 .. .. 0.000 o.oo o.coo .c 0.C000oo G 0.000 o.ono .05is0.000 0.(n00 0.000 0.000 0.513 o. .108 0.0n0 "4.e85 0.000 0.000 0,CO0 0.000O 0.30' 0.0O 0.000o 0.05oO.o000 0.0o0o 0.000 0.014 0.413 * 1.401 . q2 000 0.00 0000 0000 0 18 000 0 0 .263

0.000 0. 0'0 0.110 0.0 2 0. O. u 0.000 0.000 0.000 0.000 0.00 0.000 0.010 0.03

0.000 0, 00 0,0 0 0,000.0.0000 0.46 0.92 , 0*0 0.000 0.000 0.000 0.000 0.000 0.000 0.0a0 0.00t

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0 . .0 o 0.000 O.0Oo....O.0 _. 0 .1!Z )0.017 3.000 0.0' 29- 0.000 _ 0.700 0.000 0.000 0.000 .000 0.00 . 0.00 .0.000 . o 0.000 0.001n 0.019 .0021 0.017 0.021 0.000 0.000 0.00(0 0.000 0.00f 0. 00 0.000 0.004

0.000 0.000 0.000 0.00? U.07 0 ... .'L.1. 0n- a

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" l OII'OAFD OU$ PUOAFU oMtuT

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0 0 0 0 0 0 0. 2

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0.000 0.000 0.0 0 0.0lo 0.1

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. *oL 3.0nq 19 1.4

NOkMALIZED AHSoPrEU POWEk AFt AU ESOWUE D POwEq AF__o_____oo__________._ _ _ oSV~oooo o P. 100 0 6.. .oou .... v___ i_ ___ po____ oo.____.oo_ _.. .,

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0.000 0.0 0 000.00) 0.0.). .03' ..0102 .0100

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0.00 0.00? 0 . 000 0.100 0.000 0.1110 0.00( 0.'0J

0.001 0.000 0.010 0.003 0.027 0.000 0.00 0.030

0.000 .000 . .000 .... 0.Oco 0.._ . o0 0.004 0.036

0.000 0.00 0.000 1..u00 (.. .01 (1.011|1 WE=ltl

OEGREF~~DE RE E- I00 ~1R U N .. S E G M N T =1 6

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0 0 0 0 5 0 0 490 0 0 0 7 2 74- -- - ---

SUMAP 9.413 SUMNAP. 0.076

SUIMAP 59.6b52 SUMNAP. 0.969A- -_BS -o_ , -AF . . .. - . .......

0.U00 0.00 0.000 0.49 0.000 10. 109 12.143 3.034

A8SORtED POWER AFU 0.000 0.000 0.091 0.193 1.681 4.16 5.00b ).20 510.000 0 0 O ' Q 0.000 0.00. 0 ... U 00 I.f1? 4. I 5 1.0310.0. .0 0." 0 A 0 00 U.00 0.000 0.000 0.000 0.000 0.033 0. 1- 0. 0.o U I ;. t0.000 0.000 0.000 0.000 0.000 0.000 0.000 0_.09 0.00 0.010 O.no 0 1 8 .J- ]09 0 0 0 10 0 ' .00 0, n0 .(0 O.Occ0 M OO 0 0-- -1 0.0 "I 0 1t - O.nf-b u.049 ... .,-'U "- ?.5J45

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0.000 0.Ali 0.000 .O o _ 0 . 0 0 0.000 0.0 0.000 0 017 0 .000 0 .00 0.00 0.0. 0 0.049 0 'U.000 0.000 . 00 0 ._ Q000 0.0 .0000 0.000 ,000_ 0. 00 n 000 0,000 0 1.1o . . 1 0.00 0.090.000 0.000 . 0.000 0.000 0.000 0.000 - 0.000 . (.0 0.000 0.001 0.006 0.l07 .0.000 0.0250.000 0.00n 0 0.100 0000 0.000 0.O.o 0.000 0.0O0 p - Ao. 0.000 0.001 0.002 .00 0.019 0.0140.000 0.000 0.o00 _ 0.700 0.007 .000 0.000 _0_.010. 0.000 00 __ 0.)n O ___ Q 0.000 A ).014. C .00O _ O . .0.....)0.000 0.000 0.000 V.000 v.0 '.000 0.003 0.010o

kUN . .....

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RUNI8 AFO 0UTPuT

OEGREE-=1 0 Q.. . 0 0 0 0 0SEG ENTIl 5 0 0 A 0 0 0 0-

.. 0 O T0 0 0 1 0 0 0AFO OUTPUT --.----- 0 . 0 0 1 sS0 0 0 0 o o 0 0 0 0 0 30 0 0 0 0 0 0 0 0 0 0 0 6 5 7 010 Q 0 0 0 0 o 0

.. I 0 " - SUMAP 7.951 SU, -i.....N.. .A0..... .0 0 - . 1 0 Q 0 40 0 2 .5 2 3 65

SUt)AP. 7.553 5UMNAP. 6.070

.ABSOR0ED PW. AF( 0.00 0.000 0.00 0 00 .0 0.000o-000 0.o0o0 ... 6.666 -... 1)oo c o o.3 . . 6 ( O. n ..o iioo. . . .0.000 0.0.0 0t.000 0.0) u.I0 . (000 0.00 0 0.0no

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.0 oo _ o.n u.o0 . . _.l . ;QQo II . 13 7.J.4 o.uoo .o0.000 o 0.00oo0 0.000 0.o00 .0 7o 0.00o o.AO -0 0 P.0o n 0.000 0.000 0.:)0 0 .j-. 0.0o0 0.100 0.000NORMhALIZED AHSoRBED PowER AFD .. . .O.O on3 Q 000 0.00 . O0 e

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0.000 {0.007 0.000 0.00 . 0. 0 0.00.0 . 0.0 NOwHMALIZED ASORHE P0L0R F0.000 0.000 0.001 U.000 9.011 0.00 0.000 0.021 0.000 0.000 0.000U 0.000 0.000 0.00.000 0.000 0.000 0.001 0.O0 C.06 0.005 0.014 .0. n .00 0,0. 0. - 0 0 0 0.000 0.00 0.001 .O.Uo ) 0. 00 0.0( . -.000 0.00 0:.1o0 .0 0 0 0 .000 .0 0 0 0.0 ) (. U 7 , .0 t o 0 O n o

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O0000 0.0500 0.000 0.000 --- ('.007 -..... -.] 0.012 " (t.001

RUN 8, DEGREE 2




lFACTORS At E

,.01 740 11 . 4 7 f !0 .i4 AI U C;.2b+ 1.12 I,,) J i035t.

\i-PLIT.[ IDE LF VELS f S-I .AT

0.U3 0.05 u.U 0.]3 U.21 .32 0.50

4L.U!JEP'.CY IEVE:S AR SFT T

U.U6 Q,12 U.-25 . : . U . 0 . :. 0 1 . 0

It'T t R A PI. TUfES SEKP

13.044 0.06H t o 0. I 5 0. < 7 ".."1 5

CL iTER F-RE(oI it'J Jt.S APR

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MA/ I NUM POSSIb L: COUT'.I 5 - SE- .(F_,

I 1.36 2.65 5. 3(3 ](. b'j7 21o]3 42.4 T 4,,. b3 169.7 5

*AbSU~r3't. PO'd E MAT IA1.30 61 i. .33 7 1 ....1 6, . , , , .9l1 1v.0-3i 1 0 3 4 1) 9[2.l.53473 2.1 9 97 1.. (972 -':. +3. 21 32 4. 32913 _o7bd 00.2244 0 y.9054+ W414'-) ( 1. 1 " 75ti2 I. b'41. 0.432JF2 ). 494

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0.01557 0.06 33 . 11 -)9 o. 1 '.o 0.t.125<+ .124,9 U.:'?& U.0 034O.

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J.46777 -, 1 4'UV 6.1 : 2.1 0 V .3 0.24759 . 0.0C172

0.40709 Q. ~.5 3 .0 2, 45I 1.,, 0.10204 f 092. , 07 1,.1 6777 0.3/+4" 0 .03900(,' 1.;47].. :.q1'-tu 0.0 42.'J. 0.103..J 1 O,,,lc)

0..0 91.4 0,.1407.3 b.34~i1 3U. B br 1. 170.. U .01733 Q. 0i1 7 o. ,)l2w.0?850 0.S -'J ,.l'4 2 C.177 " .C7 o .. )714 '..QO,5 0. t jm

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10(10 690-00 0( o -00 e 0 1

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--L---- 1 0 -0 O -;-,0o ~ 0 S21 001 0 ol0o ~000*0 000u0 00"0

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W N.fll4

..- URUN--R U N O .E E =2 D E GE E N 7

HUOREGROC.,O - - IEGRFE-2__________________ ___

SEGMENT- 7

AP0 OUTPUT _ _o-0 0 0 0 0 00 0 0 0 0 0 0 1

SEGMENT. 5

AFD OUTPUT

0 o 0 0 0 0 0 0'0_L...... .. .. .. .o . . . .. Q .... .. 0.. . .. . . - o o -o 0 o 0 0

S 0 0 0 0 0 30 0 1 0 0 0 0) 0 5,28

2 0 0 0 0 0 0 44 , : _

0 0 0 1 0 .0 0 0 56

0 1 0 0 0 0 Is 34 0 1 0 0 0 3...

.' SMAP. 17.426 SUMNAP__3.19_ -. .. SU.AP 5.190 SU-NAP. 0.6066

ASORHED POWER AFAOP- -ORI E ASOBED FO_0,0000 O o 0. 0 .00 0.01 1----- 00 0-000 0:000 -0.000 0.0 00 0 .000 0.000 O .u00 0.000 0.000 0.000-- o.ooo- .. 00. 0 9f--- o.000 ----- 0.00 - no. 0. oo 0.00

0.OTO o. 9 1079 0.000 0.000 0.000 0.000 0.040 0.000 a .ooo 0.000 0.000 0.000 0.000 0.000O 0.10

0.00o000 n .201 0 .0000 00 - .000 .0 O_ .000 O .000 1 .12t;.

0.000 0.000 0.000 0.000 0000 0.0no 0.000 1.4B4 L .__ 0 . 00 ., _ 0.00 0.000 0.,10o . ...0,0 0.000 1 , 0

0.003 0,. __ 0.000 0.00.0 0000 00 0 ,000 0.97 -- 0.000 0.00 0.00 0. 00.. 0.00 .000 0.000 0.00. O00 0.(100 708 0.000 . 0000 n * ..... - 0 _ t10 0 e9001 - 0 000510.75I0000 0,063 0.000 0.000 .OU. .Oo 41 :136 a.10. 0.000 '0.1.3 O°O.o 0.O00 0.000 000 0.088 0.097

OA -O AOSOOOEO O El rlo NO)MLZE SOSOROED OWER 00

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0.000 0.000 U.0 0 .00) u u. Ou IJ*UU u. 0.0 o.001 0.00) 1. .3. 1 0OUU) 0.000 0.1'00 0.0010 .O o5 0.0d

0.13 0.0 rO 0.000 0.000 0.000 0.uo O O.0 05 0.138 0.000 ,__ 0.011 0.000 0.00 i .00 ,,U 0...00 . .

0.000 O.on 0.0143 ,0,000 000 0.00' ,I0) 0,00. .. "i 0.000 0.00I0 0.143 0.000 0.It00 C, 0q0 0.0o0 0.0030.000 0.0 0.000 0.00_,_ 0.00 0.0)0 0.00Z 0.001 0.000 0.024 0,000 - 0.Oo 0.000 1.000 OO.i 0.001

- ,- -------- -UN,,-

RUN-8 I)EGRE

I m . 6 F - - --. -SEGMENT. 8

F- U-AFUL OUTPUT

00

0 0 0 0

0FUoUTPUT ......................... .. ...- 0 Q 0 __ 0

1O 0 0 0 0 0 0 0 0 . 0 00 0 0 0 0 0 0 0i .. . .00 0. 0 0 0 0 0 00 ....... 0 .0 0 0 0 ,0 0 13

SI)MAII 0.395 SU .AP 0,09 SU 0. 0.153 SUMIVAP- 0 --0--.

i _ j500tF_ O .ER _AF'O _- _ _. I . ... bS0R[; 0 POWFR AFO .. . . ... .. .. .. ....... .. ..

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0.092 0.0 n 0 0.000 0.000 0.00 0.000) . 0.041 : 0.0092 0.070 0.000 0.300 0.000 0.000 0.000 0 . 0d0

v 00 .')Tn) o- ..0 0.00' I. 10 0.00 oI.i 0.00 0.000 G. .00,un (UO00 0083 0.000 0.000 0.003 .01,0 0.000 0.3?0 0.000 0. 00 , U bOllI - A-0.0. 0.015

0o .00 0.o6 0.... .o0- - . .. . o.o - .oo o.on . .0013 ..- .0 o._ ,o O tk . _o .

NORMALIZE ASO U P .NOMALIZE AHSOUEO POEH AFL).

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OO00 0 00 0 00M.10 0.,73 1.0,, 0.0011 1.01)1 0.000 0.000 0.000 00000 0.o*O io. o 0.0nO 0.000

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- v U ' e ' . 0 0 0 O n ) ' . 0 o . ' l u - 0 .0 0 0 o 0 .0 3 ) 36333)03333,37 0 . 030 ). r 0.00 u.O O 1)..n 0.000 0o~ L..000'o _00 033 .00 1).o . 0 - 0- 0 .)0 __ 0.0 - 3.3

l M000 .) 0.--)- 33.. .0 3)0 U.U .3n3)o30n0 .o0n 0VO

RUN-8 . . rGF 3

.E lMENT. 7 . .... ..0--- . 0 3.. . 3F3 3t TPIJT

0.... ... ..00 .3O 0.0 .30 000 U.30 00) .0 .0) .0 0 0.0 0- 039 ___0 00. 00 ...........000.0) 0330 0333 .30 0.333 30) .0 .U 0.00 0 00) 0. ' 0 09 3. 303 * (1, , 3 3 33

0 0 0 0 0

AF00 GUP

0 3 3 • . 2. 0 .. .0 ... - ----..... .. . 0 0 11 ... ...

____________________0 03)2$3

0 3 0 0 I 3

.0 0 o o o0o 9 3

0 1 0 3 0 132 - 00 .. 0 370

0 0 1 U 3) 0 3

1)0 33)3j0 o

___mAp 1.793 SUU _P_ 0012 o Cos2 SU0 0ap_0

-0 0 0 0 3) 0 3) 35 .. -0- 0 .00 1 3) 0 0 3) .3 3.. . . .. 0

1 ..ABSOR HUO PQIEI AFL,--- AHS . ..0ED -POW0R AFU ...... . 0.000 .00 0 0 0 .. " 0-. . .

0.00 0 0 3......0 . 00n 0.U03 3 0 o. 30 3 .0 u 6 0 . 0 0,)on.3.. (. .. . .. .033vN.3.. . . . . .0*000 o o00 - .0 0 .000 (,_ 0__ 0.00 09 0.00 0.3) 0 0.003 0.00 o n0 . 0 ) 0.0Q Q 0. 0 n0 U0.000 0.000o 0.03 0 0,3. I.30 3 0 .030 0.003,0 00 0 0 00.-0 . '"'.0 0 0.0 - 0.30.000 - . 0 .000 _ .. 3o0 3... - .000 0.1700 0.0 0 0.7 0 .0 ) 3 3 , 3

NOMAIED 0'E Pw NF0 MLIZED A, b(opva PO0 .R AFU0.00 3 E.000 0.300 0.000 (.co 0.3)0 0.000 o.- 0 0.003 )00 0.0309 0.300 0.3))3) . 00 0.(0.000 0.000 0.000 0, .c00 0.000 0.00o 0 0.0. 0.03) 0. 0 0.000 3.000 0... .. . 0.) 000 .)0

0.000 0.000 0 ).000 0 0 .0 . o 0.0 00 0000 000 0 0 0 0 .00 .00 000 0.00.o 0.0000.00 0.0 0 0.000 0.00 0.00 COoO 0.030 0.003 0.00 0. - 0.0 .00 0.030 )0 0.3 330 00-00 .00 0 o0.000 0.)00 0.000. 0.000 0.)3 . 000 0.0 0 0.002 0.000 0.3)30 0-.)0 0.)0 0., .3-0 0.000 {.,0q0.00) 0.0)0 0.00 0.03 ) , Q.30 D ,0 3 O.00 0.002 0.000 ' 0 3 U.00'0 . .0,0 0.000 3.0010.000 U--- , 0- 0.000 3.0 , Q t' . Q '333 V. A 0.)1 , _(t. 0 0 0 0 0.9c) Q.000 3.0330 0.0 0 6.03 0,3333

0.U D.....0~00....0.0 0Q03) Q..0003) 0.00.0 0.3 o_____ 0 o G

-UN-BGUN._-- - -------E G

_EGRF = E t O G E I.

SEGMENT.10 I_ _AFU OUTPUT L ~ .. -- .... .UTPUT

S 0 0-0 0 0 0 0 0 0 0 0 0 0 00 0 0 0 0 0 o oo o

0 0 O 0. o. o... 0 o 0 0 0 -- - 0

0 0 0 0 0 0. 0 4Z . 0 0 0 0 0. 0

S 0 0 0 0 0 0 0 00 .0 0 0. .

0 03 0 0 0 0 Q0

0 0 0 1- - Z7T

A .. .. .. -.- I

.. 0 0 1

SUMAP., o.755 UN8 .2

SIIMAP. 2.091 SUM.NAP 0.05. S-AP 0. SUNA. 9 .

-is' FABS ORHEI Pow w AFD

.000000 0.000 0. O O .000 O 00 AB oR 0 000 0..o000 O0. _

* 0 .000 .01 0 0 . 00 0.000 0 .000 0 .00 0 0 .000 0 .0 0 0 0 0 0 _ 0 .00 0 0.000 0 .0n0 0.0 ,' _ . 0 *0 0 .0 0 0 0 . 0 0

0, 00o 0.0 000, 0.000 0.000 0.000 0.000 0.400 0.000 0.000 0.000

0.0 0.000 0 .000 00.00 0 i. , .0(-0 0.010 0.0 0 0.000 0.000 0.000 0.000 0.000 . .. 00 0.000 0.003

0.000 0.000 0.000 0.no0 0.0 0.00 0.0.0 .0 0 ., O.OO 0900 0.0(10 .000 0.O 0.00 Oo 0U,.0 D.ol _ 0.000)

O ¢ -. 013-

. .. 0.000 0.000 .000.... 0o .5 ... 0- 7 7 0.130 a . 0OOP. 0 On 0000 0.0 00 .OO OO O 0.000 O.e .00 0.03

NOWMALIZEP ASOREO POWS0 0-- RALIZE6A, SORd b POP wER AF - 0-0- -

- ,,0.000 0 O .o. ,o0 .... 0...... .0. 000 0.000 0.000 0.000 0.00 0 (.0n 0 . 00 0.000

~ ~ 0.00 0000 k 0'0 ~ 00 0.000.000 0.00 ___ 0.00 0.300 0.0 U.00 OVO O____ 0.0 .00 -

0.00o0 Oo 0.000 000Io. 3 .7 .0 .0 .00 000 030 '.0' '0' .0 0.000

S 0 000 0.000 0U.OO 0.000 0.0N. 0.00U O.00 0.0400 0.000 0.O000 0.000 0.000 0.*000 0.O 0.000 0.00

0.0 0 0.000 0.000 o.00 .. 0.0(2 0.001 0.000 V . - -noQ 0___ 0 0 . ,0 u 0.0 0 0 1.( o 0.0 O o .0 0"

0,0 0 0 0 . o0

. O 0.vn .90A.Oh 0.000 0.000 0.000 0.o00 O.6oU 0.0 ooo 0.000o~~ooo o.,,o _ o-oo -o,_ _.0 . ,,, -.---- ,-- __- - ._o- , . . ... (,.C.o -t..l--_.: o _o-------. -- _-----oL ....---o-..-. o . t~ ~ .. ~ o

UN -E _____ _ -- --OEG-EE-3-....

OVE ,' 0.3 - - SEGMENT0I 3

... ..... ... _EGMENTm_11__

tV ---- - --- - - - -- ------ - - -0F 6 - 0 fU

0 0 0 0 1 u 0 0 1

0 0 AF0- ----

O.......... . ...0 0 2 4 0 0 000 0 0 0 0 0 0o

0 0 0 0 0 2 1 0 0 1 . 0 0 0 .

0 v0- I 0 0 0 9

( 0 0 0 0 .. . 0 2 3 0 1 . .... 0 1 I 0 44 0 ..4 ... .

SCMAP0 2.005 . UOIOP' 0.10, SUMAP. 3.055 SUMNAP- 0.227

0.000 0"01

'0 0.000 0.

f O u 11 .00 0."0 uOAO O.ODU "0.000, 0.000 0.000 0.n 0 0."0 '.03" 0.0n0 0. 91

0..000 . 0.0 0 . 00 0.00 .. .. . .. 0 0.000 0.0 0 . .0 Ono -"O ^n .n. 0 0 0.000 O. 1h O (1 3 - - .0 0 000 000 .0 00 0 000 .~ 000 0 0' .000-' 0.000v .000 .0_ .. .. 0 0_. ....... .0 0... ... ......

O.OO0 0.0(40 0.000 0.000 '.010 .O00 0.000 0.090 0000 1. 0 000 0. 0) .0 0.000 0. 000 6.oo O. s

0.000 0.0€0 0.1(00 0.000 '. O' .0. .. 0 0oU .400 o 0 '.4 0.000 0.00O0 .. 0 1O I.03 v.000 0.000 O.On0 0. t

O 00 0.000 0.0000 Po 0.-, f.oO _ 0. o. . .. . .. . . . .0 000 0.000 0.1o 0 .0 00 0.... .. 0 0 L. . 0.... . 000 .. ..

6.Von ---- ,onno .... .Pon" o.Pon0o .ooo , c g o o.ono0 0.059

NORMALIZEQ ABSORUEU POLN o. ____0 .0 0 0 0 .0 0 0 t • U : .0 (1 0 . . 0 t0 t.: 4 • .494-

0 0 • 0 .0 n0 0 . U 3

0.000 0.00 0.00 . 0 0 u .000 0.000 O.000 -0.0010.000 0.00 _ . ,00 0. k200 ' .00 . nt .. O .

o.0o ... 0.oo . 'o . . 0 - 6-0 o - 6.v . ...0 0.005 0.0000.000 0.000 0.000 0.000. 0.000 0.0.9 0.00 0.000 0.000 0.0.000 0.003 0.000 0.000 C. 0o 0.000 0. 5b,

0.000 .000 0.000 .I.910 0.000 0.000 0.'0 r.. 9 .. 0.1,1 2 __

4MALIZE() AdoORlEl R0400 003PonL .O - 0.000 - O.VO0 . .no0 . 0.OO.. -. 90 . 0.000- 0.001 . .

0. 0.000 0.00 v .000 0 .1 v0 k.,J0 o.JID 0.000 . V I

'k - - 0.000 0.0ono 0.000 0.000 O.O0n 0.U0 u 0.o o 0.0-13

0.000 0. o___ o.oo J 1 . 4 I 0.000 .0

S0.0000.000 o0.000 0.000 0.000 0 .000j 0.000 0.01 1

___ 0.00 00Q---Q..fl-0- ~ 0.000.5.L' 0

. 100 000 ~ ~ . . f 3 0 ~ . ' ~ 043 .3 .n .0 . 3l

RUN-A , RUNafDEGHF F-3 E .CPFr= 3 _ _ . . . . . . . . . .•.

.. SEGMENT=14 . EGEN 16

AF)J OUTPUT o-_AFu OUTPUTr'

0 _____ _O _0 0 0 0U0P0T0 0 0 0 0 0 0 0 0 0 0 0 0 00 0 0 0 a _ .. .. .0 0 P_ . . 0. . . __ o 0 ( 0 0 0 2

0 0 0 0 0 0 0 38 0 0 0 0 0 0 0 140 0 0 0 0 0 8 00 0

- 0

51MAP. 0.495 SU.. NAP 0.003 S..L. .AP. 0.21A Sn144F= 0.001

ABSORBED POOER AFD ... __.. AHSOROOED POWER AFD- ... .. 0.0.0o00 0.0.00 0.000 0.000 u.o i .0r0 0.000 .0n 0.000 0.0(0 0.000 0.000 0.030 .O0N 0.000 0.00.000 0.00 .000 0.. .000 U .0.000 0.00 .00 0100 00, ..- 0.00 0.000.0 .0. 0 .0 0.0000 0.000 0.000 .

0___.000 0.o00 __ 0.000 0,00 0.000 .jr00 0.000 0.000 0.000 0.000 .n000 0.000 G.000 ".000 0.Uo, 0.""0 0.Voo0.000 0.000 0.000 0.000 0 n0 0.000 0.000 0.094 0.000 0.000 0.300 0.100 0.000 0.000 0.000 0.0 270.000 0.000 0.000 0.000 0.000 o.o0 0.0o0 0.oi0 0.000 0.010 0.000 _0.000 0.'00 0.'r, . 0.0010 .077

O 0.000 _ 0.000 _ 0.000 '009_ ,O_ .100 1 Q,000_ __ 10__Q.91 . 0.000 0.00 0.000 0. 0.0 0.000 .0 . 0.000 0.114

NORMALIZED A0so04EU PO.FR AFu NORMALIZED AtSOROED POWER AFu . . . . .V.000 0.000 0.000 000 0.000 f.1oo1 _0.000 0.000. 0.000 0.oo00 0.000 0.Q00 0.0(0 0.000 U.u0 0.0000.000 0.9000.000 . .0.00 0.000 0.000 0.000 0.00 . 00 0.000 0..0000 0.000 .0 0000 .0 0.00 0.0000.000 0.000n 0.000 0.000 0.000 0.000 0.000 0.0ou00 L .. 000 0.000 0.0 __ 0.000 0.Oo 0.0,0 9.000 0 . ,0.000 0.00 .. 9 0 _90 00 .000 0 .0 .1 0.000 0.000 00000.000 0 0.000 0..000 0 .0 0-0.00oU.000 .0 oon.o(00 0.000 0.000 .00 0.0n0 0. o, 0.000 0.010 0.000 0.000 0.000 0.00 0.000 0.0000.00l o0110 O.0O (o00 0.00U .r.v 0..nu 00.00 0.000 0.000 0.00 0.00 .000 0.0 o.000 0.001

NU N=....... .. . . . . . . . . .

HUN 8 - . -FE-3- _

SSEENT.15 DEGREEs3_______ -' SEGMENT-1 7

AFO OUIPUrOFO ((00000I"o o o o (0 0 0 0 0 0 I0 0 O 0 n O 0 0 - ' _0 0 0 0 0 0 0 10 00 0 0 0 1 3

o o1 0 0 0 1___3 -10.0 00 0 c 0 0 J;

0 0 0 0 0 0 0 0 SI tSAP= 1.302 OoEPW 0.0010 0 0 0 0 0 ) 0

0.- ASUROED 0 OWERQ AFU0 I -0 - 0 0 - 9101)010002 0 0 0 0 0 0 5 I 0.000 0.n000 . 0.000__V.0Q0._ 092 .v00 .. 0,f000 ' 0 00000 0 1 0 0 0 . 9 23 0.000n (.f10) 0.,00 0.(0v 0.1/,00 011 0.u, n I 1'h0 0 0 0 0 0 0 00 0.(00 01. 00 (.000 0.,01 .(0 (.VQl'( (10l .. .1)

0.000 ". 0 ". 0 0.:0 "o n Q_ --- - f 0.' ; 'jP0 ' -50.AP 0.340 S 1apA 0.002 0.000 0.01)0 0.000 0.100 0.010 (.024 0.1°0 0. 0'0-00" 0 0.0 000 0.0.00 0.00 . 0. 00 '0.00 0. ur 0.00j

A65()NtID pOweR AF[ *

0.000 (.000 0 .000 0.000 0.000. J.000 0.000 0.0 0 I ORMALILED AtS-ROLEU P1)wt Au0.00 o' 0.0 0.00 0.l0 0.00V J .( O 0.0100 01.00 I 0.000 .O000 0.00 . 00 0D.0.0 U. 0 .00-1 0 .0.001' 0.00 -0.000 0.00% 0.)00 0.0U00 1.0On 1 .0 0 0.000 0.0100 0..00 - 0.00 0.00 0.00 00 0.1,00 1.11o 0.000 0.001I0.000 0 0 ( 0 (1 P 0 " .'n 11 . o U 00 0 0 70.000 0.000 0.000 0.000 0.000 0.U00 0.000 0.0000.000 0.010O .000 0 0.000 0.000 .'00 0.000 . 17 0.000 0.00 000 00 0.000 .0 0.0 0.00C *000 0.000

0.0n00 0.000 0.000 0.000 0.00(, 0.00 0.000 0.lo .14

NORMALIZe) AHS1 bFO PUtH AF)00.000 0.0 00 0.0o00 0.000o 0.000 V. (00V 0.000 0 .000 i0.000 0.(110 0.0(0 0.1101, 0.000 .0 .0 0.000 - 0.) _ _0.00o 0.000 0.000 0.0n00 0.000 0.0n0 0.000 0.0000.000 0.000 0.00 0.000 0.00 0.11t 0.000 0.0000.000 0.000 0.000 v 00o -. 0- 0 0 . . 0.000. .0000100.000 0.000 0.000 0.000 .00 l ,00 . 0.001 000 .00 0.000 .00 0.0 U 0.0103 0.

" ,. . .0.000 1. 000 0.0l 0.o''0 0 0.0 00 ,. 00 0.001 0.0(00

RUN 8, DEGREE 4


degrees 3, 4, 5 are degrees 1, 2, 3 for center seat'.)


FACTORS ARE

0.0008? 0. r0f330 0().001325 1, 0 15631 .0 0'460 .21 ,C, 0.]4590 0,03647

IMPLITI.IDF LEVFLS RE -SFT 4T

,03 0 P 0.e 0. 13 0,21 ,.32 0.50

PF0J0ENCY I F\/r1tS AOE SFT AT

06 0. 1 .25 0.50 1. 0 .00 4. 0 .00 1 n

CENTERP AMPI TTUFS AkRF

C 44 0.0R ).. 0.r5 .0* 7 C I/4 1

.FNTF FPFUNjFMCTES APE

. 88 0.177 o.35+ 0.707 1.414 2. I .657 11 .314

I A.1MUM PcSTI..

LF COUNTS PEP SEG.T

1.326 2.63' 5.3 3 10.607 21.213 4?.4 84 53 169. 705

*SOPRfD POWEP iATkIX_ 0.06382 .. ,iLo2T46 0.11024_ 0.q1 Zn467- 10.10910 12.143'4 3.03440

0.00281 0.," 132 0.04r 3 0. 3 0 .+35+ 4.1625. 5 ,00465 1.25056

I-.00 11Cl5 . 72 a 0795- . 341-5 .1.71703 2. 0256 0 .51539

0.0004 0.0012 ,.n077) 0132 i< .14326 0.70764 0.1? 04 0.21241

0-Q:0C } o' ".0 ,0-31- ., l -35__ Ce C59- .- 91 -, 3533 1 0 08675'4-

On 0 0.0003 0.00131 0.0P5 '.( ~) 0 )12019 0.1&-432 0.0(3608

NO _MAI.. T AHqPP !) Pol-P ePSr000 -15 .01015 0_02 7.9._ 0 441 7 ?.- 9 I9 - 2382 0 ,31),1 0. 17P.c

0.00212 0.0042 7 .00Q57 0) 8I 1. , '307F 0 .*f 20 0, o 89' 0.007/3

~0.0~ ~__-._1,A 0 . -3-5 -.7c:, , -0 i: -0.04047 -. 0 24. 31 0o 0304

"0.0O0' 0.00072 .0Cl1+4 f.r, 9 4.,0675 ( .160, 3 .oI]0'? 0. 0!25

.0 000 15 . .0 3': .. . .0 6 .. . 1 7 . , ?)7 ._0.0687 5 00- 1.3 0.00052

0.000 0.00!12 9.00) 2 t. C ', 3 ).00i1 0. 10283 e, l 1 0 0.00021

E-107

7,'- F I0 =4- . ..-- - . SEGMENT= 3

- - --.. .AF) - -DU T ---.. .. .A

1e.. .. .. L. . . . . ... . ... . . . . . . . . . . . . . . . .0 A 1 2 9- 0 39 . ...R0= 0 ( 3 0

PF, -RF I - 2 8 9 45SF ENT= 0 0 1 1 3 9 7? 23A.4. . .- - 16 . -- I . . . . .

AFD OUTPUTS .R.MAP=17 .051 SUINAP

= 1.951O. ~ ~ ~ ~ ~ i -0 0... . __ -"A 5 . . HS R FD_ P nER F )

. -2 1 0 0 0 . 0 . n 51 .- SO D4P 0 .A- - I 0 7. 0 0 . 0 0.000 .469 0.000 3l 10 9 12.143 ?1. P4

0 - 0 .- *1 0. 5 3. 34.. '42 0.00 n .0 0. 000 1-bd.-4063 .7 ..7 .Q 30.97??0 0 1 0 8 20 7 0.000 0.00 --- 0.00 0.033 . 1 77 - .5. 1 7.60 0. 9

SIIMHAP= 91.7P6 SI)MINAP= 0.765

ABSORHF PnwFw AFn.. 0..000 - 0.000 . 0. 00 0.0O.O . 0.000 2.000n 0.0;0 3.034

0.n00 0.P0O 0.045 0.193 0.000 0.0,0 0. 00 n A. 76q1) .. - .0090 -. 019... . 0 L . D 0 . .. O ..0.000 - 26.2b5 . .... -0.000 O nO. 0.000 0.033 0.143 ),70H I. o00 14.89 --

S. O.c0 0.000 O 0.003 0.700 ..295 .b75 11.931 3.t77 . A.. .0.000 0.000 0.000 0.r6 0.000 0 .9O 4.17 0.6)3 0.000 4..07 '0.003 - 0.04 -. 177 n.4.'7 7.707 .013

--- -a -- -n -o - 00 r --. L.- .n -1..2.2- ..3 10-- .f6NOPMALIZFn AP apsnP ) PnwER AFD- 0-0 00 - -. nI-- - cOOO .. G __.o . JDO.. .O.000 ___ O. . __ 0.91082-- NOR'AL F. .u. .o.FR F00 00 O3. h 00609919.)) "

nO O On o 0noo 0.009 0O IR A nA0

O 000 ..ooo 4 .110 n.34 .143 0. 375

0 0 : .n O t)e . O.nil O. lf 0")OIR .oO,/ O.OAO 0, eA70000 - .. 0 0 , 0 . n 000 004 o A N000 00.000 .00 0.044 0 .000 0.3

0.000 0.An 0.00n 0.0 0 1.000 0 A 0 0.000 0.1 -' 0.000 0.° . 0.07 0 19 .0 00 0.001 - 0.. .. 0.0 0.004 0 0 0.00 0.017 0.0 0 0.0 u a o , L 0 0 5

0.000 - -00,0 0 077)l . 0 0 _ 0.1 . 0, o . . ..... f OnoJ.

0.00-0 .. 0000 .. 0.01 0.000 . 0.014 0.0 1 O.'O 0.07?2 .nn 0.P0 0.0 -0 0 v ..1.1,. . .0o0. 0.056

rDE GRF F 4(1.0 0.1120 3. 0. - - - - 3 0 - - . LO . . ...... .... .. .. . . . ..- A . ....

0 0 0. 0 . 0

0 3 0 0 0 0 q 0 7 0 0 0 0.... " .0 .0 0. .. .0 _ 0 0 OS . , .7- .-- 0- -- - . . O L .. . .. .. .0. . -. ... .. .

0 0 1 0 4 0 3 35 0 0 0 0 5

S 0 0 1 .0 3 . 5 19 13 1 0 0 0 0 0 0 540 1 03 .0 0 0 0 7 75- 0 I- - - - .. . . - - - - -n . . ..- .0 -0 2 0 39 +1

S1100009.197 SU0.1P0) 1.474 , SUIP-3 -8-- .... MNR .R.A

AR50P0) P0,00 Ff)

0.000 0.000 0.000 0.000 .0 00 0.00 60.68 BS03FDPoFR AFD.. ..... .

0. 000 0.03 0.000 0.000 O.07 0A.0-0 0.0,0 93.79?

0.002 o.. OLn._. 0.000 .000 .. 0.002 0 -..' 0.0003 23.J4

0.0 0 0.000 0.0 2.000 0.73 ..0n 2.50 7.4 4. 0.000 D. 0.000 ._ 0.003 0.000 0.177 .0 6.616 1.138 --

0.000 0.000 0.000 0.0 6 0.iPP 7.6 a7 .oV3 0.21 0

01OMALT7EI AH00PtAFIl PoMw9 AF11 ..

D_. 00L .- 00C0_...0.000... . 70. O ..O .1 0* ' 0".a 0.000.. - 0,35 --0.000 0.004 0.000 0.000 A.0 Qo1 1.00 0.000 A . ;7;3 .000 0.000 0.000 0.000 n.000 0.010 0.0 0.000Uo

0.002 0.000 0.00 0 . 7 7 7 0 0.00 * 367 _ .0.000 .1. L .0- .0l0_ _ .00 _. 00A10-7 a ..O . ._--0.00O 1.2 510o000 0.0"10 0* 0| • 0.oi 0 000 A. 1)7 . h 0 On A"I O. O.L , A r, 0lno U; -) . 1111) 0 (. )h) ,)~d

0 0 0 ° 70.00 0.000 0.003 . 000 0.727 0. 00 0.01) 0.044 n A.0000.o0 0.101) 1.700 9.1)70 .164 0.000 7.471.0.000 .. 0.000 0.100 0. 010 0.790 .0.:34 0.0 - 0.707 0.00n .000 .0.010 7.000 - 0.000 - .000 0. 7 1133.420

.On00n ..0 0 0,00) 0.0 I n 00. (0. 3 0. 0 0 A.00' 007 0 0,n000 A.n3 0 - 0 . O0 ' .4,2 456.2

0.000 0.no00 0.000 0.100 0.1)"n .QAO 0.10r. 0.f10S0.000. -0.000 -- 0.000 . 0.010 0.000 C.11C 0.Oo. 0.0v70.000 , o.n,? 0. o 0 .0.0 f.170 .. , , .000 0. ;150..O OO-- -- .0o0 -- .00 0.000.. 0.00 .. o 0.00 .O.OnO 0.0680.000 .0n7n 9.001 0.000 0.100 O.1,0 , 7.070 7 .039

--ngeRFF.4SEGrEN2r 7

AFO OUTPUT0 . . 0 . .0 - 0 . 0 .. . ... 0. 4 .o 0 0 0 - ' 0 0 35

............. ......0 1_:- 0 -. 0 . .. 0 0 ..... . SROII.R I 0 0 0 0 0 3 53

,F1 F NT. 0 0 A 0 0 5 8 36 13

AF)) oU7PUT0 0 0 0 0 0 0 3.n n 0 0 n ?0

I 0 0 0 4 3 6 63.1 0 _ _ A 0 1 . 6 10 ._35 . -. . . . . . . . . ...

0 0 0 1 5 4 30 17

10001P= 96.71, SUMNAP. 0.71 "t0IMAP0I 10.435 SUHmNP. 0.754

ABSOPF) onFO I A SO0UP iFn 0 0 0PoF- Arr

.0.000 0.000n .. 0.000 .0.000 . q 0 S . 00 0.0 0 9.103 ..... 0.000 0.0o 0.000 . 0 000 - 0.000 . 0.n0O . n .0n, I.3 -1 -1.000 0.00n0 0.0

0 0.000 i. 0.000 0.001 0.000 25.011 0.000 0.000 0.000 (.000 0.0n00 I.,00 0.000 43.7700.000 - 0.005 0.019 . .000 . 0.0o00 1.717 O.OnO 25.770 - ------ 0.00 0 .00on .. 0.000 O.000o 0.000 .. nno 0.000-. -2..2R50.000 0.000 0.000 0.n000 0.73 2 P.173 . o00 13.392 0.0n00 0.000 0.000 0.000 0.000 .000 ?.on0" I I .?

__._0 L 0 .0 P-..... . ft. 0.0 3 _.- .. 0.000.. . .003. 0.00... V..I.- - -3 A .5 4 .. 2.39. .. .3 -..0.000 .000no 0.000 o.on06 0. I?? 0.491 4.31 0.613 0.000 0.000n 0.000 0.000 0.10 .342 . 9Q *.4.9

NOPMAL .7Fr A"SORFO POWFZ AFl "

NORMALTZFn A0s0nwHFr P(!WF AFt).... 0..000 .- - .0.070 o 0.000 . 0.000 -0.000 0.000 0.00 ... 0.054 0.000 .... 0.000 ... 0.000 .0 00.... 0.000 . . 0.000 . 0.000. 0.97 ..

0.0nn00 0.000n 0.600 0.000 0.000 0.000no 0.0o0 0.147 0.000 0.non 0.000 n.nnn no.00 ,10ll 0.0(0 ,A,

- 0 c 00 0.PL, . 0.I.00 0..0') 0 .U( 0,.J.1ni 0, . . .. 1o20 ...... .. 0.. _. 0.000 .0.;100 l0.00 0.0,0 0.000 0. 1550.0nn 0.000 0.01o0 0.0( no 0.0 ,,'7 . ,i n., ., t on. n .00 no .0 ..(10 .0 0.0 .0.000 .0.010 0.0*00.000 0 ..... 0 OL 0.000 . 0.003 ..... 0941 . .041O o. 0.0 8 ..... .. 0.000. 0.000 0. 001 0.000 0.000 . 0.014 0.0,4 0.015 _

0.000 n.000n 0.000 .00 (n 0.00; 0.011 0.001 0.o 0 4 0.000 o.0nA 0.000 O.000 0. 0J. 0i.3 0.061 0.003

.0UtlaR ..000..... I R-.SFMENTI 6 SF ,.ru T

. .. .. . AF OUTPUT0 0 0 0 0 0 0 0 0o

0 0 0 0 0 0 0 0 0 0 0 0 0 0 0

.0 0 0 0 0...0. 0 0 29 0 0 0 0 0 0 0 701 0 0 0 0 0 2 5 1 00 0 0 0 20-.-...- - -- O-- -- - -0 ...... .0- . ......0 .... . . ..... .9 ... 3 , . .. ........ .... i " 0 ; ;

o. -. 0 0 0 0 0 0 5m

S-AP. Ia.3?9 .... SUINAP. 0.120 SUMAPs 6.031 $'VLAP= 0.036-- 3(00 0.3(0 -- -SUINO. 017 - -SlOP. 6.031 SIAP- 0.036

ArlsokHrn OnWVW' AeM ... .: :. . All RB I poW.FP AFnkl6.on no000.0 000,11> AF."o n-ot n-n .~o, SoOWoIr) 0 o1>f 0.0n0o 0.000 6.000 2.h002

- 0.On( 0 ".00 0.00 o. 0.000... 0.000 0.000 0.000 0.000 0.007 0.0,0 0.000

0.00 .. .000... .. 0 00.(.00......C.700....0.0iL. -U.0. ..... 0.000 0.0 00 0.000 0.n0 0.000 0.0n1 .00 " 0.0o0.000 0.000no 0.000 ".no0 .. 'a' 0.In00 0.000 3.00 _ _0.000 --- 0. 000 .0.000 ....... 000....... .6 0 .. _. l. ...... 0.000. 0 .......

.....0.00h 0.0.00 00.00 0.000 .000 .0.000.. 0.0o0 A.160. 0.000 n one e 0.nn 0.0I0 0.D.0 0.0,0 1. 480. 0n o n. 0.000 o . 07.00 A.00 0.000 (.000 .. 0 0..r0 .. 4IA

.0.000 - -O.O0.... 0.000... .2 .000 .o 0 .Ooo .. 0.00 I. .S0.0nn . 0.0-T ... 0.000 ' 0.00 O.0b .. 0.n00 . .200 . 0.910.

.M _ _ ...... ... -.N IOA L IZEOO--I3 SO0 Efl.(!0(2O C.F >L- i... - -. __

0.1(00 ((.00 n 0.0I0 nj (' O -p P.00 n.060 n.000 0.00.10C.000 0.00 0.000 0.100 (.000 0.000 0.0no0 0.000.000 0.no0 0n.o. n O.e0j 0.601 o6. ..00 0.00 0.010 F8e 0 000 .0 00

.- o.00.... nO.o 0.0o0 0.000 .0a.... .0 ' .. .0no 0.036. . . F .... ...... . .. .. .0.000 o.on'0 0.000 0 g . 000 (.o , n I o. 0 ) . n 0.070,

0nnl nnn p 000a .-10 U 0.000 0.000 0.000 0.000 0.000 0.000 0.0012 ?.0,)2-

I NOPMALIZFf ,.S(rO'Ei3 P00)0E AFIIo-0.00.. ... m.oo ..... 00 - .nn0 . 0.0 00. -nno 0.0 . 0.00 n

S 0.000 0.000 0.000 0.n O r,. 2 0.o0n 0.0. q r.00 .O.On - -.. 000 - .0.000 . O.nno .0.0. . 0.0.0 -- 0.000n O .8 -

0.00 . .00 0.0 0..00 0 .0 -0.. 0.000 ' ., 0.f.09

.0..0.:L .0 ..O 0.000 0. .... 0.0n0 .o0.000 .... 0U.01.S 0.000 ((.000 0.000 0.000 0. 00 0.0(1 0.000 u.OIO

nFGPFF.4

SFGMENT. 9

0 0 0 0 0 0 0 3.0 . 0 0 0 . 0- .0 0. .13.

P0,11=8

SEGmIENT l 1

-- - - -- _ JFD..OU1.-PUT,t0 0 6

0 040 0 0 0 0 0 0 3

•0 .0 .. o-----2---- - . .. ...... . - 0 0 0 1 1 -3 35

1 0 1 0 0 3 14 4 6 1 0 0 1 7 I '?

. 0 0 0 0 ; 26 17 -.- 4_ _ . D......." ..... 5 ...... 7 ._ 2 ... 44 ... ... -

_ . ;300P 0.364 . $S.NAP= 0.59P- " Su-AP= 38.173 SUINAP= 3.321

BSLRBED.POwE.-AED .......-- -- -.----.---- -RD POWER AF

0.000 0.000 I 0.000n 0.3 0.000 0.0 .On0 0.10q3 0.00p 0.000 0.000np 0. ro00.0 0.00i0 0.00 0.0)0 ). In3-. 0.000 0.000 0.00" 0.000 3 .00n C.010 0.000 1 A. 257 A.Q______0_0_____ Vfl0- 0oe. . 3... 0o000 .. 0.0n00. 0.000 0°000 0.00f .. 000 0.000 ]0.2.7 -... D...L...0 .0.000... -3.000. _ .3.000..._ 0.000 . 7.503....

0.Coln 0."00 0.000 0.000 .An0 0.00n .00c 74.2m4 0o.o 0.n0 0.Io0 0.000 0.3- 0.On 0.000 1. 031

.0.0O0 . 0.000 0.000o 0.00 0.000 1 .41 0 1 .700 11.0tH2 0.000 . 0.000 . 0.300 - 0.00U 0.143 0.1i 2.5 0 7.43.0.000 o.on0 0.003 0.00 oo0 0.0n 0 0.87 4.9nb 4.07f 0.000 0.000 0.100 0.014 C.l 0. .o 0.300 0. 4,7

-- D. - .a0 .L.-Q - 0 --

O0

.A- -

.049 _

3_

712.

3-

- - -0.7

r4 _ . 0

1 3 . .000 0.00c__ 0.000 0.017 0.122 C. .1 .. 0.2.9 1 .587

NOO1ML! I A'O SlIOFII FO1[4 AF00 t2. IlMALI LiJ) AHSI'LULU .U . AL) ...0.n 0 0 000 0.00 0..00 0 .00 0 0.01 0 0.0 00 0.04 0.000 0.000 0.000 0.000 0.00 0.00 0 . 0'oA 0.054

C. 0.000. . 0o0 . 0.000 . 0.000 0.o . 0.030 0.0n0 . 0.006 0.000 .. 3c00 0.00 . 0.000 0.00 0.33 0.00 1.04.

0.000 0.n? 0. 00 0.000 1.0 a0 "1.00 0.00 0.149 0.000 0.00n0 0.000 0 .00 0.014 .0 0 0.0,00 0.006

_ -tCl a0_ (. Q0 .. _0.00- - . C 3 0 C..... 033 0._0. 00- ... 0.61 . 0.000 0.000 0.000 0. 00 0.°07 .017 0.310 0.0*

0.000 0.000 0.01 0.000 o0.:)00 .071 0. . 0.004 -0.000 0.000 0.00o0 0.001 0.01q 1.017 0.004 0.012

. .000 0.000n 0.000 00110 0.00? 3.017 0.044 0.0.4 -.-- - .... 00 . Po. _ 0.00 0.302 3.356. .0)0 0001 0.009

Y.UN S .. .. EGE- - -- _

--- - -.. . .- O---- - FUNP

AF1 OUTPUT 000 OVlOJO"0 0 0 0 0 0 0' 0 . .. . ..f.l -. 0 00 0%00 0 0 n 010 0 0 . 0 0 0 0 0 0 0 0 0 0

0 0 0 0 2 1 0 39 0 0. .... ....-.. 0... ..0 .. .... 0... 5..

.. .. .. 4 . 3 _ 6 4 ... 0 0 0 0 0 0 10

0 0 1 4 0 0 - ... 0 . 0 0 0 0 2 0 3 27

0 0 . 0. 3 3 13 23 24 .4

SUIMAP. 70.627 - SU:NAP- 0.757 SIn,0P0 11.614 SIVINAP- 0.003

AUOic r)F~w~? F AI,,, (11-I l P1,11 -- A~fl

0.Io0 .Ppo 0.000 0.000 0.000 . .0n 0.00 0.00 O.000 0. 00 0.000 . 0.000 .000 . 0.00 0.000o - 0.000

0.000 . 0.00 . 0.000 . 0.000 0_.3 _ 0.00 .,O3lo , 10.034 o.000 0.000 0.q000 00.00 0 00 n 6.00r0 0.100 I .,,l

0.000 n.0on 0.000 .000O 1.9 1.717 0.con 71.100 _0.000 . 0.000 0.000 0.00 .00V0 0.0010 0.000 2.577

0.000 0.000 0.000o 0.000 0.573 P.1 01 5.100 r 9.346 0.000 Aon .P.0 P 0. a3 I0 . . G 0. 0' ?.1?4

0.000 0.000no 0.00 0..1 (1 001 4.. 0 a, 6. ",3 6 1.414 .0.000 .. .0.00_O .. 0. 200 . 0. 0 U 0 1.____-C0:o ..1.01 1 1.364

0.000.. .0.000 ... 0.000.. 0.017 ... 0.073 1... .55 3 4.043. 0. ..01 0.000 0.000 0.000 0.000 0.12? .2.O .0.0> 1.04,.

NORMAL 10010 090000013 P0,09 A0NORMALIZED ASOBED POWE D 00 00M0 0 0o 0.300 3. 0.000 0.000

S0.000 0.000 0.000 0. 0. 0.000 0.000 n.Ono 0.00?

0.000 0.000 0.0O0 0.o00 0.000 1A. 1011 0.009 0.0130.000 .0.0-0 ... 0.000 0.00 3.006 3.030 0.012 0.01'

0.000 0.000 0.000 0.00. . 0.000 0.006

0.000 0.000 0.000 0.000 0.030 0.000 0.000 0.00

"_'"-.0. 00l0.L _.0.f0 0.0..00.0 .- 0....,000.- ...0..0.00 . .0. aQ.. . 0..... 0 __0.010. 000.19.. .

0.000 0.000 0.000 0..00 .0A11 0.n0. 0.000 0.11u

-- ~~~~~~~ ~. n ..0.n n n on-- .0' . "n-o 1.00- o", n0 ._ 0 .... 0. -- -.. GM.. O n .--- 9.. .

0.0On 0. no0 o.n00 0.11no 0 O.011' A .040 G.Onn o . 18

-.... 0l00 ... 00.-0.001-.0.000. -0.0d 0.0 - 0.0.D 0.0050.000 0.0n0 0.000 0.001 0.028 0.006 0.074 0.0700.0On .. n.nn0 . o0.000. . 0.0112.-.003. 0.017. 0.0t48 . 0.00oq

- - -- - - ----- AF9_n.OkTPUT. -000000000- - - -- &-- --- I -... .... . .........W.P - - - - ....

0 0 A 0 A 0 0 0

0 1 0 0 0 0 0 580 . ...0 - 0 .. 2 . 0 .. .. 0. . - . -1 0 0 0 5 3 16 52.. - .. .. 1. . . .. 2 ... 6 -... 31 16

--- - - SUtAP:_60.3.90 ..... 5U NAPa.._-0.5 ... - -. __.

. . .... ....-. .-- A SORBFr. PoWFR AF .,. . -UN-.-.. • . . . .. .0.000 o0 0 0.000 0.o A. 0.000 0.n0 n 0.0-0 0.000

FGPr-.4 -.. 0.000.oNn 0.000 .0.0n00 . 0.000 . 0.000 -,0.0 0.OO . 6.253.... . FGMENT 13 . .0.00 0..n0 0.000 0.0o 0 G 0 .%no 0.000 ?9.093

S00---.0---00 0.000_ 0. . ... )o0 J1.000 15. 93....

0A.1-D-LIP J 0.000 0.000 0.000 0.000 0.,Or .875 5.6-5 4.,20 0 0 0 0 0 0 4 A . 0.000. 0.o . 0.001 0.011 .0.146 .. 0.771 4.476 0.577

.... 0 -0. 1 0 0 0. 0. 32 .

0 1 0 0 0 0 0 7 -NORMALIZ ErD.. ASORHbFD POWEP. AFD .0 --- 0- 0.... ... - -0. .0 49-- - 0.000 0.000 0.000 0U.mQ 0.006 0.000 0.000 0.0002 0 0 0 4 0 5 289 .o...................f.0 0 0 .1nO .O0. . -. . .0. 0D a-0 Of l s a . .00 .0. 0 37

.. .. 0 _ ..J-... -- L . 3. L.3. - 0.000 0.0n 0.000 0.000 0.00'l l.1.A 0.000 0.1760.000 .. -00_nO_ 0.000no .0.000 . .0.014 - --0.03 0.00 . .0.090

. StiMAP421.463 -...... SUMNAP 0.69. 0 0.0 0.000n 0.0 0.10 . n0. 0.0.14 (.C01 0.0.6 1.021.AHS.O.B>F-.P .I.F0 0.... ... .. 0.00. . J.0.. . . .. 0. - a -"

.A11SO01101. PlttwF1 AFO- --. - - .- -- ____ ____0.000 0.000 0.000 0.000no 0.000 .00n 0.000 1 "118U

... 0.0 .00d.0.L...0.04. ... 0.0__0.300 ------ .. .. 0.000.40.08 __ 01. .. 10FAOPFF4 -

0.000 .no 0 0.000 ( 0.1o 0.000 0.0 0.00 30.6A5 S l.;Fm NTI6.0.000. .... 0,an0O 0.000 0- .033 0.573 ... 0 0. 0.000 10.408. .0.000 0.000, 0.000 1.0n00 0.236 C.O0 8.7r6 2.4. AF ()oUTPUT

- 0.000 - .0.000 .0 01 0.000 C..170 - .8 - 5.611 . 0.469 .. 0 0 A A0 0 2 1 0 1 1 20

N.. . ORMA L t IZED .- AAS flE D.PO ER D. . . .. ... - . .. . . 0 --0 . 2 o1 3 61 .... ........0.000 ,n000 0.00n0 0.00no0 0.000 0.000 0.000n 0.070 - 0 1 0 0 1 1 3 720.000... 0.000 . 0.009 0.0 0 0.0 0 0.n00f ..0.O0no 0.236 .... _1 .... .0 .....1 3. 7 15. 3 -0.000 .no, on 0.000 o o 0n .1 n 0.000 0.44 U0 0 I ' 5 0, 140.01in 0.11,10 0.1100 0.1)(3 0.02 ? 0, U 0.00A1 0.061 ____.__.0.000f 0.000 0.000 O.1)10 0.011 0.n000 O.|A3 0.014 Rt 0J4A Pm 34. 244 SUMNAP. 1.4A6

-...... O.00.. --. .. 0.001).... OO .... 0.3.0... .00. .020 -.. 0.006 0.003.....-..... ..In q- -AHSOPPFf) PofFP AFnt

..... 0.000 . 0.000no 0.000 .0.469 0.000 10.10n9 12.143 3.034

RUN. 001A 0.000 0.000 0.'91 0.1IY 0.0oo 4.1,6 5.00 2.(,011n_ FRFF_ _ -___ _0, L - -... .. .. _ . .o ..... 0. 000 ..... 0.695.. ..1 ..... 6.lA . 31.439-.

S MENI- ............. 0.00 0.r 0.000 0.00n0 0.141 0.7.,f . 00 19.2930.000 .0 0 0. . 00.000 .014 .0.117 . 2.041, .5.25, .2.601

..... AFD OUTPu T- 0 000 0.000 0.001no 0.1111 0.12 0.6bn1 3.7l;4 0. 500 0 0 0 0 0 0 I

. 0 0 0 ... 0 .. 0 . 0 ... 0 -. 8 ... NOMAL6IZF1 A0SORPIFT) POWER AFF00 0 0 0 0 0 0 4 9 - .- .00-0-.OO. . - il01 -. .0 0 0 . . ., q * .. ..0 0 ........ 0 3 .... .0 . 14 3 - . 0._1_.

0 A _ 02......-. . .. 0_ .. 76_. 0. 1 7 0.01H A. 00 r.040 0.0 9 0.1i 7

0 0 .0 0 9 0 2 44 - .. 000.... 0.002 ... C-00 0.000 0.033-. 0.040.. 0.073.- 0.1,5 ...0 0 . 0 0 8 4 40 19 0 .000 n . i 0.000 0. 000 0.not A.017 0.i10 0.011

0.000 0 .00n 0.000 O. t,1l 1.00i 0.048 0.002 0.017. ... SIJMAP.73.493 ... SUMNAP. -0.559 .. .. 0.000 0.000n 0.000 0.0A1 0.00 0.014 0.014 0.003

AESUROED.2O .IEP:AF ........ .. . .. . . fWl rF.O.0on 0.n0 .000 0.000 0.00" 0.000 0.000 0 .00n A F

- 0.00 - 0.000 0.000 0.000 .0 0 0.00no 0.000 10.004 .. . . ... 1.1..i170..... ....... .. .

0.0on 0.000 0.000 0 o. no u. 1r A0.1 0.00 .254

0.000 0.000 0.000 0.000 0.000 0.00O - 1.70 . 14.143 - .AFO OUTPUI.

0.000 0.000 0.000 0.000 0.790 n0.o*1 Q.108 3.05? 0 0 0 0 0 0 0o o0.0..__0.000. 0..000... 0.000 _. .- ...4A 1 .. .775. S i . . 0 . . O .O. o 0.. _ 0 2

NORMALIZF AHSORHED POwEH AFU 0 n ....... -.. . .. 3 . .. . .3 .. 31

0.00 n 0.000 0.000 0.Oo00 0.000 .AO O00 0.000 0.000n 0 0 0 2 1 8 9 710.000 "0 0.000 0.000 0.000 .0.000 .000 0.000. 0.059 .0 0 . 0 0. .. 11 16 43

0.00n 0.000 0.fn00o 0.001 .o01 .Ono 0O.00 0.149

. .D0o - - . ,0 O - 0 00 -- . . . . 1.0 0 .. .. 00 . ..- 0 0 . . S AP 44.547 SUMNAP. 0.447

0.000 0.n000n 0.000 0.0,0 0.01 . . 0n0 0.107 o0.03 I

... 000 . .00o ...0.00 000 -00 .0.00.. .01 0.068 .0.004_ --__ SO . _Ar __ __/EP........... . -.....0.000 0.000 0.100 O.00O 11.001 A.6no .0n .01no*00 0.0 0 .O /0 0.' .00 .000 0i..002. 0*... .O032 1 1S0.

0.0on00 0.000no 0.00f0 r.- *, t77 n.1 ..:3 I.b .3', . . ./. 0 __. . .( O anO 0,.000 0.Or0 0.430 .0q0 ? .5; I, .58b I

----- _G0 on .,00 _O.0o-.0. 0. .2'.2_ .32 _b2310 . i .....

-NORMALIZED AO)RHED POIEP AFL ..

0.00 0.00 0.000 0.000 0.016 0.0 40 0.000 0.0,

0, -.0.-., .. 0. _ 0.0 0 _ 0.,000 . 0.62 .0..03_. _.10 0.0"0 . _0.0390.000 OAn 0.00 (i00)O OCa 0.000 0.003 oco ao .1 0.011O.Onn n*. A0 0 n .OA00 O.on3 o . o A .0 t A.0>7 0,0lI- -n .. o .a00 0.000 0.000 OOOft 0.1'1 0.0::17 O.Ony

RUN 8, DEGREE 5



K F~iCTORS ARk

).015740 0ue6407. :931 . .0 , 7H SA. * 6, 2.. oi 'od Uo00022900 0.003500

AfM-'LI f .iF I. \EV L S.-T ,I

o0 L. Do / . .,1 / 1t o[ >,' le, .J J

0 . _ kU .1 ,-4u S - -I I ULI i) I

oEN_, R i l I T E,'( S ut

J 04 -l 4 L 1) U i'! I. 0 S*0o00 ." 0.17 7 '. ,. 4 :,-+ O, .37 1,4o~ / o"- ' . o:', . 1,, 51

MaA- Y'J|'UJ " F SSI Lr. CUU,,:I-S IPr_ br ., ,'.

U,",'.3')73 ,b1 ,:-97 ) , %(r' cc, '."-". ,/o; 1 j,,', 1 '%o2-s, M ,,'b3 Uo Ir'0A

UQU 222 / O ( ,. 3I'L¢4 ,( ]1,. .''J."c!, '.'.,-'. . L € ( :.]. )eL J7 O.']!'':{ I

S . 3 7 3 (d J0 .7' .3c 'i : ol -; . 2,- / 4 0. 9 14+ b ,+4 t 11)1.. ( !,:) -e)d l J. ((-13 r'30 u ~ nU 30 o 3 T Io.I.379 , 6, 1 o. -d ' , , , .50300 0.05+97 U3U 'L.uo j%5/ , o . ' 3 ] Uol?' - o ,. , u 0 31 33.,

.0 I 7 n C3 -1 o - 3. 31 u7/ , j t.-2 . 0 3,:

U'-..7" -A Q B P 3 ;o 3 " ., -i .it i; } o A1

6 " t '7 7 l; - 4 .r ,.3 , . .- / 3. ' C I. ?" j U,, .0 +0 0 14 2Z 3 c03'+ i.:: . 2u ' ';I ;c? U 0 /1(,777 & 1l12

0'o06,9 14 b le,, T:-, . o3'+-,cdi o. 43 -. ,: ,.',,01 /33" ,:0,:, j./_ . ; ,, l i-L

0 0 0 Uo1M' 1, 9 5 7.1 utjil z, r w , C U,000 !74 ,, / b,, t .( , ,,,, r" c.. , ,, 29< ou,, ,.,(. : -11

E-112

RUN 8ot-EN s -- -00 -

S'GMENT= 1

... ... . ... .AFQ OUrPUT ....-

0 0 0 0 0 0 0

o 0 0.0 0 Q ( . RUN.0- 0 ~RUN DG 9m

o . - - 00 00 0

1. I 0 0 0 0 0 0 20 - -0- -

, 0 0 0 C 0 0 4 06 S. A -... .

.. 0 Q. 0 . 0 0 60 _ 5 .M O

. 2. . . . . . .. . . . . . . . . . . . . . .0 - - AFO ou T~ u T

SIJ0 AP1 9 8, SI .0 ,AP 00107 .. . .. 0 E. O 0 1..

0 ... 0 ---- 0 - .

0 1 0 0 0 1

00009R1F0 P0000EW - - -0 0 0 0 0 0 0

0.000 O.nO0 0.000 O. OO 0.00t 0.000 0.000 0.000 . . 0 . . 07. 0 _ ._ 0 0* . 0 - 0 0

.000 0.000 0.000 O 0 0 _ .000. 0 .. .000 . 2 0 3 0 0 0 9

. ..0.000 0 .000 0 .00....* O.00 0*0 -0 0 0 0 Z" 45

0.0. 0.000 0.00 0.000 u .0U0 A.0 0.0 0 0 .40 .0* O* 2 0.0 O.cO0 .000 9.n0 J.02 UP 7 . -- .0UMN8. . .. 7,1 1.452

0. 00 0. 0.0 .00 ( 0.34 0 0. 11OO0 0 00 0 00 0.000 0 O 0, 1 . 0.000 0.0000 .00 2 ABSO 3ED . AD0.000.. 000. 0.000 0.000 0.000 0.00 v. .. 0U0 0.000 0000 0. ,17 0.000 0.000 0.000 0.000 0000 0.00

0.000 0 0 0.000 .000 .000 0 00 0000 0.000 0.000.oo, . ,1 .. . J .. .. 00.,_ . .00. _. 1. -.o

-0.00-- -- _*0.092 0U 0 0.000 0.000000 0000 0.00 0.0 0 0.00.. 00 0... ... ... ... 0 ...00 1, .E0.GC 22 7 O.0 00OOu 0.000 0 33 __ ( V )

OFOOU U 00 0 0 217 OOV 0 0 J0 0 OJU 0. d

0.0 0. 7 co. 0 U - .0L o000,v 0O

NOORMALIZED A0F 0 O wF1 AFU

S-w -.... .0.0no 0. 0.00 0.000 . '0 . . . '.. 0 . .00 .00 . 0VO 0

S0.00.000 0 .9. (.0U00 0.000 0.000 0.000 0.OnO 0.000

S... ... . . .. ... . . .... .. .0.000 (.0 00 0.000 0.000 U.0 0 3.00 0 0.000U 0.001

0.000 0.000 0.000 0.000 0.0 0.00 0.000o 0.001 0.0690 .. 0.000 -0-- 00 .O_ Ve 0U0.000 .000 . 00 . .

0.057 0.000 0.420 .00 ou0 U.ou 0.0O0 0.004 0.003

-- D 0 9 0- 00'0 ---. 90 Q- 5 00 -Q. OV - 0. O~?' -0.000 0.049 O.O23 0 .777 0.000 0 .0 00 O.u 13 O.Di229 0t~q__ 0.00 ..... ,p00._ _0,G00. _,.000_0• ,0..;L0Q0 0.0 _00..0.0.. -- .000 0 00 0. ( 0,

0.000 0.000 O.U0 0.01 .On0 0.000 0.003 0.003 .000 000 0.000 0.000 . 0 0000 0.00 0.000

0.00( (.024 0 00

u.01( 0 o 00 0. 0001 0.00014-

R UN0 .-----.... .... -- 0 .-.. . -- - (0 . =0000

0000 0"J00 2 SEGMENT- 4

.,o Ourur A..o OU ooUo

0 0 2 0 0 0 o 0 0 0 0 o 0 0 0 0

0 6 0 0 0 g7 - _ _o .0 2 _ I 1 0 0 .3 0_ - . .. .. . - ""0 . . . . .: .... .-" .. . 0 . . 0- - .. . 0- . . .

"- 01 0 0 0 0 0 . 0 6 I I0 0 0 0 0 0 1

.1 2 3 1 0 0 o 72 0 .... . . . o 0. 0 0. 0. 0 o 0 .0 . . .

1. 0 0 2 0 . 9 . _ 0 0 2 0 0 0 5 * o

0 1 2 C 0 0 34 26 - ,

....... ... .- 7. 3_.- .......-- -.- - --_..- , .183 -... . SUNAP.._._ o

ASSRHE PnEP FOAHSORHFI) POWFP AF0000(101,'0PA~) (('90 O OOO( (0 0 0 .. . . ..O0UO011. .. . ... ......C } ), r , 0 . 0

0.000 .-- ".0 .000 . 752.360 - 2 ., ,, QoOO0- .0 n0 0 .0 0 0 0 0.OQO 0.0 0 -.- -OO U 1O.ol0 0 O U - 0.000 00 .

0 .000 4.306 10.79120.949 .0 .00'0 0.000 0.000 *040 0.000 0.(100 0.000 0.000 .0no 0.000 o 0U00

'.222 0.O00 0.0011 0.J ,0'. p.0,0 0.U00 0.297 0.000 0.000 0.000 0.000 ....... . . ... . 0 .00 0_ ,

______ 0.000 0.000 - o0 .0-0.0 00 '.0009. - Q.QeO - . - -_ . .. . . . . - . 0.0011 0.000 l).100 0.10 U.000 0.,(.0 U.')O 0.420

0.000 O.00n 0l.62J 0.777 ". U00 0.00.) 0.113 -. .209

.... ~-- -- -.. -- NOk00LL~I SUOO8E P~hEN AOL)U000 On O 0.000 U.u00 0.00 o.000 0.000 .JO00.000 .000. 0.00 0 0.. 0.0 0 . .0.000 . .000 0.00 -..

0.000 0.000 0,9)0 0. , 0 0.000 v.0u( U. U 0.000

0.092 - 0.746 5.51 4. 577 .0.000 (.C00 0.0 1 000 - 0.000 0.00 U .000 0.000 oioo 0Q.000 0.0( o v.OOU

0 .03A 0.000 0 .000 3. 73 1.4,1 . .(. !0 n. . .99 _ 0.0 1, . . . . .-.. .-.. . . . . . .. . . . . . . . . . ..

N .(l' 1 .(' : H ( .',. 5 .. -0 .- - -. - - 1 - - . 77U 0 - - - - -

0.00N 0.000 V.d00 0. 000 (..-j U 0.00 o.000 0.00;

0,000'" 1.657 2.0306 2.541 0 .COO Q. -00 0,0f.)0 000 !

0.168 0.(00 0.003 0..00 .hl On.000 0.OnO 0.00; -

0.069 0.281 1.031 0.432 0.010 100 0.000 0.009 - 0.00 0.000 0.000 0.U00 0.000 0.000 0.000 0.004

0.028 0.000 0.000 0.356 0.070 0.000 0.006 0.004 I - 0.000 0.000. 0.. _7 . . ,.373 .00 - .. 00 . . 000 o 0.00 -

0.000 0.011 0.017 .1'.7 01.o ,) 00 1110-__.Q? 31 ... .....

kUN=84L)5.0OEGREE=5

SEO4*NT 7

AFu OU TPuT. 0 . 0 . 2 ... 0 - 0 . 0 . 9 - .-- -- --

0 3 1 0 0 0 0 01r50 3 0 0 0 0 0 0

SEGPENT ... 2 0I 1 1 2 0 1 3 b2

AFO OUTPUT 0 2 0 4 0 3 20 59

0 0 0 SUMAP= 06.851 SUMNAP. 13.917

0 3 0 0 0 ABSOE POWER AFo 3 2 () 0 . --- .lb)~ 9000- - - 0.9 -.-- --

1 .9 1 70 0.000 0.00V 52.39t .00 ,00) 0ouo V.0O0o 0.00

0 0 1 2 0 2 10 51 I 0.000 2.197 I0. 197 U.000 .0, J. V0 . 0 .0 0 . 0 0.00_ 0.00n 2.716 0.000 V9 ,0' . l0 . '.090 0.0 0 0.0nu .

SUNAP=158.556 SUMNAP= 23.456 0.092 0.000 3.666 -. 577 0.000 0.000 0.00 0.4280.038 0.154 0.756 3.773 0.900 0.303 0.165 0.521

.850 0ED POWFR AF) - .. .. 0.000 - 0.127 0000 _3 li0 0.00 ~.375 . . .53 .. 0 40

o.0oo 0.000 5e.98 - 391 o. -1o)- 0.00 NOR31ALIZE A0.SU.E... P.E0 0F..0 .000 ? .19 7 2 1.5 95 0 . O00 .0o ' .0 ,10 0 .0 0 0 .000 N t)R12L 1Z9 t A9 S0800') P O WE R 0 F0

0.000 2.716 - 0.00..9 000. _ 0 00. 0,00 . 0.000 0.000...

0.092 0.373 1.834 4.577 0.019 1.-71 0.000 0.JO6

0.038 0.000 0.706 0.000 1.406 3.000 0.270 0.08U0.000 _ _ 0.0n0 _0.31 1 .555 _L .0 2... ' .

25

0 0.22 .1_-7' .... . .

9N0HMALI.ED AMSORHE) POWER AFU

0 .0 0 0 .0 0 0 - 9 .8 8 0 6 . 16 5 .0 . ) 0 0 .0 0 0 . 0 0 - 0 .0 . .. ...

0.090 0.829 4.(972 0.000 U. 00',) " .• O O.VO 0.002

0.000 1.021 • 0.1 0.000 0.o0t 0. .000 .2 0.000 0.000 0.00r 1 0.0 0 9.83b0 u.aOU 0. . 000 0.0 0 0. 0000.U69 r. .11 0 .3 4 t 0.132 0 .,h01 12.v035 - 0 0 - - . .002__- - -- . . 0.000 U .0 829 ... V, 36.- 0.O ___.. 00 __ l V __( 0.000 . 0

0.928 I].0,"}0 -0.143-' 0.000 "" .v ' It - 1.O00 .. . .0 3 0.003 0.000 ,1l.024t 0.1lou 0.0v0 u) , .000 0 0, 0n "I..'CO

0.000 0.000 0.059 0.147 -0.0O0 . 0.0) _ - 0.03 0 01 .. . 0.069 0.900 10,92 0.132 0.000 2.0.)0 0.000 3., 430. 02A 0.05 0.143 0.356 0.UO0 0.007 0.002 .0:3

im . . . .0.00 0 0048 0.000 0.23 U .uol 0.009 0.005 0.001

09891 S5HNT6 HU----- -- -6___

DGEOR FE b

0 0. 0 0 OUTPUT 0 0 .......... .S EN a--

00 0 0 0 0 .. " .

1 1 0 0 0 0 0 10... 0 =I 0 0...0 0 . *o* *

0 1 1 0 0 0 5 59

SUMAP= 2.e17 SUNNAP. U.136 .. . . .- -. ---

At0S()hFO PO*FR AFO0.oo00 0.000 0.000- 0.0O0 .o -- .-o 0.0oc--0. ... 0.00 . . . ". --0.000 0.P00 0.000 0.000 0.000 9.000 -0.00 0.00 0 0 0 0 0 0 0 U0,222 0.905 V .000 U.n2 09 0 .00 ..0 U.000 0.000 -- 00.000 0.373 0.000 0.000 .0.) O ;.000 0.00U0 U.00 f) u - 0 - -- 0 -- - -

0.000 0 0.0 00 0.000 0.00 0 .0f, 000 3.00 0.00 4 0 0 0 03

-.- -... . .. .. 2 0 1 0 0 0 0 63

-- 4A

2.11 SUIl) .P -. 778

AB50R6EO POO R AFD0.00 0.000 .00 0 0.)0v 0.00 0( 0 0.000 0.000. .. . . . ..... . ... -- - -P 0 0.000..113 0.,!,4_ .))))1 , 0.00'0 C u , I - , O. OO - 0.o0O

0.000 0.90 0.00 0.000 . l 0 Q () V 0 000 _0. 9000.000 0.063 0.311 0.00 9.00 .000 0.113 0.204 . 0.373 000 .00 .O 0.0 00 0.0

0.000 ". 7 0.L ) 0o ... 0 . .00 .0 .. ... 0 0.000 0.031 0.00 .311 0.00 0., n _ 0.0) 0 . 0.000 0. . .

0.00o 00030 1 0.000 010 0.000 0.VO0 0.00i ORM.LIZE. AHStn P.u P R AFo0.000b 0.341 0.000 0.000 0.-00 0.0000 0.000 0.000

0.000 0.141 0.000 0.000 0.00) 0.000 0.000 0.000 OU.000LIZE0 0000 O.0001oV0 00 0.0000.Ib .31 0.)1 .10 0 to 9.9 009 .600.00 .00 0-~o .02u 0.1)00 V0.)9 9.2)), 0.290 0.000o

0.000 0.90 0.000 0.000 9.000 0.000 0.000 0.000 - 0.00 0.000 0.000 -0.OO0 - --oO- -- (.00) " 0.000 0.0000.000 0.00t0 0.000 0,.)00 0.1 00 0.000 .n 0.000 0.000Q.4

0.000 0.0?4 0.059 0.000 .000 0.0u 0.1 0.001 0.00 03.1 .000 0.000 _ .0 0.90) 0.00 0.00 .0 0.069 0.141 0.00 0.000 .f. 0 O.uO 0 U.0100

0.000 0.000 0.143 0.00 .0, 0.000 0.uo0 0.v00V0.023 0.00)0 - 0.059 _ 0.))0 .19.0 . (-.02 . ,.090 0.901

. ... . RUN-

RUN=8 DEGR5F=5.. . .. EGRE0

=5 .... __ .............. ....... SFG30 -NT.1l . ... - ......... ......---- ---

SEUMENT 9 - - -

All) ouT.PuFAFO" OUTPU

S 0 0 0 0 _

S0 0 0 0 0 0 0 0

0Q 0O 1 2 0 0 0 0 "o *1 0 o . . ..0 .. . . 0. 01 .....-----.--..-.- ..-...--- ---------

0 0 0 0 0 3 0 60 ....... 2 _ . . 0.. 3 33 00 ___ i- - - - -

SIIMAPm 20.588 SUMNAP. 4.23

0.000 0.0no 0.000 .0000 0000 0.00 0.0 0.000 1 0 0 0 0 00 0 5

.... .. ... . . o -- o o 0 0 . . ..... 655..O 1 0 0 0 1 0 55

.i SUMAP. 4.219 SUMNAP- 0.906 7

S ABSORBED POWEk AFD

0.0 .09 0.000 0.000 0.000 0.000 ,_ *_O .On 0.000

0.000 . 394 V.000 Vow(0 0.000 t00 0 0.000 0.0,1000 ., O,0n( 0.0000,000 * 0905 - , 900 .00 - 00k 0000- _,p 0 . - 0.002 .9v 0.*0 0,000 •0 0.00 f0 0,n ioO

0.092 OO*O 0.000 0.000 0.000 .0,0 0 0.22 0.03 0.154 2... 67 0.0 0 .00 0.000 0.110 0.134

0.000 0.0 o 1.51Z 0.000 0.0( 0.000 1.099 0*'m 0 .0 f) 0 00)0 0*125 0.023 0. 19

0.000 0.063 O.0.0 1.555 0.&00 0375 0.775 0 .0 0063 0000

.iIoMALI ZE0 AtiSuPBEU POWEH AFUNONMALI7FIO AHSORREID POWER AFD t0) U 0000 0.0 Q.0 00 i 00

0.000 0.if0 O .'D a .Ou0 OeU O U. ,1 j 0 h(I

- V ,~u .V UeVLI 0 . '} 'l 0.0000..0 0 011)(0 )."Oo u .lO m) .. 0..

0.000 0. 0 0.00670 0.000ut) 0*000 O.oo 0.000 0.000 0.341 0.000 0.000 , 0.000 0.0n0o 0.000 o.000

0.00 o.noo 0.000 OlO .o. o .Ooo 5.000 0.0 13o 0.0o0 0.00 0 0.00170 o.c.0 0.000 o.o00 o.OOI-- _O.... o , o ooo o I. 9 . 0 0.--o o o.00 ., 0 -o, oo-t.ose o.coo o., .. o.oo 0 o.aco C .o o O.... 0.601

0,690 0.000 0.o0 0.000 -. 9 0.000 .013 0.0!3 0 .008 0. 050 8 0.428 0.000 0.f00 .000 0.001 0.001

00000 0.00 0.285 0.00 0 0 009 000 .012 0.04" 0.000 0.0 0.00 0*.00-3 00000 0.001

0000 0.034 0.000 0.14? 0.010 O.*09 0.009 0.001 0 0?4 _ -0 ___---

U1

RUN.8 HUN8

-.0E G R E E 5U E Q P FE . - -.. . .. . ... ... .. . ...5 ......-- -. . . ....

SEGMENT-10 _SF mE l4Tm12

AFD OUTPUT ' FL II-UT. . ...

0 0 0 0 0 0 0 0 0 0 0 0 0 0

0 0 0 0 0 0 0 0 0 0 0 0 0 0. 0

0 0 0 0 0 0 0 0- 0 0_ 0. 0 9 .0 .0

0 0 0 0 0 1 2 1 0 0 0 0 0 0 0 0

1 1 0 0 0 ' 33 33 0 : 0 0 0 0 0 0 5

1 3 . -23 4 --- -... . ..- - - .. . 0 -... 3 ... .- . ..... ... ...

SUMAP. 11,970 SUMNAP. 0..85 'SUMAP. 2.659 SUIMNAP 0.3741

"ABOR9JE9I POwI' AF'I ABU tIED) PowLk AF0.000 0.n00 0.000 0.000 0.91 0.9 0.090 0.0 U . L0.A O FO 0000 0 0 0 0.00 9.000 0* .000 0.000

O.009 _O.no0 O.0 .. o.. 1 0 0 Q. 0___ U01 0.00 .... . 00n .. 9600 ... 0 o.O V U . .0 1 .. ' P .. 000 - .0 .. 0

.. 0.000 0. 0 V. f)00 U.000 0.o.00 0.0"p 0 .0 0.000 0.000 0. (00 0.90 0 Q.000 .19.00 .0 0 0. O 0.1 .000

0.000 0.000 0.000 0.00 0. 000 7.13! 0. 257 0.O20 0.000 0.000 0.0110 0.000 . l0 1 ) v. 6) o0 0.0A0 0. 000

0.034 0.154 u.,00 0.One 9.030 1.ul0 0.060 0.' 0.000 0.00 0.000 U.nou .1. 0, 0 ... o000. . 000 0.0-10

0.016 0.190 1.246 3.330 2.,0 0.99 0.012 0.196 0.000 -0.963 0.93'. 1.,55 u. 000 0.110 0.073 0.04 .

NOWMALIZEU AHSO9P9 ED PO 00EN A0 00 ... . NOWMALTZED AoH15(WhEI) P) ER AF0i ....

.000 0.00 0.000 0.000 -.0 0.000 .0 0.00 0.0 .u0 0.000 0.00 0.00 0.00 .00. o.o " 0.000 0.000

0.00 0.000 0.0ou0 0.0 00 _ V9.1oL 0.* _ .0. 0 . 09 00 . 0.000 .pno0 0.1,00 0.000 9u ..0... .0.0 ) .000

0.000 U 0.1)0 0 - .00. -01l00. W00L .00 .. 0.vOO __V90 _____ o____ 0.000 - .00 ~O 0, V .000 I-V- Q ~J 091. .000- V.900-

0.000 0.000 0.-0o 0.000 0.U90 0.") 0.003 0.00 0.000 0.000 0.000 0.0t"o U.uo0n o.bOu 0.000 0.00

0.008 0.10 0.00U 0.6010 6.0 o11 o. 43 0.008 0,02 .00 0 .000 0 . .000 .000 .0 0.000 ,1*000 0.00 U.100v

... 1 ... 9 3I 0S- 10 7ll .09 .007 .0 .... I 0.0 0 .. 0 . 02- .1 I 047 11.241 10 701.h 1.4l

SF , E =- 15

" i .... .. .. . .. .. . . . . . A F tD O U IP LIT . . .. . . . . . . . .

0 0 0 0 0 0o o 1 0 1) 0, 0 0

- 0 .. . 3 . . . .. . . .0 0 _ II .. . . .0 . .. . -_.. . . ..1 0 0 0 0 O

10100058o ... .. . . . . . . .0 . ... ... (I .. . .. 30, .. .. | . . ... .. . . .

RUN- 8 - - 50MAP= 24.2 2 5 .0 wAH 4.bT7

I)EGRE F =5S06MENT 13 ABSORHF__ POwI AFD"

0.000 0.000 0.000 0.000 0.000 0.000u 0.000 0.000.. . AF OUTPU1 0.000 .0.000 10.79 f . 0.000 0.000 .000 0.000_ 0.000 .

0o 0 0 0 0 0 0 0 0.00 2.716 4.450 0.000 O. O0 0.000 0.00 0.000

0 . . 0 0. 0 9 " , 0 . ,- - -0.092 0.000 3.8 0.000 3.0 1 0.000 0.00 0. I o

0 0 0 0 0 0 0 0 0.038 0 .000. v,75 , 0,000 . 0 . 00 0.000 . - 7.487

0 0 0 0 0 0 0 17 0.000 0.063 0.000 0.000 U.Vuo00 ('.00 0.193 0.20 0

1 0 0 0 0 " 0 19 4 t.

S 0 .J. 0 0 0 "_ 0 _44 56- NORMALIZED ABSORBEt) POwEi AFL0.09 0.000 _ 0.000__ 0.000 . . ), .000 .0O000 0.000 .

SI)MAP- 3.38.8 5.m.NAP= 0.084 0.00 0.000 Z.03. 0.U. 0. . .0 0.000 i .. .0 .0S 0.000 1.024 0.839 0.000 0.n1 0.*00 0 0.010 ,00

ABSORHED POE R AFO• 0.069 0.000 0.b92 0.000 ,'0 0..jU0 0.000ou 0.001

0.000 .00 .00 0.000 000 .00 0.000 0. 8 .0.090 00 .0 3 .0.0 0.0.000 0.00 . 3 .0 .0 000 0.000n 0.003

0.000 0.0000 0.000 0.000 0 on 0.000 0.090 0.000 0.0 0 0.)'.P 0 .O ; 0.0n 0. C.1n0.000 .n9 .ue1

0.000 0.000 0.00 0.000 0.00 0. O 0.U00 0.000 RUN="0.000 0.000 0.000 0.000 0.00 0.000 0.00 0.341 DEGEE=5

0.038 .0 f000 0.000 q.000, *. 0 L ,90 1."044 _ 0.700 - SEGMENT1f;

0.000 0.063 0.000 0.000 0.000 0.000 0.997 0.19 4 .-

AFU OU PUT

NOoMALIZEO ASnRBEL0 POWIR AFL0 ) - -. U .. ,. . 3. ... 0 0 0 0 0 o .0.0 00 0.000 0U1) .000 . u.00 0, .000 0 . 0 .0.0..0 0 0 00.000 .000 .(co Q.o v.A 0.000 0.000 0 1 0 0 0 C 0 00._ . 0 U.00 00 0.00 0, 000000 0000 0.000 . 1 0 0 9 0 0 5, .O.00( 1.600 0.000 0 .000 u.000 V.,00 0.00 0.(00 0 1 U 0 U 0 5,0.000 0.o0 0 0.000) .000 . 000 .0, 0.0 11 . _ ft4. 0 0 .... 490.000 0.004 0A. 000 0 .0t 00 _0 0 1.000, . 0 oo 0 .

-5l P - "-3.084 -

UMNAP= O.bll

0N DEGREE- 5.... .................. -1O0 0 .000 . O. - - - - - . .VC 0. 3(,v U. oO u.

SEGMENI= OO 0.000 .0.000 0.000 .. 0.0 0 .00 0.0(0 0.000 .00

0 0 u .0100 0. 0.000 0.050 0.000 0.000 o..0.0 0.O 0.000 0. U.U(. OUIPVT 0*01 0.000 U000 0.000 O..5o 0.0 00

0 0 0 0 0 0 0 0 0.000 V0. 154 O.OOU 0.000 ,.,00 0.0 C.0.020 0.3l• 0 0 _ 0 0 0 0 0 0.0(0 (.000 .11 O .0.000 0. v . ,0 0.566 o.ll

0 0 0 0 0 0 00 0 0 0 0 0 0 1 - NORMALIZEf A44 cuP M Pt, 14 A1f1 0 .0 0 ._._ 3 0 34 . 1 0.000 0.oo .1:0 0 0 0.0 ~0.9 0 1. 0 .00 0.000 .0 0 o 0 0 5 07 12 0.000 0.000 0. 00 u 0.010 0.0 0 ( .o 0.000 0.O"oo

0.000- 0.34 0.000 0. 0 U0 00(I 0.000( 0.n00 0.000___ A-C0 ..C 0.00 0.Q C69 .0.00,,,, 0 1000 -. 0 -0.'0

511 A0n .900 -- 0 00 )0 - C.00 0 0 V. _ _0.0i .0 O o . 00 0.003 1. . 3

ABSORBEO POWER AFP 0.012 0.000 0 .111 0.n00 0.,l, 0.*0 , 0.0.7 0.00I... . 0.000_ _0.000 ,0. 00.0 , . 0.0.0....0,00 .. 0.900 0.000,. 0.000 . .

0.000 0.01 0.00 0 0.00.0 0.00.0V90 0.000o 0.000 H UN..0.000 0.000 0.000 0.000 ".00 ,- . 000 .O - 0. O. O E0'F =E S

S G E , q T=17

A AFI) VQUIU V... . . .. ..0 0 0i 0 0

- 0 0 0 u u o 00 0 0 0 0 0 0

.. 0... - 0 002 250 0 0 0 0 0 0 25

".000 0.000 0.00u 0.01.0 0.(0, -. ,0u 0.000 U0.G 0.... (1.030 _ 0.0' 0 0_F.00.. . 0.090 ___0.0On1 -__0.001o .. .. 009 . 0.5i0 . . .. so-oo= 0.109 0,U71N.104 0.30',

0.000 0.1l. U.0 0.F0 01 .,0 - 0 1.01U 1.0 61 0..9o

.. A8SOHbF'b POWER "AF . . .NOkMALIZE6 AHSOR8EU P)001 R 10 AFO 000 0001 0.0 00n000000 0.00 ( .. 00 0 0. 00U00000 0 .000 .n- 0 0.000 . 1'o U . COu 0 .(00 0.o 1O0.000 0.000 0.000 0.01(0 11.00 0.000 0.0n00 U.000 . U. 0.000 . 0 .( 90 r .U

0.000 0.000 (.p10 9.010 00( .090 0.00 0 0.000 000 _ 0.1100 ((.000 0.000 0 .e 0.000 0.001) 0.01 u00.000~~~~~~~Unn .(% 0.10 .000 Cib~ ulO, .~n 0. ..... 9.0 .-h 1,O~ 0.0 U. h o l O.ll .s . i . u

0.008 0 no0.000 0.00 0.000 . -Ov 0.0 0.003 000. "0 00.. 0.000 0.000 .00 0.0 0 01 0.b

NO4MALIZED AfSOP8O POwER AFD00U.000. 00 0.0 00 0.000 0.u v . v . . ,'0 0. 001 0. j000.000 0.00 0.00 0.000 .0e } ) L_ . O. .unO 0.0 0

( 0 0 00.00. 0.000 00 0.000 0.. 0- 0 .0000- . ..O on O.u,0.000 0.000 U.00u 0.0O0u O.u P.000 0.0"n 0.0000.00 0.000 0.000 0.000 '.01 0.10 0.090 0.0100.000 0.000 __ 0. 0.000 Q.- 0 0*. o 0.0? 0.001

RUN 8, DEGREE 6

(Note: Degrees 1, 2, 3 are degrees 1, 2, .3 for front seat;



I FACTORS ARE

O.OUOO f0 0 0. 'C 00 U.000000 )go'+0t0i U.6.. o,:.i0. ':'( ). 35u r. 0.002300

IMPLITUDE LEVELS A 5E SET Af

0.03 0,05 0.08 0.13 0.2) *.32 .5(

IRtL.WUENCY LEVEL5 Aft SET AT

I.06 0. 1 0 .?5 .o 0, .O.

CEi\j ER AMPL1 TU, S A E

.044 0.0 8 (. It f 165 .o2 7 U .

CENiTER FREtTUEN,,CIES A --

IV. 088 0 177 1).354 0.707 1. 4 2.2 5. 11.31

1 AXI UM P(SSI, _ CuUNSS Li SL , -T

1,326 2.652 5 .3i93 10 ,) )7 2i.213 42.420 84.i r,3 1b, 70S

IBSURLED POWFP ,ATfRIIX0o00000 0. o000 . 000000 2;7,? :._. +9,2151 21. 32 6 2.91209 U, 1913Y

, I)000 0 .o0 0 . 00 I.• ,t,') 72, 1 U O71, S91544 1o20016 0 , b,3

I 0.0000 0 0.000C 0. u000 4od 4v 3. 791. 3.67431 0.490 0o03250

00000 0.000 , 0. 0OO 1.992 3o+9 ?; I.01,+29 0 .2305 U.013400.00000 0,0000 0.00000 0. 11 1. +,019 624. 8 0 )0.06401 U 005p2

SO.0000 0.OOr1-U U.'OOO 0. 3363+ -, 3 U.I- c:7?u 0, 034 b2 0.00226

,,1AL ] ZE!) A6SQF ""L POWEk HA

O. 000 .f , 0 . 0U 2 o 71:. .. )332 1. D99 0 .,343 ? .0.00113

0.O)00 0.0000' .UOOOO (.9I v0.1ow6( ,.?710i44 0,01414 ., )4 0U00000 0.00oC 0.U0 0!) "I.1 o39)9 1 ,08o 6U C.UU5I3 0000190.00000 U0 ,0 ) U . " 0 O0 U b., 1 (' - . .4fj U .,035b9 3 0 '2+ 0. 0O0o.00000 0uG 0000. '.7 / .,079 ".0147i •.0009 0.0 00030.00000 0.000 0 O0 O0 0.'317 I :,ot 79c .0 (1006 0, 0-)I 0.00001

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0 0 0 0 0 0 0 10 SEGMENTI 8

0 ( 0 0 0 4 5300 00 0 .... .. .. . . AF) OUTPUT

*0 0 0 I) 0 0 0 0SUMAP . 235 SUMNAP 0.011 0 1 0 0 0 0 0 0

0 I 0 0 0 0 0 "0'AWNURbFO Pn40W AFD 2 0 1 0 0 0 0 0

U.000 0.000 0.000 0.000 0.000 0.000 0.000 0.00 0 0 0 0 0

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0.000 0.060 0.000 0.000 0.000 0.000 0.003 0.000

U .NUMI0ER2 40- _ _ _

RUN.FlWUN.9l• -. oE(01~E ................. ..................... . ...... . I......... ... i.URO.0DSEGMENT.

. SF.GMENT. 7 S04ENI. 9

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00 1 2 . I J 0 .> 0. 0 0 0 -- .. I .-.-. 0... . * 0 ... .. .

. .2....... . 2 I _ 1 0 0 1 0 .1 16 46

SIIMAP|09.306 $UmlNAlPo 0.770 .. . 01 AP- 76.117 SuooOP._.0 . .

A-U.,E, PO,.F A .) A8SOPBED PO,.1 A'O

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-- AF0, OUTPUT

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1 0 0 0 0- 0 - A 0 01 0 .. o o 0 0 0

0 0 0 241 0 0 0 21 _ 0 10 1 0 0 0 3 49

SUAAP. 8.904 SUMNAP 0.163 .AP 1.57 U'Ap= 0. .21ABSOHBED POW'R AF ABSORBED POQ,2 AF1U.000 0.000o 0.000 0.000 0.0o0 v.000 0.000n 0.000 0.000 0.o'. .00 0ouo. -0--0 .000 (1 . nf A -_ O . o .0 -V I. f . 01 Q__. ' .It0ll 0.000 U *LI D O 0 .000 Q.Ou O 0 .00 0 0- 0 0 . V0 .OnO 0.OOv0.000 O.n0o0 0.00 0 0 - 0 .00¢* a 0.00' - 0.000 .. . o 0 0.000 . 0.000 .000 o.O .oO . O n o.o0'.0 . 00 0.000 0.000 0.000 0.00 . 0 0 00 0.0 0.000 O.Ooo .oo -- o. o o . 2o.0 .o) 0.000 0.00 .

0.000 0.000 0.000 0.000 .000 . 0 0 .00. (IO O.voo .0 . 00 0.U05' *.00 o.000. 0. 00 000 0.000 0.000 0.000 .... 0.000 ... 3.120 __ .. 0, . . .0.000 0 .000 0.000 0.O 0.00 .o. 0. 0, 0. 13-0.000 0.000 U0.000 0.000 o.00 2.0 0.707 0.102 0.000 0.... 0.000 0. 0 . 0 . . - . .18 It

NOR00CIOE, AIOPS)000 P 1,,)E. 0), - - - 400AL7E OsnoGOO (000 AU .O . .. 00 _-N0.AL0IZEl anso)ag Pow(W AFu NO MALIZED A.SORbFU POWER At U0.000 0.000 0.000 0.000 0.020 - .000 0.000 0.000 0.000 0.000 0.000 0. .

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l, - -

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C 000EE. IOEGRF 1.:SEGMENT 11 0 0E0l1 13

.. ...0 0. . .. . . . AF _OU00 PLj . .. ..0 0 0 0 0 0 0 0 0 0 0 0 0 00 0 0 .. S_ 0 _-...-- -- - 0 0 0 1 0 A ) 0

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00 1 0 - . 3 3 42 .

_ 5MAP=_ 0.559 .... .. . o_ 9 . SUV-'P 5.117 SUINAP. 0.o04

AOSOPLEO POWE"? AFt O AmUSORHED POvFi AFb .. . .. .-0.000 )0 .n0 V.000 0.0 J0. 0.000 01009 0 00

0.n000) 00,0.000o 0.000 0.000 . 0.000 0.00 _ 0.0 0. 00 0 0. oo ..... 0050 (.00no 0.000 0.000 0.00 0.000 O0.oo 0.0000. 000 0 .0000 .00 0.000 0.0) _ .000 0.000o 0.000 oo 000 . O.0 0 u .000 0.,,,l C,. Qn0 1u 12 0.06o0.000 .000 0.000 0.00 U00.000 p..0V 0 o.0 ') 0.0j0 0.0 O.O O.rrO0 0. OOs _',.'. Z.O .0 0 . .. :. I -0.000 0. 0 0 0 O.OO 0 "OOU U Co c.?57 0.173 ':09b O.0.000 0.000 0.000 .0 0 V 1.(00 0.500 0.000 0.00 . 1,

NO04"IALIZEQ AHSOPI EL P,)-E R A F L NORMI'ALIZt A05tIPdLU POWER AP U0.000 0.010 0.000 0.000. 0.000 0.000 .On 0 .000 0.000 -- - . 0.000 0.000 0 90.000 . o U0 - ,000 . 0 0. 0.12. 0.00 .0.00 0o000 0.000 0.0 5O.0- 0040 0.07 0.000 0.000 0.0.0 O.U0 .000 0.00 •,u .5.01 O.un 0.1'.0 OO 0Ono .) U °(if)U V.0 0ll 4-Vo'0 Oo)I U.VUU N06io0 0 100 0 .000 )U0.000 0.000 0.000 0.000. .000 0.000 0.000 0.000 0.000 0.000 0.000 U.000 0.00 5.000 ... O0 0.000

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L.1 .J. .. 0.. !_ S o o 5 _ __•

SUMAP- 2.40? SUMNAP. 0.054

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0

.NORMAL I ZED) 4HSOROFU P0EH AFUAHOSOHED POWER AFD 0.000 0.000 0.000 0.00 0.00 0. 000 0.000 0.000-

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SEGMENTi15- 0 1 0 0 0 1 5 51

AFU OUTPUT ' o SUA 1 17. . . SUMNAP .0.02 9-A.---.. ..... ABU ED POWEN AFO

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0.000 'O.000 0. O u .96b O. GO V ~ ) 1. OfRU O O.OQ U ...... , p oo ... ... . .......... ......... i~o

.. .000 O .".0 000. 0.00 .6 2 G0 0.0(0 0.00)90. 0 .59 0.00.0 0 0.00V . . 0 0 ... .0 C.0. 0.046 . . .

0.000 0.000 0.00 . . P .00."0 FU .F 0?V t.Ur , N O_0.000 0.000 0.000 0.000 0.000 0.00 0.00? 0.0010of). 0.000 0.000 O0.06 u..000 0.01? 0,019 0.001 0.000, 0.000 0.000 U.O000 0.00 r 0.006 O.007 0.001

APPENDIX F

Absorbed Power (AP) Bus Correlation Data

PRECEDING PAGE BLANK NOT FILUM

Table F.1. Bus Ride Data for Run 2,.Front

Segment Vertical Lateral Fore-Aft Summation A-1 A-2

1 0.385 0.231 0.018 0.634 3 3

2 0.379 20.188 0.019 (20.586) .398 2 2

3 0.490 0.206 0.027 0.723 2 2

4 0.005 0.002 0.001 0.008 2 1

5 0.291 1.722 0.014 2.027 3 4

6 0.033 0.352 0.000 0.385 2 2

7 0.418 16.940 0.030 (17.388) .448 3 4

8 0.041 0.084 0.000 0.125 2 2

9 0.624 2.603 8.206 (11.433) 3.22 3 3

10 0.269 1.139 0.021 1.429 3 3

11 0.163 0.125 0.001 0.262 2 3

12 0.061 1.986 0.008 2.055 2 1

13 0.341 0.106 0.063 0.510 2 2

14 0.380 0.170 0.037 0.515 2 3

15 0.627 1.149 2.539 4.315 3 3

16 0.158 10.375 0.016 (10.549) .174 2 2

17 0.208 21.367 0.001 (21.576) .209 2 3

2.5

2.0

4-i

- 1.5-

0P-40

01.0

0.51I.--

1 2 3 4 5

Subjective Rating

Figure F.I. Objective vs. Subjective Ride Rating for Run 2, Front

F-2

*Table F.2. Bus Ride Data for Run 2, Center

Segment Vertical Lateral Fore-Aft Summation C-1 C-2

1 0.139 0.049 0.006 0.194 3 2

2 0.426 0.771 0.004 1.201 1 2

3 0.737 0.809 0.006 1.552 2 1

4 0.032 0.104 0.000 0.136 3 2

5 0.345 0.171 0.005 0.521 4 4

6 0.013 3.265 0.000 3.278 1 4

7 0.436 0.265 0.008 0.609 3 3

8 0.302 3.074 0.000 3.376 2 2

9 1.177 (16.398) 2.139 (19.714) 3.316 2 3

10 0.142 0.255 0.010 0.307 3 2

11 0.184 1.149 0.002 1.335 2 2

12 0.045 0.260 0.000 0.305 1 2

13 0.374 0.196 0.003 0.573 2 2

14 1.071 (3.730) 0.013 (4.814) 1.084 1 1

15 0.446 (14.862) 1.170 (16.478) 1616 2 2

16 0.190 0.120 0.000 0.310 1 2

17 0.180 1.169 (7.597) (8.946) 1.349 1 1

F-3

2.5

2.0

4J

1.5

o

0 1.0

0.5-

0 -1 2 4 5

3Subjective Rating

Figure F.2. Objective vs. Subjective Ride Rating for Run 2, Center

F-4

Table F.3. Bus Ride Data for Run 6, Front

Segment Vertical Lateral Fore-Aft Summation A-1

1 0.274 0.547 0.190 1.011 3

2 0.208 (2.713) (2.928) (5.849) .208 2

3 0.311 0.016 0.010 0.337 2

4 0.018 0.029 0.001 0.048 1

5 0.254 0.076 0.010 0.340 4

6 0.015 0.070 0.016 0.101 2

7 0.292 0.058 0.014 0.364 3

8 0.072 0.254 0.002 0.328 2

9 0.179 0.081 0.009 0.269 5

10 0.182 0.288 0.033 0.503 3

11 0.152 0.029 0.002 0.183 2

12 0.038 0.488 0.010 0.536 2

13 0.147 0.039 0.011 0.197 1

14 0.094 0.037 0.004 0.135 1

15 0.124 0.040 0.004 0.168 2

16 0.138 0.010 0.003 0.151 2

17 0.213 0.120 0.005 0.338 2

F-5

2.5-

S2.04-J4J

0

P4 1.5-

1.0 oI

0.5-

0 1 2 3 4

Subjective Rating

Figure F.3. Objective vs. Subjective Ride Rating for Run 6, Front

F-6

Table F.4. Bus Ride Data for Run 6, Center

Segment Vertical Lateral Fore-Aft Summation C-1

1 0.155 0.046 0.001 0.202 2

2 0.193 0.588 0.002 0.783 1

3 0.213 0.209 0.003 0.425 1

4 0.021 0.003 0.032 0.056 2

5 0.122 0.058 (13.220) (13.400) 0.180 2

6 0.009 0.072 0.000 0.081 1

7 0.213 0.566 0.003 0.782 2

8 0.018 0.056 0.000 0.074 1

9 0.187 2.557 0.065 2.809 3

10 0.106 0.169 0.022 0.297 2

11 0.030 0.004 0.000 0.034 2

12 0.034 0.073 0.007 0.114 1

13 0.117 0.095 0.001 0.213 1

14 0.072 0.018 0.000 0.090 2

15 0.129 1.185 0.001 1.315 1

16 0.081 0.010 0.001 0.092 2

17 0.253 0.132 0.002 0.387 1

F-7

3.0-

2.5-

J 2.0-

o

1.5.

0cO

1.0

0.5.

0 1 2 3 4 5

Subjective Rating


F-8

Table F.5. Bus Ride Data for Run 7, Front

Segment Vertical Lateral Fore-Aft Summation A-1

1 0.022 0.071 0.001 0.094 3

2 0.025 0.002 0.000 0.027 2

3 0.129 0.502 0.004 0.635 4

4 0.005 0.069 0.000 0.074 2

5 0.143 1.060 0.084 1.287 5

6 0.002 0.012 0.016 0.030 2

7 1.165 9.392 8.761 (19.318) 1.165 4

8 0.027 0.071 0.001 0.099 2

9 0.148 (12.482) 0.005 (12.635) 0.153 6

10 0.162 0.189 0.003 0.354 3

11 0.006 0.030 0.000 0.036 4

12 0.019 0.070 0.001 0.090 1

13 0.128 0.349 0.188 0.665 2

14 0.812 3.041 2.534 (6.387) .812 3

15 0.043 (5.382) 0.002 (5.427) .045 2

16 0.028 0.374 0.001 0.403 2

17 0.184 8.526 0.003 (8.713) 0.187 6

F-9

2.5 -

2.0 -

1.50

0

1.0

0.5 -

2 3 5 6

Subjective Rating

Figure F.5. Objective vs. Subjective Ride Rating for Run 7, Front

F-10


Segment Vertical Lateral Fore-Aft Summation C-1

1 0.043 0.119 0.001 0.163 4

2 0.030 0.058 0.000 0.088 2

3 0.156 0.967 0.001 1.124 2

4 0.006 0.256 0.000 0.262 2

5 0.174 1.802 0.003 1.979 4

6 0.011 0.076 0.016 0.103 1

7 1.088 (13.135) (11.258) (25.481) 1.088 4

8 0.032 0.601. 10.701 (11.334) .633 1

9 0.141 (14.724) (11.640) (26.505) .141 6

10 0.135 0.594 0.002 0.731 3

11 0.008 0.069 0.001 0.078 5

12 0.021 0.359 0.018 0.398 1

13 0.186 2.556 0.032 2.774 3

14 0.884 4.306 0.187 (5.377) 1.071 2

15 0.045 10.169 0.188 (10.304) .233 2

16 0.046 0.466 0.000 0.512 1

17 0.201 0.147 0.891 1.219 5

F-11

2.5

2,0U) 2.04J

0

1.5

,. 0.5 -

-F-12

o7

1.01 I

0.5 1

0 1 2 3 4 5 6

Subjective Rating


F-12

Table F.7. Bus Ride Data for Run 8, Front*

Segment Vertical Lateral Fore-Aft Summation

1 0.166 15.083 6.101 21.350

2 0.172 2.519 0.249 2.940

3 1.095 16.611 6.752 25.458

4 0.048 0.984 0.002 1.034

5 0.154 3.190 0.197 3.641

6 0.008 0.094 0.009 0.111

7 0.170 0.666 0.012 0.848

8 0.003 0.070 0.000 0.073

9 0.127 0.566 0.003 0.696

10 0.246 0.107 0.054 0.407

11 0.i43 0.108 0.037 0.288

12 0.025 0.001 0.000 0.026

13 0.152 3.029 0.227 3.408

14 0.076 0.009 0.003 0.088

15 0.076 0.557 0.002 0.635

16 0.969 16.090 0.001 17.060

17 0.108 0.004 0.021 0.133

*No subjective data available for correlation.

F-13


Segment Vertical Lateral Fore-Aft Summation C-1 C-2

1 0.765 0.107 0.029 0.901 4 5

2 1.404 18.905 10.362 30.671 4 5

3 1.951 1.452 0.280 3.673 3 4

4 0.238 0.196 0.007 0.441 3 3

5 0.791 23.456 14.000 38.247 5 4

6 0.120 0.736 0.011 0.967 2 3

7 0.758 15.917 6.770 22.445 4 4

8 0.036 0.778 0.000 0.814 2 3

9 0.592 4.237 6.102 10.931 5 3

10 0.757 0.845 0.163 1.765 5 3

11 0.321 0.967 0.009 1.297 3 2

12 0.093 0.347 0.021 0.461 3 4

13 0.869 0.084 0.064 1.017 4 4

14 0.559 0.070 0.040 0.669 3 3

15 0.527 4.870 6.874 12.371 3 3

16 1.466 0.611 0.054 2.131 4 6

17 0.447 0.006 0.029 0.482 6 4

F-14

24.0 -

20.0 -

16.0

S12.0

0

8.0

4.0

0 1 2 4 5 6

3

Subjective Rating


F-15

APPENDIX G

Bus Seat Transfer Function Data

PRECEDING PAGE BLANK NOT F ..M

1.17 1.18 1.12 1.15 1.17 1.19 1.30 1.21 1.13 1.13 1.35 1.50 1.69 .82 .35 -- Average.15.15 .07 .04 .03 .04 .05 .05 .07 .06 .07 .06 .09 .13 .20 .06 .05 -- Standard

bDeviation

1.17 1.12 1.16 1.15 1.24 1.29 1.20 1.08 1.07 1.12 1.28 1.64 1.91 .83 .43 .56 AverageO .10

.07 .11 .08 .09 .12 .12 .10 .05 .06 .09 .08 .16 .23 .07 .18 .05 StandardDeviation

1.21 1.08 1.00 1.04 .99 .98 1.03 1.05 1.12 1.15 1.27 1.58 1.99 1.02 .39 .48 Average.05

S.15 .10 .06 .12 .12 .07 .07 .10 .10 .11 .16 .25 .33 .13 .03 .06 StandardDeviation

1 2 3 4 5 6 7 8 9 10 12 14 16 20 25 30

FREQUENCY, HZ

Bus Seat IA Lateral, Transfer Function Amplitude Average/Standard Deviations for 12 Runs

1.05 1.12 1.25 1.18 1.18 1.24 1.17 1.17 1.17 1.08 .93 .91 .92 .87 .96 .80 Average

.15 .04 .06 .04 .09 .09 .08 .11 .19 .17 .17 .16 .15 .18 .19 .18 .16 Standard

Deviation

1.16 1.17 1.20 1.26 1.06 1.23 1.23 1.23 1.22 1.09 ".90 .87 .85 .84 .88 .72 Average.10 .09 .08 .10 .17 .11 .08 .14 .21 .20 .17 .14 .12 .15 .16 .16 .14 Standard.

Deviation

1.12 .94 .97 1.07 1.05 .99 1.07 1.09 1.12 .89 .86 .71 .60 .68 .68 .59 Average.05U .09 .10 .08 .11 .12 .12 .13 .17 .18 .11 .11 .08 .13 .07 .12 .08 Standard

Deviation

1 2 3 4 5 6 7 8 9 10 12 14 16 20 25 30

FREQUENCY, HZ

Bus Seat IA Vertical, Transfer Function Amplitude Average/Standard Deviations for 12 Runs

.15 1.20 1.19 1.13 1.16 1.19 1.21 1.32 1.21 1.19 1.16 1.37 1.53 1.73 .80 .35 -- Average.05 .04 .04 .04 .05 .05 .07 .07 .06 .07 .07 .12 .20 .08 .04 -- Standard

Deviation1.20 1.13 1.16 1.20 1.23 1.32 1.19 1.12 1.10 1.15 1.28 1.65 1.95 .82 .44 .60 Average

0 .10.07 .10 .09 .12 .10 .11 .11 .07 .07 .08 .08 .17 .22 .07 .15 .00 Standard

DeviationS 1.23 1.13 1.05 1.04 1.00 .98 1.02 1.06 1.14 1.18 1.31 1.63 2.02 1.08 .40 .98 Average0 .05


1 2 3 4 5 6 7 8 9 10 12 14 16 20 25 30

FREQUENCY, HZ

Bus Seat lB Lateral, Transfer Function Amplitude Average/Standard Deviations for 12 Runs

1.01 1.12 1.22 1.15 1.21 1.24 1.24 1.14 1.10 1.01 .92 .93 .86 .82 .82 .79 Average

.15 .04 .08 .06 .07 .08 .10 .10 .10 .09 .12 .13 .16 .14 .15 .16 .17 Standard

Deviation

1.14 1.15 1.18 1.20 1.09 1.25 1.30 1.22 1.13 1.01 .90 .90 .81 .79 .82 .75 Average

.10 .08 .08 .10 .13 .11 .16 .16 .11 .12 .14 .15 .15 .14 .13 .14 .19 StandardDeviation

1.08 .95 .94 1.08 1.02 .99 1.09 1.14 1.12 .95 .87 .77 .63 .68 .62 .59 Average.05

S .06 .10 .05 .09 .12 .12 .12 .15 .13 .11 .15 .09 .12 .09 .12 .17 StandardDeviation

1 2 3 4 5 6 7 8 9 10 12 14 16 20 25 30

FREQUENCY, HZ

Bus Seat 1B Vertical, Transfer Function Amplitude Average/Standard Deviations for 12 Runs

1.17 1.20 1.17 1.20 1.26 1.23 1.35 1.23 1.16 1.17 1.56 1.59 1.69 .74 .35 -- Average.15 .07 .05 .06 .07 .05 .06 .00 ' .09 .06 .07 .12 .14 .21 .08 .04 -- Standard

-Deviation

1.16 1.14 1.20 1.19 1.25 1.36 1.19 1.11 1.09 1.14 1.52 1.86 1.81 .82 .34 .55 Average.10.10 .04 .06 .10 .10 .14 .09 .10 .10 .10 .06 .16 .16 .25 .08 .09 .04 Standard.

Deviation1.20 1.09 .99 1.00 .99 1.00 .98 1.02 1.06 1.13 1.48 1.94 1.71 1.06 .34 .48 Average

.05 .09 .09 .11 .04 .10 .00 .05 .06 .11 .16 .19 .16 .30 .11 .08 .09 Standard

Deviation

1 2 3 4 5 6 7 8 9 10 12 14 16 20 25 30

FREQUENCY, HZ

Bus Seat 2A Lateral, Transfer Function Amplitude Average/Standard Deviations for 12 Runs

1.00 1.10 1.23 1.14 1.11 1.09 1.09 1.05 1.03 .95 .83 .80 .78 .76 .79 .66 Average

.15 .05 .05 .05 .06 .07 .13 .12 .12 .12 .10 .12 .14 .15 .14 .16 .09 Standard

Deviation

1.14 1.16 1.21 1.28 1.05 1.07 1.12 1.06 1.02 .92 .80 .79 .71 .69 .78 .63 Average0.10-

.0 .09 .10 .09 .17 .10 .13 .15 .09 .15 .12 .13 .15 .14 .10 .15 .08 StandardDeviation

1.04 .95 .95 1.10 1.07 .92 .96 .94 .96 .77 .74 .63 .54 .59 .58 .50 Average.05 .07 .10 .06 .12 .12 .12 .10 .08 .12 .09 .14 .13 .10 .12 .12 .08 Standard

Deviation

1 2 3 4 5 6 7 8 9 10 12 14 16 20 25 30

FREQUENCY, HZ

Bus Seat 2A Vertical, Transfer Function Amplitude Average/Standard Deviations for 12 Runs

1.19 1.20 1.18 1.20 1.27 1.23 1.33 1.24 1.17 1.19 1.58 1.63 1.73 .76 .33 -- Average.15

.15 .07 .05 .05 .05 .06 .06 .09 .09 .06 .07 .12 .14 .23 .09 .03 -- Standard

Deviation

1.16 1.14 1.20 1.18 1.27 1.36 1.19 1.13 1.12 1.13 1.54 1.87 1.86 .82 .35 .73 Average; .10

. .08 .09 .09 .09 .14 .10 .13 .11 .10 .08 .19 .16 .29 .11 .12 .22 Standard.Deviation

1.21 1.11 1.03 .97 .95 .95 .97 1.07 1.09 1.14 1.46 1.90 1.70 .99 .30 .79 Average.05 .12 ..10 .13 .09 .12 .10 .11 .26 .12 .14 .22 .20 .20 .15 .13 .05 Standard

° Deviation

1 2 3 4 5 6 7 8 9 10 12 14 16 20 25 30

FREQUENCY, HZ

Bus Seat 2B Lateral, Transfer Function Amplitude Average/Standard Deviations for 12 Runs

1.01 1.11 1.22 1.12 1.09 1.09 1.13 1.08 1.06 .97 .82 .81 .85 .78 .74 .64 Average.15.15 .04 .05 .05 .09 .07 .07 .10 .12 .11 .15 .13 .18 .14 .15 .16 .12 Standard

wDeviation

1.10 1.14 1.23 1.21 1.00 1.06 1.15 1.11 1.01 .98 .78 .81 .78 .71 .71 .58 Average.10


S1.06 .94 .95 1.09 1.01 .89 .94 .91 .92 .81 .72 .65 .55 .64 .51 .45 Average' .05o .09 .08 .07 .09 .08 .12 .09 .10 .10 .14 .08 .11 .10 .10 .09 .09 Standard

Deviation

1 2 3 4 5 6 7 8 9 10 12 14 16 20 25 30

FREQUENCY, HZ

Bus Seat 2B Vertical, Transfer Function Amplitude Average/Standard Deviations for 12 Runs'

1.18 1.19 1.15 1.18 1.22 1.22 1.33 1.22 1.16 1.16 1.47 1.56 1.71 .78 .35 -- Average.15

StandardDeviation

1.17 1.13 1.18 1.18 1.25 1.33 1.19 1.11 1.10 1.14 1.41 1.76 1.88 .82 .39 .61 Average.10

S1Standard

Deviation1.21 1.10 1.02 1.01 .98 .98 1.00 1.05 1.10 1.15 1.38 1.76 1.86 1.04 .36 .68 Average

' .05S0Standard

Deviation

1 2 3 4 5 6 7 8 9 10 12 14 16 20 25 30

FREQUENCY, HZ

Bus Seat Lateral, Transfer Function Amplitude Average for All Seats

1.02 1.11 1.23 1.15 1.15 1.17 1.16 1.11 1.09 1.00 .88 .86 .85 .81 .83 .72 Average.15

StandardDeviation

1.14 1.16 1.21 1.24 1.05 1.15 1.20 1.16 1.10 1.00 .85 .84 .79 .76 .80 .67 Average0 .10

EStandard

Deviation

1.08 .95 .95 1.09 1.04 .95 1.02 1.02 1.03 .86 .80 .69 .58 .65 .60 .53 Average, .05

0 StandardDeviation

1 2 3 4 5 6 7 8 9 10 12 14 16 20 25 30

FREQUENCY, HZ

Bus Seat Vertical, Transfer Function Amplitude Average for All Seats

APPENDIX H

Absorbed Power-ISO Standards

Correlation

, ~1 00 o

An International Standards Organization (ISO) standard defining

human tolerance to whole-body vibration has been under development for

a number of years. It is understood that it has received the necessary

approval by ISO member nations and is likely to be published shortly. A

Draft International Standard (ISO/DIS 2631), "Guide for the Evaluation

of Human Exposure to Whole-Body Vibration," was submitted on April 28,

1972 and voted on by August 28, 1972. It seems likely that European

countries will incorporate the ISO document into their own new standards,

and replace existing standards of which the most significant is that of the

German VDI (12).

Three degrees of disturbance are postulated: reduced comfort, fatigue

decreased proficiency, and an exposure limit above which an acute physical

hazard due to the vibration is considered to exist. The standard suggests

methods of dealing with broad frequency band linear vibration in a given

direction, but does not deal adequately with combined effects of different

directional vibration components or effects of rotational vibration.

The limitations of this standard are well known by its originators,

and it has been stressed that the criteria suggested must be confirmed

in each individual type of vibration environment. There are four further

limitations of the draft standard: first, the standard deals with vibra-

tion only above 1 Hz, whereas significant amounts of energy even in the

vertical direction exist below 1 Hz; second, only two alternative measure-

ment procedures are specified allowing either (a) third-octave analysis of

each vibration component so that individual frequency components can be com-

pared with the appropriate limiting criteria for that frequency, or (b)

averaging of a component vibration in a frequency-weighted meter with a total

effect indicated from the weighting; third, no provision is made to account

for more than one degree of freedom at a time (it is not reasonable to say

a person can be vibrated up to the limit in all six degrees at the same

time); and, fourth, the present standards are only good for three degrees.

Since the authors were successful in correlating AP with subjective

data in this work, a further correlation of ISO standards and AP was made.

Figures H.1 and H.2 show a comparison of constant AP levels (across the

frequency spectrum) with the proposed ISO standards for the vertical direc-

tion. Figure H.1 is for one-hour and Figure H-2 is for 4-hour exposure.

These curves were obtained by plotting the ISO curves onto an AP versus

frequency plot to find the mean AP over the 1 to 100 Hz range. It is noted

that in the whole-body frequency range, AP is slightly more conservative; in

the 10 to 100 Hz the two agree; but in the 2 Hz and below, the AP is not as

restrictive as ISO standards. Since AP only accounts for vibration effects,

such things as motion sickness are not accounted for and thus there is justi-

fication for the harsher requirement of ISO standards in this range.

Figures H.3 and H.4 are a similar set of curves comparing constant AP

for fore-aft and side-to-side motion with the single ISO standard of hori-

zontal motion. Perhaps the most important finding in this comparison is

that for each exposure time, the constant AP magnitude was the same for each

of the three directions. Since AP is based on the fact that ride comfort

can be measured by a scaler (i.e., absorbed power), these findings support

this idea of a single number. Table H.1 lists the AP for each of the three

ISO motions.

The final conclusion is that one can use ISO standards as an overall

criterion and can combine more than one degree of freedom by using the AP

H-2

technique to add them up. It thus appears, if the proposed ISO standards

are to be used as a standard, a combination of ISO Standards and the AP

method is required.

The method proposed takes care of the third objection and still leaves

the other three. In particular, the first and fourth are the most severe

limitations.

H-3

Table H. I

Average Absorbed Power Levels to MeetISO Levels for FDP

Exposure Average AP

Time Vertical Side to Side Fore-Aft

1 Min. 8.22 8.22 8.22

16 Min. 4.64 4.64 4.64

25 Min. 3.28 3.28 3.28

1 Hr. 1.47 1.47 1.07

2.5 Hr. .52 .52 .52

4 Hr. .29 .29 .29

8 Hr. .103 .103 .103

To obtain AP for

"exposure limits": multiply AP (FDP) values by 4,

"reduced comfort boundary": divide AP (FDP) values by 9.9225.

H-4

.

oy

I,

O-%

L

0

N.1

Ii

*I_

.I I IO 100

FREQUENCY (Hz)

FIGURE H.l. ISO-Vertical and Vertical Constant Power

H-5FI l l(, :r: -u" A (x'cI

IOO

0

C1

I I 10 100FREQUENCY (Hz)

FIGURE H.2. ISO-Vertical and Vertical Constant Power

H-6

100

I0

00

H-7

FREOUm CY (hZ)FIGURE 11.3. ISO-Horizontal and Side-to.-Side, i'ore-Att Constant Power

H- 7

J~I I( r i-!,r~' In I' .v'

100

(S )

IO

Cq "

4

I

U

.1

000

*1 I i O 100FREQUENCY (HLz)

FIGURE H.4. ISO-Horizontal and Side-to-Side, Fore-Aft Constant Power

H-8

lu!l La n ,mic. 3 x 3 (,Ly c

Documents

REPORT ON OBJECTIVE RDE QUALITY EVALUATION · the Subjective Ratings (Front Seat) for Bus Run 7 . . . 37 4.2 Listing of Absorbed Power (Six Degrees of Motion) with the Subjective