RESISTANCBS on: TWO mass or
mvmmc FITTINGS r-on RECTANGULAR
DUCT:

Theda for Tho Dssrsa of M. S.
MIU‘HGAN STATE COLLEGE
Robert J. Waalkes
19151

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SUPPLEMENTARY

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IN BACK OF BOOK

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RESISTANCES OF TWO TYPES OF DIVIDING
FITTINGS FOR RECTANGULAR DUCTS

By

ROBERT J. WAALKES

A THESIS

Submitted to the School of Graduate Studies of Michigan
State College of Agriculture and Applied Science
in partial fulfillment of the requirements

for the degree of

MASTER OF SCIENCE

Department of Mechanical Engineering

1951

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ACKNOWLEDGMENTS

The author wishes to express his sincere appre-
ciation for the consultation and guidance of Dean L. G.
Miller of the School of Engineering, and for the assist-
ance of Professor C. H. Pesterfield of the Department of
Mechanical Engineering.

He wishes also to acknowledge the work of Mr. L.
A. Yerkovich and Mr. J. H. Yohn who have previously
worked on this project. Material from their theses has
been re-evaluated and made a part of this paper.

Mr. Donald Seble and Mr. Carl Redman are also to
be thanked for their assistance and cooperation in the

laboratory.

2558711

TABLE OF CONTENTS

PAGE

INTRODUCTION . . . . . . . . . . . . . . . . . . 1
GENERAL APPROACH TO PROBLEM . . . . . . . . . . . 3
DESCRIPTION OF TESTING EQUIPMENT . . . . . . . . 6
Volume Measuring Station . . . . . . . . . . . 6
Static Pressure Measuring Station . . . . . . . 10
Orifice Plates . . . . . . . . . . . . . . . . 12
ORIFICE CALIBRATIONS . . . . . . . . . . . . . . 14
TEST PROCEDURE .. . . . . . . . . . . . . . . . . 26
First Straight Type Fitting . . . . . . . . . . 31
Second Straight Type Fitting . . . . . . . . . 33
Third Straight Type Fitting . . . . . . . . . . 33
Actual Measured Lengths . . . . . . . . . . . . 4O
CALCULATIONS . . . . . . . . . . . . . . . . . . 41
DISCUSSION . . . . . . . . . . . . . . . .-. . . 47
CONCLUSIONS . . . . . . . . . . . . . . . . . . . 53

DATA SEETS O O O O O O O O O O O O O O O O O 0 O 5 6

LIST OF ILLUSTRATIONS

FIGURE
1. General View of Test Equipment . . . .
lA. Layout of Test Equipment . . . . . . .
2. Volume Measuring Station . . . . . . .
3. Static Pressure Measuring Station . .
4. Typical Orifice Plates . . . . . . . .
S. Fittings Tested . . . . . . . . . . .
6. Increaser Fitting in Place . . . . . .
7. Straight Fitting in Place . . . . . .
8. Orifice Plate Being Placed in Position
9. Damper Adjustment Being Made . . . . .
10. Set-up for Runs 87-118 . . . . . . . .
11. Set-up for Runs 119-147 . . . . . . .
l2. Set-up for Runs 148-176 . . . . . . .

CURVE SHEETS

1‘60
7-9.
10.

11.

Orifice Calibrations . . . . . . . .
Friction of Branch Ducts . . . . . .
Frictional Effect on Takeoff Branch,
Increaser Type . . . . . . . . . .
Frictional Effect on Takeoff Branch,

Straight Type . . . . . . . . . . .

PAGE

7
Pocket

9
11
13
27
28
29
3O
32
3A
36
38

17
23

Pocket

Pocket

CURVE SHEETS PAGE

12. Frictional Effect on Straight Branch,

Increaser Type . . . . . . . . . . . . . . Pocket

l3. Frictional Effect on Straight Branch,

Straight Type . . . . . . . . . . . . . . Pocket

--------

 

 

INTRODUCTION

The objective of this research project, which is
a cooperative effort of the American Society of Heating
and Ventilating Engineers and Michigan State College, is
to determine the resistance offered to the flow of air
by dividing fittings for rectangular ducts wherein a
portion of the air stream is diverted ninety degrees and
the remainder is carried on straight in a branch of re-
duced size. At the present time there is little pub—
lished data available on the frictional effect of such a
fitting on the diverted branch, and practically no in—
formation as to the effect on the branch (or reduced
main) which continues straight.

The original project proposed the testing of
three different designs of fittings, with three combina-
tions of branch sizes for each design. Tests of the
three fittings of the first design were completed by
Mr. L. A. Yerkovich and Mr. J. H. Yohn, and the three
fittings of the second design have been tested by the
author. This paper presents the complete data and re-
sults obtained with the second three fittings, and in-
cludes a re—evaluation of the data and results of the
first three fittings. Hence, the conclusions and recom-

mendations given herein are based on an examination of

2
the results from tests of six of the originally proposed
nine fittings.

The results given are empirical results obtained
by actual test, and it is not within the scope of this
paper to present an analytical interpretation. Such an
interpretation should await the completion of the test-
ing program when all variables will have been considered,
and a significant interpretation can be attempted. The
empirical results can be used as an interim guide for
designers of air handling systems until such time as a
rigorous analysis of the mechanics of flow involved can

be made to explain and verify the test results.

GENERAL APPROACH TO PROBLEM

From a study of the problem it appears that the
losses in the fitting will be dependent on several fac-
tors, namely: (1) the design of the fitting; (2) the
respective sizes of the "takeoff" and "straight"
branches; (3) the equivalent length of the two branches;
(4) the relative proportions of air flowing through the
two branches; and (5) the total quantity of air flowing
through the fitting. These factors therefore become the
variables in the test program.

The first two variables are taken care of by the
selection of the three designs of fittings and the three
combinations of branch sizes previously mentioned.

To keep the duct system from becoming cumbersome
and at the same time provide a means for measuring the
flow through the two branches, the equivalent lengths
are varied by providing a series of rectangular sharp-
edged orifice plates for each branch. These are insert-
ed in the branch duct downstream of the fitting, and si-
multaneously change the equivalent length of the branch
and the amount of air flowing through it. The orifice
is used to measure the quantity of air flowing through
the branch by calibrating it against a static pressure
reading taken Just ahead of it.

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The fifth variable is controlled by means of a
damper placed in the main duct well back toward the
blower. The total volume of air flowing through the
system is varied by adjusting this damper in increments
from the open position to the closed position.

It is desired to express the resistance offered
to flow by the dividing fitting as an added equivalent
length for each branch. This is accomplished by the
taking of data which together with the necessary calcu-
lations leads to the determination of the total pressure
drOp from a point in the main duct just upstream of the
fitting to a point in each of the branch ducts down-
stream of the fitting. These total pressure drops rep-
resent losses between the two points, and are converted
to equivalent lengths by use of the friction chart and
observed data on quantity of flow and duct size for each
branch. The subtraction of the actual measured length
between the points in each case then gives the added
equivalent length of the branch due to the dividing fit-
ing.

This procedure is repeated for each setting on
each of a series of runs made with the above factors as
variables. The final plot of all these added equivalent

lengths, with average curves drawn, then gives a picture

of the frictional effect of the fitting over a wide

range of flow conditions.

DESCRIPTION OF TESTING EQUIPMENT

A general view of the testing equipment is shown
in Figure l, and a layout is shown in Figure 1A in the
pocket at the end of the paper. It consists of a cen-
trifugal blower connected to a system of ductwork with
quadrant damper, ASME long radius nozzle, test fitting,
static taps, and sharp-edged orifices located as shown
in the layout. The equipment is located in the Mechan-
ical Engineering Laboratory of Michigan State College
and is still set up for further testing.

The blower used to supply air to the system runs
at a constant speed of about 1290 R.P.M., and the total
volume of air handled is varied by means of the quadrant
damper.

For purposes of description and discussion the
balance of the testing equipment is divided into a vol-
ume measuring station, a static pressure measuring sta-

tion, and orifice plates.
Volume Measuring Station

On the layout, Figure 1A, this station is shown
simply as a nozzle in the 14" main duct preceded by an
egg-crate type straightener to smooth out the flow con-
ditions at the nozzle entrance. The nozzle is an ASME

long radius type which is used when the ratio of throat

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to pipe diameter is 0.53 or less. This type nozzle is
shown in Figure 20, page 29 of "Power Test Codes," pub-
lished in 1940 by ASHE. The contour of the nozzle is a
semi-ellipse with the contracting portion followed by a
cylindrical section of the same diameter as the throat,
which is six inches. A static tap and impact tube are
used with the nozzle to measure the velocity pressure.
The static tap is in the straight portion of the nozzle
two inches from the end as shown in Figure 26e, page 37,
cfl'“Power Test Codes." The impact tube is located in
the center of the nozzle jet with the end of the tube in
the plane of the nozzle end.

Figure 2 is a view of the volume measuring station
showing the large Uehling Type B inclined draft gauge
and smaller Ellison inclined draft gauge, with the
flange of the nozzle, the impact and static tubes visible
on the main duct. The range of the Uehling instrument
is O to 8 inches of water, and that of the Ellison gauge
is 0 to 0.5 inch of water. The two gauges are connected
in parallel to the static and impact tubes and thus read
the velocity pressure (P3 - P2) directly. The Ellison
gauge is used for more accurate reading of low velocity

pressures o

 

 

FIGURE 2

VOLUME MEASURING STATION

10

Static Pressure Measuring Station

The static pressure measuring station is located
at the point where the fitting under test divides the
main duct into two branches. The location of the static
taps is shown on Figure 1A. On the data sheets, P4 is
the pressure at the static tap in the main duct upstream
of the fitting, P5 is the pressure at the static tap in
the straight branch downstream of the fitting, and P6 is
the pressure at the static tap in the takeoff branch
downstream of the fitting.

Figure 3 shows the static pressure measuring sta-
tion with the dividing fitting and ductwork in place.
The three Ellison draft gauges are used in measuring the
static pressure at the three taps. The ranges of the
gauges are 0-0.5, 0-1.0, and 0-3.0 inches of water.

Each of the three taps are connected to a single instru-
ment connection by means of tees in the rubber tubing.
The insertion of a glass stopcock in the tubing from
each tap makes it possible to connect each of them to
the gauge separately. The pressures are thus read con-
secutively on the same instrument, eliminating the er-
rors which may arise when a separate set of gauges is
used at each tap. The three gauges are necessary to

read accurately the range of pressures encountered.

 

FIGURE 3

STATIC PRESSURE MEASURING STATION

11

l2
Orifice Plates

All of the orifice plates used are rectangular
sharp-edged orifices, and their general location is
shown on Figure 1A. A set of typical orifice plates for
the 3" x 8" size duct are shown in Figure 4. The sizes
of orifices used in other branch ducts are shown in
Table I. There are two of each of the orifice sizes
listed for the 10%" x 8" branch duct since in this case
the two branches are the same size.

The branch ducts are provided with special U-
shaped channels about 3/'" deep soldered to the inside
of the duct on three sides. The edges of the orifice
plates slide in these channels, and a slot is cut in the
fourth side of the duct, permitting the insertion or re-
moval of an orifice plate from the outside without dis-
turbing the ductwork. Masking tape is used to seal the
crack between the orifice plate and the duct to elimin-

ate leakage.

13

61/4 X 11/4

 

 

FIGURE 4
TYPICAL ORIFICE PLATES USED IN 3" x 8" BRANCH DUCT

ORIFICE CALIBRATIONS

The rectangular sharp-edged orifices used in the
branch ducts to increase the equivalent lengths of the
branches and vary the proportion of air flowing through
them must be calibrated if they are also to be used for
measuring the quantity of air flowing in each branch.
This calibration is accomplished by putting a blank in
place of the orifice in one branch and causing all of
the air to go through the other orifice. The quantity
flowing is varied by means of the quadrant damper, and
measured at the main volume measuring station. The cal-
culated quantity of flow in cubic feet per minute is
then plotted against the static pressure reading at the
tap near the sharp-edged orifice to establish the cali-
bration curve of the orifice.

Curve Sheets 1 - 6 are the calibration curves for
the orifices used in this investigation. It will be
noted that similar sized orifices in the two branches as
shown on Curve Sheets 1 and 2 have similar calibration
curves within very close limits, indicating that the
calibration is good whether the orifice is in the
straight branch or in the takeoff branch. This is fur-
ther emphasized by the fact that Curve Sheet 3 which
represents the large-sized orifices in the takeoff

branch agrees very closely with Curve Sheet 6 which is

15

for the same orifices in the straight branch. The same
agreement exists between Curve Sheets 4 and 5 for the
small-sized orifices.

Curve Sheets 7 - 9 are plots of the frictional
resistance of different lengths of ducts of the three
sizes used for branch ducts in this work. They are
drawn from data taken from the friction chart in the
1950 ASHVE GUIDE. The purpose of these curves is to de-
termine the equivalent lengths of the various sharp-edged
orifices. A comparison of Curve Sheets 4 and 7, for ex-
ample, shows that the 7“.x 2" orifice is equivalent to
about #8 feet of 5.8" round duct. Table I gives the ap-
proximate equivalent length of the various orifices in
terms of feet of the size duct in which they are used.
These values are approximate because it will be noted
that the orifice calibration curves have a lesser slope
than the duct curves, and hence at low rates of flow the
equivalent length of a given orifice is less than at
higher rates of flow. The equivalent lengths given in
Table I are the mean value taken at the mid-length of

the orifice curve.

l6

 

 

 

TABLE I
“3°33‘c‘iularE1‘fifiiifmogggce 2231;332:126
Size Size Length
3" x 8" 5.8" 6" x l" 480'
3" x 8" 5.8" / 6 1/4" x 1 1/4" 230'
3" x 8" 5.8" 6 1/2" x 1 1/2" 135'
3" x 8" 5.8" 7" x 2" 48'
10 1/2" x 8" 10.0" 7" x 4 1/2" 305'
10 1/2" x 8" 10.0" v 8" x 5 1/2" 115'
10 1/2" x 8" 10.0" 8 1/2" x 6" 69'
10 1/2" x 8" 10.0" 9" x 6 1/2" 43'
18" x 8" 12.7" ,“’ In" x 4" 275'
18" x 8" 12.7" 15" x 5" 118'
18" x 8" 12.7" 15 1/2" x 5 1/2" 70'
18" x 8" 12.7" 16" x 6" 46'
18" x 8" 12.7" 16 1/2" x 6 1/2" 31'

 

 

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MLIT-232

MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

Running Log of

Sheet No.

 

 

 

 

 

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Date

 

, 19—

 

ML|T1232

Running Log of

MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

Sheet No.

 

 

 

 

m1

 

 

orator—t No.

(cm-065014?-

NHHHHI—‘I—‘HI—IHH

1

25 1

Remarks: I

 

Date

 

, 19—.

 

TEST PROCEDURE

The general outline of the test procedure is to
select a particular style fitting in one of the three
combinations of branch duct sizes; make a series of runs
on this fitting with the variable between runs being the
combination of orifice sizes in the branch ducts and the
variable for each individual run being the total volume
of air flowing through the system; and then replace the
fitting with another one and repeat the process until all
fittings have been tested.

Figure 5 shows the fittings which have been test-
ed. This paper covers the test work on the straight
type fittings D, E, and F, and includes an analysis of
the test results on fittings A, B, and C as previously
‘mentioned. Figure 6 is a view of fitting B in position
ready for test, and Figure 7 is a similar view of fit-
ting E. ‘

After the fitting and branch ducts are put in
place, orifice plates are inserted in the U-channel fix-
tures in the branch ducts as shown in Figure 8, the
damper is opened wide, and the blower is started to be-
gin the tests. The data taken consists of the velocity
pressure P3 - P2 in the volume measuring nozzle, the
static pressures P4, P5, and P6 as described on page 10,

the wet and dry bulb temperatures of the air, and the

27

 

 

fix N m? 9.. 1K «LN-K T11. K 4 3c m Egan—”rm
\xc. ... .1 k. {b “3&1. 1... -.1?

 

QNk-nflwk WWZFNKTK

1w.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

NnKXK WNWWNQr-ver

 

1‘-” ~— -(.’ —————— ——«>—1
4.

 

 

 

 

 

 

 

 

 

28

 

FIGURE 6

INCREASER FITTING IN PLACE.

 

FIGURE 7

STRAIGHT FITTING IN PLACE

29

 

FIGURE 8

ORIFICE PLATE BEING PLACED IN POSITION

3O

31
barometer reading. These data are taken for each of
about eleven different settings of the damper control-
ling the volume of air flowing. The damper is adjusted
in increments from the wide open position to the fully
closed position which varies the quantity of air flowing
from about 1750 cfm to 200 cfm. Figure 9 shows this ad-
Justment being made. These eleven points comprise one
run, and one or both of the orifice plates are then
changed to set up the next run.

In the taking of the data, the velocity pressure
P3 - P2 is read on the 8" inclined draft gauge (on the
0.5" gauge for low pressures) after a steady state is
reached following the damper adjustment. The static
pressures P4, P5, and P6 are read on the 3", l", or 0.5"
gauge as required. The arrangement permitting all three
pressures to be read on the same gauge eliminates the
possibility of variation between instruments, but causes
some loss of time since for considerable variations in
pressure additional time is required for the instrument

to settle out.
First Straight Type Fitting

The first straight type fitting tested was fit-
ing E. The set-up of the fitting and orifice plates

for the series of runs on this fitting is shown in

 

FIGURE 9

DAMPER ADJUSTMENT BEING MADE

32

33

Figure 10. There are four different sizes of orifice
plates for each branch duct, making a total of sixteen
possible combinations. The EISposition of orifices in
the individual runs is given in Table II, and the cali-
bration curves for the orifices are on Curve Sheets 1

and 2.
Second Straight Type Fitting

Fitting F was the second straight type fitting
tested. Figure 11 shows the set-up of the fitting and
orifice plates for this series of runs. Five different
orifices for the takeoff branch and four for the
straight branch make a total of twenty runs in this
case. Table III gives the disposition of orifices for
the individual runs, and the calibration curves for the

orifices are on Curve Sheets 3 and 4.
Third Straight Type Fitting

The third straight type fitting tested was fit—
ting D. It is the reverse of fitting F, and the same
orifice plates are used as for fitting F giving again a
series of twenty runs. The set-up for this series is
shown in Figure 12, and Table IV shows the combination
of orifices for each run. Curve Sheets 5 and 6 are the

orifice calibration curves in this case.

34

 

SET-UP Foe Bax/vs 67-//c‘5

 

 

 

 

 

 

 

 

 

 

 

4; 5m T/C TAP-w—

OE/F/CE PLATE—L

FIGURE 10

 

 

.11L
’1
ZOHx 8 N
x; STAT/C 7‘HP———~~1 -——~~--—u--»0~~--- -- 1
r / I /”
r - 4 __.-..----“ we: ~-—-:.~
1
l
= r
L I 1%
1‘ l o 1*
“N I RI
‘3 :A.
I ‘
/ 4-12 5771 NC TAP L
/ 11
4 0/2 lF/CE PLATE ‘ . 11"“

 

 

 

 

_3 u

 

 

TABLE II

 

 

Orifice Sizes

 

 

Run
N°‘ Straight Take-off
95 911 x 6 1/211 9" x 6 1/211
96 ll 8 1/211 X 6"
97 n 8" x 5 1/211
98 II 7" x 4 1/2"
100 8 1/2" x 6" 9" x 6 1/2"
101 " 8 1/'" x 6"
102 n 8" X 5 1/211
103 u 7" x 4 1/2"
105 8" x 5 1/2" 9" x 6 1/2"
106 " 8 1/2" x 6"
107 u 8" x 5 1/211
108 " 7" x 4 1/2"
110 7" x 4 1/2" 9" x 6 l/2"
lll " 8 1/2“ x 6"
112 " 8" x 5 1/2"
113 " 7" x 11 1/2"

 

 

 

JEr-UP Foe BUN: //.9-/47

 

 

P o‘mr/c TAP mm»

4.

-~<——— // ’—’—+++————-—- 9 ’—/ ”-———«—~»«

m

 

20'} {3’ ”

__.___ ___1_> 0 --.—__.,___v_.— 4

 

 

 

 

 

/8 "x 8 ”

 

 

A
v

 

 

 

 

 

Z '
x2 JTflT/C TAP I;

OE/F/CE PLATE

OE/F/CE PLATF—~~.

FIGURE 11

 

 

 

 

 

2.4

——>—:-<——-—/

/ I

I I
f‘-
a 44

57A T/C TAP ———1>Ov -

 

 

 

37
TABLE III

Orifice Sizes

   

 

 

Run

NO‘ Straight Take-off
128 7" x 2" 16 1/2" x 6 1/2"
129 u 16" x 6"

130 " 15 1/2" x 5 1/2"
131 n 15" x 5"

132 n 14" x 4"

133 6 1/2'4 x 1 1/2" 16 1/2" x 6 1/2"
134 n 16" x 6"

135 " 15 1/2" x 5 1/2"
136 n 15" x 5"

137 u 14" x 4"

138 6 1/4" x 1 1/4" 16 1/2" x 6 1/2"
139 " 16" x 6"
140 " 15 1/2" x 5 1/2"
141 N 15" X 5"
142 " 14" x 4"
143 6" x 1" 16 1/2" x 6 1/2"
144 Ii 16" X 6"
145 " 15 1/2" x 5 1/2"
11’s it 15" x 5"
147 u 14" X 4"

 

 

38

 

 

SET-UP FOE £70va /4<5-/76

 

 

5; 57A T/C TAP

I, ”
.,.( .1-/{3% _>1.<___1_1._.-_3 ’_ 7 :5 __.,1

 

 

 

 

 

 

 

 

H
X

1

‘7) f"

 

 

 

 

”i
0 «g4 -.1[;;/,

 

 

LP JTAT/C TAP

6
OBIF/CE PLATE

 

 

 

Ag. STAT/C TAP

 

OE/F/CE PLATE-1

Y
i
w
77‘

 

N

L—//

 

 

 

FIGURE 12

 

 

39
TABLE IV

Orifice Sizes

 

 

Run

No. Straight Take-off
157 16 1/2" x 6 1/2" 7" x 2"
158 16" x 6" "
159 15 1/2" x 5 1/2" "
160 15" x 5" n
161 14" x 4" "
162 16 1/2" x 6 1/2" 6 1/2" x 1 1/2"
163 16" X 6" n
164 15 1/2" x 5 1/2" "
165 15" X 5" II
166 14" x 4" "
167 16 1/2" x 6 1/2" 6 1/4" x 1 1/4"
168 16" x 6" "
169 15 1/2" x 5 1/2" "
170 15" x 5" N
171 14" x 4" "
172 16 1/2" x 6 1/2" 6" x 1"
173 16" x 6" "
174 15 1/2" x 5 1/2" "
175 15" x 5" II
176‘ 14" x 4" "

 

 

40

Actual Measured Lengths

The actual measured lengths from static tap P4 to

static taps P5 and P6 are:

First fitting:

Straight 11.98 feet

Takeoff . . . . . . . . 12.69 feet
Second fitting:

Straight . . . . . . . 6.35 feet

Takeoff . . . . . . . . 12.48 feet
Third fitting:

Straight . . . . . . . 10.56 feet

Takeoff . . . . . . . . 6.39 feet

 

CALCULATIONS

The obJec tive of the calculations is to develop
from the observed data the amount of the total pressure
loss from a point in the main duct upstream of the di-
viding fitting to a point in the branch duct downstream
of the fitting: to express this loss as an equivalent
length of branch duct; and finally, by subtraction of
the actual length between these two points, to determine
the added equivalent length due to the fitting.

Briefly, the steps required to do this are:

1. From observed velocity pressure and area of
main measuring nozzle calculate total quantity of air
flowing (Q4).

2. From total quantity of air flowing and area
of main duct at static tap P4 calculate velocity pres—
sure at plane of tap (VP4).

3. By addition of calculated velocity pressure
and observed static pressure obtain total pressure at
static tap P4 (TPA).

4. From observed static pressure P5 and orifice
calibration curve determine cfm through straight branch
duct (Q5).

5. From Q5 and area of duct at tap P5 calculate
the velocity pressure at plane of tap (VP5)'

42
6. By addition of calculated velocity pressure
and observed static pressure obtain total pressure at

plane of tap P5 (TP5)-

7. 8. 9. By steps similar to 4, 5, and 6 ob-
tain total pressure at plane of tap P6 (TP6).

10. By subtraction obtain total pressure losses
between planes of taps P4 and P5, and P4 and P6.

‘11. From quantity flowing in branch and equiva-
lent branch duct diameter, determine friction loss per
100 feet from friction chart.

12. By dividing total pressure loss (times 100)
between planes of static taps by friction loss per 100
feet, obtain equivalent length between planes of taps.

13. By subtraction of actual measured length be-
tween planes of static taps from equivalent length be-
tween same, obtain added equivalent length due to divid-
ing fitting.

14. 15. 16. Repeat steps ll, 12, and 13 for
second branch.

Actually, a modification of steps 5 and 8 above
is necessary, since the values of Q5 and Q6 as obtained
in steps 4 and 7 do not sum up to precisely equal Q4
(step 1). It is felt that this is due to inability to
read the inclined draft gauges accurately to three

places, and that since the orifices are calibrated

43
against the main nozzle to begin with, it is most con-
sistent to use the Q4 value as being correct. There-
fore, the values of Q5 and Q6 from the calibration
curves are added, and Q6 divided by the total to obtain
the percent diverted into the takeoff branch. This per-
centage of the correct total cfm (Q4) then is a correct-
ed quantity of flow through the takeoff branch (Q6c),
and by subtraction (Q4 - Q6c) a corrected value of the
quantity flowing in the straight branch (Q50) is ob-
tained. These two values then are used in steps 5 and

8, and the calculations carried to completion.

Following the above outline, a sample calculation

appears as follows (see Run 95, line 1):

 

Observed Data: P3 - P2 P4 P5 P6
4.91 .185 .155 .145
1. Q4 = A-V = A'4005 /H = .1962(4oo5) /P§‘:5FE

785.78 /F§‘='FE = 785.78(2.22)
1744 cfm.

2. Q4 = A-4005 /h’= A4:4005 /VF;
NF; = Q4/[(A4)(4005)1 = Q4/[(l-111)(4005)]
= .OOO225Q4
VP4 = (.OOO225Q4)2 = (.392)2 = .154"H20

44
3o TPI]. = VP4 + SP4 = .154 + .185 = .339"H20

4. From Curve Sheet 2 and P

Q

5 .155:

5 = 895 cfm

.145:

4a. From Curve Sheet 1 and P6
Q6 = 828 cfm

4b. 616/192,5 + Q6) e 828/1723 = .481 = 48.1% diverted
Q6c ==$ Div.(Q4) = .481(1744) = 839 cfm

Q = Q4 - Q6c = 1744 839 = 905 cfm

5c

5. NF; -—- QSC/[(A5)(4005)] = Q5c/[-583(4005)]
= .000428Q5c
2 2 n
VP5 = (.OOO428Q50) = (.387) = .150 H20

5 5 5

7. See 4a.

ll

8. ATP—6‘ asc/[(A6)(4005)] = Qgc/[.583(4005)]
.000428Q6c

(.000428Q6c

ll

VP6 )2 = (.359)2 = .129"H20

9. TP6 = VP6 + SP6 = .129 + .145 = .274"H2O

 

10.

ll.

12.

l3.

14.

15.

16.

45

TPI} "' TP5 = 0339 " e305
TP4 - TP6 = 0339 ‘ .274

.034"H20

.O65"H2O

From friction chart (ASHVE GUIDE, 1950), with
Q5c a 905 cfm and diameter = 10":

Friction loss per 100 feet = .410"H20

Equivalent length

(TI?4 - TP5)/(F.L./lOO) x 100
(straight branch)

.034/.410 x 100 = 8.29'

Added equivalent length = 8.29 - 11.98 = -3.69'
(straight branch)

From friction chart (ASHVE GUIDE, 1950), with
Q6c = 839 cfm and diameter = 10":

Friction loss per 100 feet = .360"H 0

2

Equivalent length

(‘1?4 - TP6)/(F.L./100) x 100
(takeoff branch)

.065/.360 x 100 = 18.06!

Added equivalent length = 18.06 - 12.69 = 5.37'
(takeoff branch)

As indicated in the sample calculation, all of the cal-

culations so far as possible are done on a calculator.

46
All operations on the calculator are carried to four
significant figures in the intermediate steps, and then
the values are rounded back to three places in most
cases for recording on the data sheets. It is felt that
this is sufficiently accurate for final values since the
reading of the manometers at very best can be done to
only three places. Values rounded off to four places
are carried on the calculator to minimize distortion of

the data in multiplying and dividing operations.

DISCUSSION

Early in the test work it was found that air
leakage from the ductwork was sufficient to affect the
accuracy of the data being taken. Therefore, all of the
Joints in the ducts downstream of the main measuring
nozzle are soldered, including the longitudinal Pitts-
burgh lock seams. The fittings are provided with gas-
keted flange Joints to eliminate leakage and permit
changes to be made easily. Every time a new fitting is
put in place a check is made to determine the extent of
leakage by closing off both branches with blanks in
place of the sharp-edged orifices, thus putting the en-
tire duct system under high static pressure. If any ap-
preciable quantity of air is detected flowing through
the main nozzle, the leaks are located and corrected be-
fore proceeding with the tests.

Similarly, the rubber manometer tubing is checked
for leakage periodically to prevent errors in readings
from this source. This is easily done by forcing the
liquid to the high end of the gauge and clamping off the
tubing near the static tap in the duct. If the liquid
does not drop, there is no leak in the tubing, stopcock,
or connections.

As indicated in the Test Procedure, the wet and

dry bulb temperatures of the air and the barometer read-

48
ing are recorded for each run. These three items have
not been used in this paper since all calculations are
based on standard air. They are recorded in the event
that such refinement of the data appears necessary or
desirable after further study.

In the section of the paper on Orifice Calibra-
tions it is pointed out that the slope of the calibra-
tion curves of the orifices is less than that of the
ducts they are used to represent. This means that the
equivalent length of duct represented by an orifice is
not a constant, but increases with increasing rates of
flow. Since the variable from point to point in any
given run is the rate of flow through the system, the
equivalent length of the branches for the several
points of the run will be somewhat different. However,
this will not adversely affect the results obtained.

The slope of all the orifice calibration curves is the
same, and hence the variation of equivalent length with
changing rates of flow will be proportionally the same
for all orifices. Therefore, the basic function of the
orifice plates (which is to vary the proportion of air
flowing through the two branches by varying their equiv-
alent lengths) is still satisfactorily performed. That
this is true is borne out by the fact that the percent of

air diverted remains essentially constant throughout a

49
run except for points of obvious experimental error.

In looking over the data sheets it will be noted
that the last two or three points of a run are frequent-
ly completely out of line with the values of the other
eight or nine points. This is principally due to the
fact that the static pressures observed at these points
are of the order of .001 - .005 inches of water, and hence
cannot be read very accurately on a 0.5" inclined draft
gauge. Those points which are obviously erroneous have
not been used in plotting the final curves.

On Curve Sheets 10, ll, 12, and 13 in the pocket
at the end of the thesis the resistance of the dividing
fitting expressed as an added equivalent length in feet
of branch duct is plotted against a ratio of average
lower velocity to average higher velocity in the branch
ducts. Thus the ratio is always less than one, and is
either VS/V6 or V6/V5 depending on the respective veloc-
ities in the straight branch (V5) and the takeoff branch
(V6). Curve Sheets 10 and 11 show the effect on the
takeoff branch of the increaser and straight type fit-
tings respectively, and Curve Sheets 12 and 13 show the
effect on the straight branch of these same fittings.

An inspection of the curves for the takeoff branch
shows first that there is no significant difference be-
tween the two types of fittings tested. It is further

5O
evident that the added equivalent length of the takeoff
branch due to the dividing fitting is always positive,
and is a maximum when the average velocity in the take-
off branch is about one-fourth the average velocity in
the straight branch. This maximum point represents a
condition of a small size takeoff branch of very long
equivalent length (about 480') with a very low velocity
as compared to the straight branch. An important point
to note here is that in actual practice a long equiva-
lent length will naturally result in a lower quantity of
flow (for a given available pressure for causing flow)
and consequent lower velocity, and therefore a bad situ-
ation becomes worse. It may also be noted that the
losses are not excessive when the average velocities in
the two branches are within twenty percent of each
other, and are a minimum when the takeoff and straight
branches are of equal size and the velocities range from
equal to twenty-five percent higher in the takeoff
branch. Finally, the curves show that whenever the av-
erage velocity in the takeoff branch is higher than that
in the straight branch the added equivalent length of
the takeoff branch due to the dividing fitting is within
the range of 4 to 15 feet. '

Looking next at the curves for the straight branch

on Curve Sheets 12 and 13, it is again evident that

51
there is no significant difference between the increaser
and straight type fittings. In this case, however, it is
seen that the added equivalent length is not always pos-
itive; in fact, for straight branch sizes of 10% x 8" and
18" x 8", practically all of the values taken from the
curves fall within the range of O to -4 feet. This in-
dicates that for these two sizes of the straight branch,
the equivalent length from the plane of static tap P4 in

the main duct to the plane of static tap P in the

5
straight branch is less than the actual measured dis-
tance between the two points. In other words, some
transfer of energy from the takeoff branch to the
straight branch is taking place to give these negative
losses.

The third curve on these sheets representing the
added equivalent length for a 3" x 8" straight branch
has different characteristics. The minimum value here
is 8 to 10 feet at a ratio of velocities of very nearly
one, and reaches a maximum when the average velocity in
the straight branch is about one-fourth that in the take-
off branch. This maximum point represents a condition
of a small size straight branch with a very long equiva-
lent length (about 480') and a very low velocity as com-
pared to the takeoff branch. The phenomena which causes

this curve to shift from the region of negative added

52
equivalent lengths for a 10%" x 8" straight branch to
the positive region with a minimum value of about 10
feet for a 3" x 8" straight branch cannot be explained
with the data available at this time. Additional tests
should be run using a similar dividing fitting with a
straight branch (or perhaps more than one) of an inter-
mediate size to determine what happens in this region.
From the present curves it appears that there may be a
family of curves obtained when the straight branch size
is increased in increments from the 3" x 8" size to the
10%"x 8" size. With further increases in size the added
equivalent length of the straight branch seems to become
almost a constant value of from -2.5 feet to -4.0 feet,

as shown by the curves for the 18" x 8" straight branch.

CONCLUSIONS

From the data and results presented in this paper

the following conclusions can be drawn:

1. There is no significant difference in the re-
sistance offered to flow by the two types of fittings

tested, known as “Increaser" type and "Straight" type.

2. For all conditions of flow, the added equiva-
lent length of a takeoff branch due to a dividing fitting

is a positive value of 4 feet or more.

3. The maximum added equivalent length of a
branch, due to a dividing fitting, exists when the av-
erage velocity in the branch is a minimum as compared to
the average velocity in the other branch. This holds

true for both the takeoff and straight branches.

4. The minimum added equivalent length of a
branch, due to a dividing fitting, exists when the ratio
of the average velocity.in one branch to the average ve-
locity in the other branch (taken so the ratio is less
than one) is within the range 0.85 - 1.0. Within these
limits, the added equivalent length of the straight
branch varies from -4 to 11 feet, and that of the take-

off branch varies from 4 to 15 feet.

54
5. For the usual condition encountered in prac-
tice where the straight branch is actually a continua-
tion of the main in reduced size, and hence usually is
at least equal to the takeoff branch in size, the added
equivalent length of the straight branch is negative,

ranging from 0 to -4 feet.

6. For the usual condition mentioned in 5 above,
the added equivalent length of the takeoff branch is
about 10 feet if the average velocity in the takeoff
branch is 80% or more of the average velocity in the

straight branch.

7. A condition of a small branch of long equiva-
lent length, with a low velocity in the branch, should
be avoided. Under these conditions the added equivalent
length of the branch due to the dividing fitting may be-
come as much as 112 feet for the straight branch and 143
feet for the takeoff branch.

8. In any layout where the flow may be critical,
the ratio of velocities in the branches of a dividing
fitting should be checked and held as close to unity as

possible.

9. This research should be continued to deter-

mine whether the third design of fitting, a "Decreaser"

 

55

type, shows different characteristics from the present
two fittings. In addition, it is desirable to extend
the present data on the small (3" x 8") branches by mak-
ing up orifices smaller than the 14" x 4" for the large
branch (18" x 8") to determine what happens to the added
equivalent length of this small branch when its velocity

exceeds the velocity in the large branch.

 

DATA SHEETS

Data sheets lOA-85A following record the recalcu-
lation of added equivalent lengths for the increaser type
fittings. Data for these calculations were taken from
the thesis "Friction Equivalents of Take-offs in Rectan-
gular Ducts" by James Harold Yohn, Michigan State Col-
lege, 1950.

Data sheets 87-176 and 95A-l76A record the origi-
nal data and all of the intermediate and final calcu-
lated values for the straight type fittings as tested by

the author.

/04

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

aura): Sheet No.
MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE
RunningLonol
Ola-aven{ { Date 19 _

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NUT-232 Sheet No.
MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE
RunningLO‘o‘
Observers{ { Date 19 _
[ .7
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“LIT-232

MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

Sheet I‘m—lai—

 

 

 

 

 

 

 

 

 

 

 

 

 

RunningLogof
DWI I Date 19—
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HLIY-zaz Sheet No.
MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE
Runninglmol
Observen{ { Date 19 _
I I ’ I
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ram-232 Sheet No, 1 4A

MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

RunnlnflLoflof
om{ { Date 19 _
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“LIT-232 Sheet No. lfé
MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE
RunningLo‘of
OW{ I Date 19 _
I . I I I : I
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Sheet No._Lé.L_

HUT-232

MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Remarks:

 

 

 

RunningLocof
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uur-zaz Sheet No.
MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE
RunningLogof
DWI I Date 19 _
II I I I
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......m Sheet No. /XA
MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE
RunningLo‘of
omI I .... .. _
I I
I
I 57-: 4.604 r 7‘74KEo/rr: :
6 I I A0050 040050 I
W 50.1.. Ac 71.45904 . 5509.0449023040. 5524.050410-
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6 -077 0.47 “All .//0 17.08 72.78.
7 -046 6.5.2 “£08 .001 “4:20 18./0
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9. -02.! 71.4.7 0.8.1. .027..13.7o Imao.
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nut-232 SM No. I 9A

MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

 

Running Log of

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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9I .03.: I/ojéI ~ 0.26. .. 0/6: 30.00 23.90.
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11‘12'1" .0063 14.28 10 (9” 3.1.3 5.8". — -"' (0.! "'

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MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE
RunningLogof
°m{ - { Date . 19 _
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6 II.08’S‘ 9.4—2. -I./8’ -037 38.50. 32.910
7. 7504-7 /0.20. —a.4—0 . .023 +1.30 595.20,
8 II.035' 10.00. 70.60 . -0/é I40.60 34.50
9 I.021I 3.641 I-/.9b ? .0// 37.21; ISL/5'.
10. II . 01.5 I /0.00 I 32.60 i .006]. 444.2: 38.15"
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Sheet I‘m—2&—

MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

Running Lo. of

 

 

 

 

 

 

 

 

 

S'T/efl/Gflr

6 ; ADDED
2 gm). Alf/loo 56L; A6714._E.g_._4.__._

 

 

112,7”.370 7.84 /0.6' -.?.7b
2 1.350 . 7.88 . -.7.71
3 __.Aba Y.“ . _'.?./4
4 .190 . 2.43 ,. ‘2./7.
5 .140 8.57 -a.oa
6 .086 , 7.30 -/.30
7 .0116 10.86 0.16
8 .037 /o.8o 0.2.0
9 .034 ”.25 . 0.6::
10. ..015' 4.65. +3.94
11 12.7" .0067 7.46 10.6' —3./4
12

13

14

15

16

17

18

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20.

21

22

23

24

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5.3" .095 47.77 (04' 01.17.
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.04—8 (96.6: 50.55
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.022 7!.00 68.90
1.014 (97.82. wan
.0// (90.85 54.7:
.aozas (98.2! lam/5'.

5'18" _ — 6." , _—

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

nut-23: Sheet No. 223
MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE
RunningLonof
Obcavm{ { Date 19 _
”*2 _i‘ T“ W“ ’ “T“ “‘ ___-_._1__,- *“r—"w
Cl ‘ ‘
I 5T£AISHT “TA/<5 0FF
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2 .;.a70 . 7.04 ,. -3.S'é 3 .560 ./$./7 7.07
3 1.2001531? “AH .440 11:.44 .1 7.3:.
4 3/00 1 6.25. «1935‘. .310 mm V0.06
5, ../40 5.7! ' “£87 ‘ .230 “.7: 20.8:
6 .4072 I 4.9:. 29.45] I.Iéo 14.38 g 8.28
7 -042 . 4.76 I —s.8’¢ ' .081 23.4.: 17.3:
8 -038 . 4.84» i “3.76 . .003 £5.22. 17.71
9 .02.: i 6.57 rigs. .040 20.73 .z‘hos
10. ...013 11.54.] V 0.94. .026 18.4; 72.35
1112.7".00¢8./¢.(p7/0.6' 4.07 5.8"..0/51 [0.00 4.1’ . 3.70.
12, ' ,
13_
14
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16
17
18.
19
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21 .. . ‘
22. ‘
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451 i: _L M _L - CELL: - 0.. 1 - -

Sheet I‘m—22L.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE
Runningbonol
Observeu{ { Date 19 _
' I I R I I
I I I I I
I 57%;»er I Tfi-xég/ZF
- I I 40050 IAbpe'p
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2 II.300 :4.33I r407. .I.300 17.33 I323
3.‘ I..:Iao I 6.94 I ‘3.641 I050 20.42. I 14.32.
4 '.180 I4.” I I-sétl‘iI I I70 02.8: I142:
5, .430 I 7.69 I I an?! I './30 21.52 I lso¢a
6 I.067 : 835' I--/.6.S'I I 078 23.08 14...?!
7. I 046 l. $2.1I F4008; 1.0‘l—8 00.83. 15971
8, .0as'I 8.84 r074 Loss I828.18. 00.08..
9. .022 9. :5'I l-/.0s . I. 02.0 28.50. 1:12.404.
10I I201: I 8.44 I I-2./¢ I ‘ I.0/3 ,3J.¢3 3.1.33.
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Sheet N0._afl___

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE
Runningbogof
DWI I Date .19 _
— TI . — I _-—I— WI _ "I” _ _ ”z z

I I I I I

1 I I

II I I I I

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MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE
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HUT-232

MECHANICAL ENGINEERING LABORATORY

MICHIGAN STATE COLLEGE

Sheet No.__¢7_éfl__

 

 

 

 

 

 

 

 

 

 

 

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MICHIGAN STATE COLLEGE
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MICHIGAN STATE COLLEGE
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MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE
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OW{ { Date 19 _
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MICHIGAN STATE COLLEGE

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MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE
RunningLoflol
OWI I Date 19 _
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Sheet No.

MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

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MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE
RunningLonol
Observm{ { Date 19 _
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MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE
Runningbogol
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MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE
RunnIngLogoI
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1 5.2" .. .370 ,. 21.110 5.8’ 15.00 12.7" .350 25.90 12.7’ 11.00
2 4.10 13.7; 12.9: .310 01.30 8.40
3. 2.180 18.90, l 13./0 .250 23.00 10.10
4. .../40 40.00. 14.2.0 .180 22.20. 9.30.
5 7.100 /9.00 13.20 .130 21.50 X160
6 .066: 19.70 13.90. .0317. 27.4.40 11.S0
7 :.038 18.4—0 12.60 .048 20.8’0 7.?0
8 -028 17.8: 12.05 .027 as.90 13.00
9 -019 21.0: 15.2: .013 20.10 13.20
10 ..0/2 16.655 /0.8§, .013 23.10 ,/0,20
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HUT-232 Sheet No.
MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE
Running Log of
Observm{ { Date , l9 _

 

 

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4. -.090 30.00. 24.20. .200 344.50 11.00.
5 . 004151.50 25.50 i./30 33.00 mom
6 1.04:0. £8.50. 22.70, .02: 2.2.30 7.40
7 .0204090 21.10 .050 24.00 11.10
8 .017 30.80 31.00. ..037 26450 11.40
9 .015 3.23.10? 17.30 . .024 25.00. 12.10 .
10. ...00 7527.400. 21.00 . .0144 18.50 15.60.
11. 5.8" .. -— “‘ . 5.8' "‘ .12.?" 0006.15.15 12.7’. 2.7.5
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Sheet No._£Q&__

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MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

RunningLoco!
°wm{ { Date 19 _
I
52-04 .6112- 7741050117.: A
6 14.0050 1400619
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2 .041 51.70. 45.90 .320 24.440 11.50
3. -072. 51.30. 45.50 .250 24.80 11.90 _
44 ..054— $3.70 47.70 .120 25020 11.30
5 .039 51.25 452% .19L0 24.30 11.40
6 .027 48.10 42.30. .091 20.90 3.00
7 .015’ 55.50. 47.80 .052 25.00 12.10
8 ...012 41.1.0. 35-80 .033 25.00 10.70
9 . .007¢ 990.50 35470. .025 24.00 11.10
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HUT-232 Sheet No.
MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE
RunnInlLo‘of
Obua'ven{ { Date 19 _
I ' I '
‘ I
52-0 .4 1022172 0 7741060161:
6 I! 3 ADDED 5140060
JM-JMEAMLQ 1.50.00 .- €2.12._.01V100_£§201..1A011..L-1€§20411._-_
1. s.8",.'.1.20 14.20? s.8' 2.00 V 12.7” .220 01.40120! 3.30
2 11.580 14.50. I . 3.70 .2100 21.20 . 8.50
3. 1.440 14.00 . . 8.50 . I. 210 20.00 . 7.10 ._
4 {”350 15.75. . 9.95 , 1.160 20.60 I 7.70 _
5 .280 12.50 6.70 I E.115‘ 17.10 . 6.20
5. .m/So 10.00. 10.20 1 0074' 20.30 7.40
_ 7 I.087 16.10. 10.30 i 1.043 2.0.40 . 7.5'0
8 I'M?" 15.40I 9.40 I .030 20.00 x 7.10 .
9 i..042. 20.0.4”. 10.85, 5.020 20.00 : 7.10
10. .5026 15.40I . 2.00 . U013 23.10 10.20
11. 5.?" (.015 7.70 5.5” 1.70 . 12.7"i -- . _— 123’, -
12 I I .
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22 I
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24. ,1
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nut-232 Sheet I‘m—LL;

MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

RunningLo‘of
om{ { Date 19 _
I
I I .
‘L . 511416117 771050.67: I
6! ' 400"" 14005.0
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1‘15.8".,.‘2‘00 13.00. 5.8' 7.20 12.7" .320 2.3.1012.9’10.20
2. -260 15.00 9.20 .230 23.00 10.10
3.‘ .. ..Iio 18.30. . 12.50.. . .170 . 7.0: 05.35:-
4. 140 14.30 8&0 .125 24.00 .11.10 .
5: @086 10.30 10.50 .021 22.20 3.30.
6. 3.051 17.60 11.80 .040 23.90 11.00,
7I :.035’ 20.00 14.20 1.03; 21.90 . 9.00
8.] ..028 14:30 6.50 :.023 21.70 3.30 .
9. ”01513.30. _‘ 7.50 . .013 23.00 10.10
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Sheet rim—SEA—

MECHANICAL ENGINEERING LABORATORY

MICHIGAN STATE COLLEGE

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

RunningLogol
om{ { Date 19—
}
£2"ng TAKEoF; '

6 ‘ ADDED 1400517

mag/100 502.4. Acr. l..- EHLQ.AP/100 fig..4.w&cr..l—..§Q¢Q.L_ __
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2. .170 20.00 1+.80 .2¢0 00.80. 7.90
3. ..12$.a0.80 15.00 ..17: 24.00. 11.10
4 ...08’8’ 03.90 18.10 ..1.-30 10.15’ 3.2S'
5 .057 22.80 17.00 .084 51.2.40 9.70
6. .,.034 33.50. 17.70 .0548 17.00 14.10
7! .016. 19.20 13.40 .03: 22.80 7.70
8: .016 125.00. 19.20 .028 17.85' 4175'
9.; 7.01.7. 16.70. 10.90 .014- 28.60 15270
10; 51".. -' - 5.2' -- 12.1" .0003 15.35123’4 0.9:
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Remarks:

Sheet I‘m—fli—

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE
RunningLogof
0W{ { Date , 19 _
I I I I I I
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:~ Srgmgnr , 7741013 01::
6 ‘ I ADDED I 140060
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1. 5.8" .../40 09.30: 5.8' 03.50 V 12.7”f .350 2310123510001
2. .100 30.00; 3040, C230 ‘ 25.90 I I12.30,
3- .07¢- 39.20.. 133.40 1.180 0.350 I I12.00.
4. ...054 I 35.30.! 0.9.40. 1.130 04100 31/.70.
5. -035 34.20,? 018.40 3.087 34.20: I11.30
6' ...01/ ;33.30I InZS‘oI I.0$0 00.00 I13.10I
7. f.01§ , 40.005 IJ‘ARO' 2.0370430 71.4-0.
8 501/ .3b.¢/0I :50.60I I.01$’20.0o I 7J0
9 ...0065'1 30.80! I 12.5.00 ..010. 0.5.00. I12.10 ,.
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0.1.7.232 Sheet No. 5-54
MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE
RunningLogof
OW{ { Date 19 _
‘ I
I
Jr1eA1§HT anoFF
6 ,. 14000'0 ADDED
M3 -D .50.L.A<:LLL£9..‘L 52.0. 48/100 50.0144710501. 4%
1. 5.9" . 1.000 14:30 518'. 8.70 12.7"..250 22.40 [2.7, . 7.70 I
2 . .7701§.30 9.50 ..180 23.30 10.¢0.
3 I .5'80.1+.60_. .880 . ..130 01.50 I 8.60 ,.
4. i .400.1£.S'0. 10.70 . ..077 23.20. . 9:30.
5 .270 10.50. 10.5‘0 . .006 22.70 I 7.80
5 ..150 15.30 7.50 -030. 22.20 9.30 .
7 .120 15.00 9.20 .018 21.40 8.50.
8 2.075 :16.00 10. 20 .018 22.20 , 9.30,
9 04116.6: 10.65. .. 01/ 27.70 14.501
10‘ 5.8" ”07.7) 3.70. {.8' +1.10. 12.7", 7" ‘" 12.7’, ""
11. I
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13
14
15
16
17
18
19. .
20 ‘
21 ..I
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23 I
24 I: ,
$00114; ._ -- _‘It— __ ; ,—: — _— 71 I
Remarks:

Sheet No._£.é_&__

 

 

 

 

 

 

 

 

 

 

 

MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

Running Lon of
Observm{ { Date 19 _.

I . 7 7 I -

I
I I
gage/5117' 7741:5001:
140050 140060

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1. 5.8"} .550 10:0. 5.8'. %70 12.7". .250 24.40 12.7’.11.S'0 I

2' II .460 11.30 .550 . .210 2.5.80 10.70

3'; II-570- 7.50.. . 5.70 , .. 15‘0 24.70 11.80

4. I I340 10.80 .5300 I .11: 10.80. 7.70

5I ‘ I.160 70.60 4.80 w .073 33.30 704-0

6. .I.07¢ 72.7: 6.95. .0#« 22.70 7:0 I

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8I {.043 I 11.60. 5.80 ‘ .000 15.00 12.10 .

9I II.02¢I12.$’0 4.70 ’ .012... 25300. 112.10 .
10; 5.8" I.I.011 I18.20. 5.8’ 12.40.; 12.7" ,.0058 17.20.12.7'! 54.7.0
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nun-232 Sheet No-
MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE
RunningLocd
°~m{ I C
Date . 19 _
II I I I F
, . I
I. I I
I fremgfir 711050.61:
5 II 40050 4-0050
£050.12 WAC-TL EmH—LMMMQfiLQ 5.00.4-
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2I .320 ;10.60I . 4.80 _ .. 20.0 08.00 12.10.
3I I I.180 7.30 ; 3.50 I. .170 02.30- . 7.40...
4I I II. 170 11.7{I ,' 5.95 I 1.120 23.50. 210.410 I
5I I . ’10./2-70I I 60.90 I I.07’7 220/0 I ?020
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nut-23: Sheet No.
MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE
RunnlluLogof
DWI I Date 19 _
I
I I
I- 57£A1§11T 7741:5051: I
I 140050 I1400.150
__QLAMMMW $4.35; 1.
1I5.8"I.280 13.90 5.8’ 2.10 12.7" .280 25140 12.7’I12.50
2II -230 15.7: 9.95 .230 24.30 I11.4-0
3.‘I ..14-0 77.15 11.35,, I . 170 .04. 70. 111.80 ,_
4II .,.100 17.00 73.20 I. 150 23.80 I10.70
5 .00:21.Sa 15:70 .08: 24.70 41.80
6 .039 17.9: 12./5'. .MLZ 22.70 10.00
7 I.0:.A' 25200 17.20 .03: 25.70. I12.80
8 .020 30.00 14.20 -023 26.10 I13.20
9I .012. ..25100 17.20 .01 3 23.10, I10.;20
0 5.8" .: '"‘ "" ' 518’ “" 12.7".0067 27.7012.7’I17.00
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Sheet rim—1m.—

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE
Runninglmd
OW{ { Date 19 _
i I _‘ “ ":-_ — _ ‘"— ,3 ' A w _7 —_ -“—
‘ ‘ I
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7 57114161147" TA/ééoFF L
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2. I .340 3'81; 72.73; 30:14.71 * 2 3.5.7..
3.. 2.21.3 . 9.:2 , .-3.2-2.. “.241 17.84 I 4.44 I
41 1‘ ./77 9.14— 1. [ 2-2.“ .. 180 17.2.2 I 4.0L
5 .1./45 ‘ 7.67 w ‘64.!“ .127 17.32. F 4.12:
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9! 3.02.55 H.751 '-o.a¢. @0226 17.70 i 4.50
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11; 10" 300624. 15.63,; //J'. 3.33' 10” ..aas'7 14.75 /9.2’. 3.7:: _
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nun-232 Sheet NO-
MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE
RunningLogof
OW{ { Date 19 _
l , I
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A 571919115112" TAchFF
5! , 140050 140050
$2.-.-AM00750.L.A07.L-EQ04. mmaa.0. A0774, 5&0.
If. 10” ...340 . 7.12 11.8’ €7.68 ID" .460 1:35" 13.3’. 2.1:
21 -290. 7.02,. .—3.18 .360 14.59 3.17 I
3I 1.231. 9.051 ,-:2.7Si .280 15.71. T 2.51 _
4- ..171 . 8.17 +3.61. .710 18./0 , 4.70
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81 .03: 8.57! ‘123 .04—5 16.28 Iios’ .
9_l . ...02412..S‘0 ‘ 0-70 .0735' 21.05 i 7.85 I
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Remarks:

(0714

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

......m Sheet No.
MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE
Runninglmd
OW”{ I Date 19 _
I I I ‘ I
I
STMIIT' figgoffi I
W5 I 5 1. '43:? __50. 001,040. 00.0. 1:07.022”?
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2. ....2¢0 : 7.53. -2.22 .420 17.86 I 4.04. _
3- ....m . 7.52.1 +2.23. T.530 17.27 I 41.17 ..
4, ...14—0 . 2.37. 23.25: ..2¢0 17.92. i 4.71
5. .100 9.00 , ;-a.80‘ @173 10.8: ‘ 3.65"
6 .,.067 I11.9%. O./‘/-' .116 18.10 g 4.90
7 .1433: 10.79? ‘ 1.173 '.068 17.12. I 59:. .
8 .028 10.71: "I.o‘l I -046 21.74 I 7.54
9. 402057. 7.75 I .--?-o‘/- ..032 15.63 2.4-3
10- -0113 1.547. .-:?.33. ..017:1s.38 . 2.17 ..
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13‘
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21. II > I I
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M LIT-232

70A

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Sheet No.
MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE
RunningLo'of
0W{ { Date . 19 _
I T WM”
JrgAfl-r 'THKELOFF
.5 140000 40050
_WQLWLAEQL.Q_ L _é-QLQiAfi/ma 50.- 4-- IiéLé-Lfihlb
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2 .../4'8 [41/7. . 2039 3520 .310?0 8070
3- .I.I/é: -1.1.07- . 0.27.. .440 42.50.. I. 9.30 ..
4 -088 12.50 0.70 . .330 22.7.5- ' 9.53 .
5 '.000 15.00 3.20 .254 20.9% i 7.74
6 ;. 041 .1¢.z.7. . 2.49 . . .157 23.84 [10.64
7 -023 17.39 5.59 .08¢ 04.17 112.79
8 “a!“ 15.96 4.16 .06: 13.08 I 9.88
9. -0132. 3.0.3. -8.77 .04-75 15.88 12.68
10 I ...0074 3.1! , .-.-3.67 -0244. 24.37 I11./9 ,
11 Io" .; —- -—' 11.3’, -- 10" -0107 10.09 15.2’ I 5.47
12‘ * 4
13
14‘
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16
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18. I.’
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21 1.:
22 7'.
23 3
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TA : _

 

um-m Sheet No.
MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE
RunningLosol
Observm{ { Date 19 _
57-001 GHT’ 7745005;

0' A9959 140050

_zfiLAMWfiLzLéa .1.._______€0..D..01’/100 . 50.1.. 1101-10 -5400 ..-__ __
1. 10" -400 - 2.71 11.8’ 37.87 10” -318 10.78 13.2’ 3.78
2 I ..381 . 7.77 -I.85 .207 10.50. . 3.10
3 .-..300 10.00. -‘l.80 . .210 10.17. 2.77
4. .225 7.78 -2.02.. -158 10.44 I 3.26
5 .15'7 11.916 -o.3¢ .114 10.07 .-7.¢7
5 ..10/ 11.28 0.0? -074 10.22 3.0:.
7 -005 11.11 .-0.47 . .044 11.18 . 4.73
8 ,.07¢13.L¢ 1.84- .052. 18.7: . :..?! ,
9. ...02814627 I . 2.7M .03: 13.074 0.50%
10. I -0173. 11.56 -0.24. .013714460 : 1J0
11I 10" .0068’19‘JI 113' 2.71 10" .006 13.33 13.21. 0.13
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Remarks:

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HLIT-232 Shut N0. 734
MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE
Runningbocof
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MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE
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MLITo232

Sheet No. 74A

MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

 

 

 

 

 

 

 

 

 

 

 

 

 

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MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE
Running Log 0!
0W{ { Date 19 _
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MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE
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MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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NUT-232

MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

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MECHANICAL ENGINEERING LABORATORY

MICHIGAN STATE COLLEGE

Running Log of

 

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Sheet No.
MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE
RunningLogo!
Oboavm{ { Date 19 _
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Remarks:

nut-232 Sheet No- X5”

MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Runningbogol
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Remarks:

"UT-m Sheet No. {3 "" 74‘

MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

 

 

 

 

 

 

 

 

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Remarks:

9E

HUT-232

Sheet No.

MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

Rmniumdmr 27/00: - Mi”): X” 3070‘ 5776. 0‘ 7:0.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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HUT-232 Sheet No-
MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE
RunningLogof
Observen{ { Date .19—
J’ru 19.17- 7'74.<on—'1=
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wv-m Sheet No.
MECHANICAL ENGINEERING LABORATORY
_ MICHIGAN STATE COLLEGE
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1.1.1.232 Sheet No.
MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

RunningLogol

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MECHANICAL ENGINEERING LABORATORY

MICHIGAN STATE COLLEGE

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Sbeet No.
MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE
Runnlnglmd
0m” I Date 19 _
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MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

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Remarks:

 

“LIT-232

Sheet No- ”A

MECHANICAL ENGINEERING LABORATORY

MICHIGAN STATE COLLEGE

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

 

 

 

 

 

 

 

 

 

 

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MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE
Rummaimmr Z7205 —- /03’:"x 8" 507-11 5m; : 7m.
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MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE
Runnluglmol
0m I Date 19 _
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“LIT-232 SM No. [a]

MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

RunnIngLoaoIMHT TYE" lpjl'”x X” 50711 57%. l 770.

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MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE
Runnlnglmof
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‘ MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE
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NUT-232 Sheet NO-
MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE
RunnlnaLocof
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HUT-232 Sheet No. 1 0i

MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

RunningLogol 57' " 0“” ” S .0
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uumaz Sheet No.
MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE
Runninglmof
OW{ { Date , 19 _
7 I I F I j“ T :— ‘T “I”
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MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

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“LIT-232

Sheet No.

MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

III

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......m Sheet No.
MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE
RunningLogof
OW{ { Date 19 _
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"LIT-232

MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

Running Lou 01.5251105107- 71/1’5 "' / 0 "l' I, 11

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NUT-232 Sheet No.
MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE
RunningLogo!
Observers{ { Date 19 _
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Sheet No.

“LIT-232

MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

107

 

 

 

 

 

 

 

 

 

 

 

 

 

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MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE
Runnlnclmol A
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“LIT-232

Sheet No-

MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

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MICHIGAN STATE COLLEGE
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“LIT-232

MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

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MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE
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Sheet No. +1

MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

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“LIT-232

Sheet No.

MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

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MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

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“LIT-232

Sheet No.

MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

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1111.17.23: Sheet No. //3

MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

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Hut-232 Sheet No.
MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE
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MLIY- 232

MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

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MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

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Remarks:

HLIY-232 SM N0. II‘

MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

n....um0_&001100r 7717.5 -— 10:3 9” 007-11 57—2. 0 130.

 

 

 

 

 

 

 

 

 

0£151c€§ ,' 53g, 51.0;552 t 85’; ”x Q” 7'70.
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MLIT.232 . Sheet No. !l 7

MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

RunningLogolWT 73/131? - 107’: ”x 9” 307-11 .5714 7:0.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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Remarks:

“LIT-232

MECHANICAL ENGINEERING LABORATORY

MICHIGAN STATE COLLEGE

Runnlude-r- Tyre: 101'”: X" 30:11 5212.1 770.
0W. 15132. at. eggeg J ’7”); 44;”770.

Sheet No. j/X

 

 

 

 

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”LIT-232

117

 

Sheet No.
MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE
0...... Lou «MHZ TYPE: 3km L g ” xi” 7: 0.

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HUT-232 Sheet No. L2_0

MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

12111111111quer 77”?" 3'1?” fire L If”): 3” 7’0.
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Remarks: CHECK Fat £é4KA‘g.
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“LIT-232

MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

910dele

amnimwamr TYPE” 3"LX" 51". fl IX’IKJ” 770.
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HUT-232 - Sheet N0. [32

MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

RunnIng Log of ’I I, /f ”X K O, 7.. 0.

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Remarks:

ULlT-ZJZ

MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

3’06 L” 5724.}
l4'x 4" 774.

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“LIT-.232 Sh”. No. (g g

MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

1205510;de - 3’01!” 03%
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Remarks:

“LIT-232

Running Log «Mr Tm ..

MECHANICAL ENGINEERING LABORATORY

MICHIGAN

STATE COLLEGE

Sheet No. /25'

3”): 3'" sné’. g 47”): i” 710.

MAJ-1:”): 1i” 5m. 4 770. 51.041550

 

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__.——
—————

 

HUT-232 Sheet No. lzé

MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

numb...“ 57720101" 77195 - 3”x L’s-12- 1 17”.: (”112,
Ms .' 624‘“ I?” 5rd. at 770. 81.05.4550

 

 

 

 

 

 

 

I Date 141/54 51 .1952

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Remarks:

“LIT-232 Sheet NO. ,2 7

MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

Runningmdw "' :3”; I" 57324 1.?”1L?” T.0.

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Date Aug, ¢ .19 £2

 

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Remarks:

111117.232 Sheet No, /2X

MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

Rmmmmdde Txnz - 3". 8" W
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Remarks:

 

 

MLIT-232

SheetNo- JQKA

MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

Running Log of

 

 

 

 

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5'77: A lé/{T‘

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NUT-232 Sheet No- /2 q

MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

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NUT-232 Sheet No.
MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE
RunningLogof
om{ I Date 19 _
I
57-14101” 7741:50170' L
6 I 140050 A0050
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nut-232 Sheet No. IQ

MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

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Remarks:

“LIT-232

SheetNo. [3&4

MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

 

 

 

 

 

 

 

 

 

 

 

 

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Sheet No-

MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

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HUT-232 Sheet No.
MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE
Runnincbonol
0W{ I Date 19 _
5711416117" 7701:5on
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Sheet No.

MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

 

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Remarks:

“LIT-232

Sheet MM

MECHANICAL ENGINEERING LABORATORY

MICHIGAN STATE COLLEGE

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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HUT-232

MECHANICAL ENGINEERING LABORATORY

MICHIGAN STATE COLLEGE

Sheet No.

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HUT-232 Sheet No.
MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE
Runnlngboflol
omm{ { Date 19 _
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Sheet No-

HLIT-232

MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

Rummamur Tyne" 5”x 6’” 51-12. L125; 3'” 770.
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Remarks:

MLIY-ZJI

Sheet I‘m—Mg—

MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

 

Runnlng Log of

 

 

......{ {

 

 

 

 

 

 

 

 

 

 

 

 

Date .19—
Sremsm' 721550;;

.5 49050 A0020
2 £0.12 411100 £Q.L.LAc77L. 50.4. 50.0. 419/120 5.0.1.. 40774.43321
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7 .031 29.3.5’ 25.00 .049 20.911 7.75
8 .025 53.48 27.13 .030. 25.00 1.1.51
9 .0143 31.47 25.12. .0228 22.37 . 1.19
10 -0033 20.4! 14.13 .0137 10.95 -1..s'3
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Remarks:

 

/3$"

nun-232 Sheet No-

 

MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

Rumin‘md 57-1 ”/6197“ TYPE _ E’IXL’LmJ /8”K1” 7:1;

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0.01.5505; 02.”; 14;.” 25g. 1 15%.”; sé”-r:0.

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Remarks:

@509

 

 

 

 

 

 

 

 

 

 

 

“LIT-232 Sheet No-
MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE
Running Log of
O { I Date . 19 _
__.—:":‘::::—_—:_::z—:~—: — - _—f :-—:+——: —r——— -~—-—.— fi—C—Tt‘ " r ‘3 — ‘1.-
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9 .0178 20.40
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MLlT-232

Running Log .._.Szazmgmr TYPE
05151ceg .' é‘i'. " x I: '

Sheet No.__LiL_

MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

- 3‘18" 57-10. g! 18”1<8”7':0.
srfi. i 1S”x 5”]:0.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

WM { Date ”141/6 7 19 £0
TIME IPg-P P4. 1:;— p‘, 775W“. 33“ r— 69¢ 05. 52‘
.; 11.0 0.3.

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11, 2:5’8- 003-000.91.000 ..005' . 70.0; 8530.29.28.15: 200 . 21.0 .. 102

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9:95;: 90230008518: 23.0

Remarks:

 

“LIT-232

Sheet I‘m—Lai—

MECHANICAL ENGINEERING LABORATORY

MICHIGAN STATE COLLEGE

 

 

 

 

 

 

 

 

 

 

 

 

 

RunningLocof
om{ I Date . 19 _

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Remarks:

 

 

 

 

 

Sheet No. lag

“LIT-232

MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

 

 

 

 

 

 

 

 

 

 

 

 

 

 

awn... Log 0.920.110 1.1-1— Tfi‘i‘ 21m ” 57%. LIL’LE’ T00.
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2; 3:00 .; 3.17 . #533090 .720 1.79 1399 222 1190
3: 3:08.231 £501,499 .530. 1.52 1194 /90 1020
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137A

 

 

 

 

 

 

 

 

 

 

 

 

 

nun-232 Sheet No.
MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE
RunningLocol
Observen{ { Date 19 _
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Remarks:

 

 

 

 

"LIT-232

RunnlmmdflaLE/LT IYPE " 5’”X

MECHANICAL ENGINEERING LABORATORY

MICHIGAN STATE COLLEGE

SheetNo. I53

 

 

 

 

 

 

I g” 57.“ at” I: z" z 2
m: 071' 'x 12L" 5:; g 16‘2"”10 0%” 770.
Date—iii” .1950

 

 

 

 

 

 

 

 

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7; 9:20 . .510 .02: .031 .014 .714 501 2 35.7 :40

8. 9.’2:I'.395' .019 .023 .011 .02? 493 30.9 480

9: 9:24 .204 .013 .01: .007 .514 404 25.0 33:

10: 9:27 .1100 .007 .003 .004 .374 294 13.3 094

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NUT-232 Sheet No-
MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE
Running Log of
O { I Date 19 _

 

Jfiqugfir'

.074
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I

MLIT-232

Running Log of

137

Sheet No-

MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

13”x [’10.
11’11 ” 7:0.

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Remarks:

 

 

OMTIM I n..._&11_&._i.19 £0
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4I 9:40 . 2.35 .141 1.170 .100 1.533 1205. 33. 1130
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Wmmggm 70.9 . 001 0-00.43.00.10 0001;4513

“LIT-232 Sheet Nth—m—

MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Runninglmol
0m{ I Date , 19 _
I I
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1 A
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Remarks:

14o

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

0.17.232 Sheet No.
MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE
RunalngLongHT ’IYPE- ‘— 3”x 3'” 57.2. ¢ 13” 003”f0
W? x 1'51? ..1 15:.” x 5"”J20.
I Date fire: 7 .19 :10.
77M! 5-K, P" 2‘ ’1 fl 3”" V5}; ‘94 0: 620
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3. 10:17.. 3.13 ..200 ..295 I .205 . 1.77 1371 . 109 .1290
4. 10:21.. 2.35, .195 ,.220. .153 . . 1.5331205 , 945-1120
5.10224. 1.03 ..139 ..155', .109 . 1297,1019 . 79.5.. 945
6.101700.I 1.00 ,.083 1.099.009 . 103 . 307 , 03.2. 755'
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Remarks:

1 4014

 

 

 

 

 

 

 

 

 

NUT-232 Sheet No.
MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE
Running Log of
Ohwrvm{ {
Date 19 _
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"mm Sheet No.
MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE
RundqudfiWdujg. J lflx J” 7'70.
Dag—mg: .' 61'“ 17.?” 571:. 4‘45”): 5" r41.
Ohurvcn{ { Date ”fig 9 .'19 __539
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122.013 .062 90.9 . 4§$..0047..0S47. 455.5.015 ..055'..0073..007 -.600
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Remarks:

“LIT-232

MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

Sheet No. I‘ll/4

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Runninglmd
0m{ { Date ,19___
. ‘T fl __..___--_ F _ -
S .3144 1670’ 72710500.“: $
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2 .207 27.17 10.74. .305 17.07 s 7.17
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Remarks:

 

“LIT-232

142

Sheet No.

MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

 

 

 

 

 

 

 

 

 

 

 

 

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3’11:43 2.38 . .020 ..002 .587 1.842 1212 ' 181 1075
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5 11:48 1.07 ;.278 :.270 , .200 1.0.-J4 812 10! 720
6 111:0 51.04.142.137 .133 .748 583 75 5'17
7 11:33 .406 '10z..098 .09! .657 5'01 43.2. 438
8 111:3 043-001 {.059 .05"! .473 387 x 49.2 340
9 11:58 .145.037 '.035‘ .034 .381 277 ’ 38.0 20:
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08:: - l A ’ ___——

 

Remarks:

Sheet Na. M344

MLlT-232

MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

RunningLoaof
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Remarks:

MLIT-232 Sheet No, /43

MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

 

 

 

 

 

 

 

 

 

Rummmdmfi‘r T1025 - 3”x2” 5m. 3! 10”;<8”j:0.
WM”770

O {W { Date—ML 19 :0
— " 1 L1 '72 7:3“— ‘2 — 3‘ :‘*——_ _-

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Remarks:

I

 

NUT-232 Shut No. L¢3A

MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

RunningLocol
OW{ { Date . l9 __
1 I ”’4 7 _.T_.____
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Remarks:

 

144

“LIT-232

Sheet No.

MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

ammmdmfir 7’1; 3'"; 1L” :re. .1! 18”.: $7110

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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W91 K-3 ngg-M

 

Remarks:

"LIT-232

MECHANICAL ENGINEERING LABORATORY

MICHIGAN STATE COLLEGE

Sheet No. l 4514

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

RunningLogof
Obavm{ Date 19 _
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4! 0375 2427i . 77.92. ..197 18.78 ' 6.30

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Remarks:

 

 

14!

 

 

nut-232 Sheet NO-
MECHANICAL ENGINEERING LABORATORY
0111211101119 STATE COLLEGE
am... ....wr TYPé 7 3”x 8’9776’. 4f IL'LZI'I. 0.-.
WM 77 00

 

 

 

 

 

 

 

Date 146- ll. 19 fl

 

 

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211100 . 4.11 .366 . .429 . .184 2.03 1595. 90.0 1510
3 11:04 3.19 .281 :.321. .217 1.716 1403 78.0 1330
4 11108-235540: .238 .158 . 1.533 1205',» 66.4 1135
5 11:10 1.62 .140 :.162. .109 1.27.2 1000 54.2 94.8
6 11:22.. 1.06 -092 '.105' .070 1.0.30 809 43.2. 760
7 11:25' .555 .048 ‘.0f5',.036 .745 585 30.9 550
8 11:23 .374..034 '.038 .025 .027 473 25.5 400
9 11:31 .240 .021 -024 .015 .490 385’ 20.0 358
10 11:35 .150 .012 ..014 .009 .387 304 .1531 280
11 111.37 .065'..00.5’.006 .004 64.0 78.0 29.26 .255 200 ' 9.7 188
12 1
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Remarks:

 

“LIT-232 Sheet "0..—[$.4—

MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

Running Log of 1

 

 

 

 

 

 

 

 

 

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IL 5‘12419117- 775-1550;; ;

o. ' 140090 (“40050
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5 -054 05.881 59.53 .139 17.71' ‘ 0.23
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7 -0126 61.90’ 525.55 .051 19.61' 5 7.13
8 w.0091 ! 71.43“ 05.0: A ..036 17.44 ; 0.90
9 .006 ’ $7.67l 45.32 . .024 . 19.58. . 7.10
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Sheet No- / 4‘

“LIT-232

MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

...... .1.. 04220131”- Wtwflflflk 8" 7'. 0.
W8 1” 3:71. 1‘ 1s”): 5” 7'10.

 

 

 

 

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Remarks:

MLIT-ZJZ

MECHANICAL ENGINEERING LABORATORY

MICHIGAN STATE COLLEGE

Sheet him—fid—

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

                 

Remarks:

 

 

 

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OW{ { Date 19 _
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02117.23: Sheet No- [#7

MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

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Remarks:

147A

”LIT-232

Sheet No.

MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

RunningLocof

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Date 19 _
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Remarks:

 

 

 

MLIT~232 Sheet No, /48

MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

RunningLo‘dMIlT TYPE “IE-”X Z" :72. 4 3”X [”170.

 

 

 

 

 

 

 

 

 

 

 

 

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Remarks: CHECK Fad LEAKAGE:
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MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

RunningLoaolMHT TYPE - Ifl’XB” ST‘KWMK'WTLQ.

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MLIY~232 Sheet NIL—Li—O

MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

 

 

 

 

 

 

 

 

 

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Remarks:

”LIT-232

MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

SheetNo. 15']

 

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Sheet him—LS-L

“LIT-232

MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

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“LIT-232

Sheet I‘m—L.

MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

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MLIY-232

MECHANICAL ENGINEERING LABORATORY

MICHIGAN STATE COLLEGE

Sheet No- /5‘¢

Runmumdmfir TYPE "' [L'lx g” ”(LL3”&J”J;Z_

 

 

 

 

 

 

 

 

 

 

 

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Remarks:

I

HUT-232 Sheet NO. ’55.

MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

 

 

 

 

 

 

 

 

 

 

 

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MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

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“”233 Sheet No.
MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE
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Remarks:

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nun-232 Sheet No.
MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE
Running Log 0!
0 I { Date . 19 _
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NLIT-232

Sheet Na-

MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

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MECHANICAL ENGINEERING LABORATORY
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MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

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Remarks:

 

nut-232 Sheet No. [MA

MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE
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MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

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Sheet Ila—fli—

MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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MLIT-232

Sheet No. /‘ ¢

MECHANICAL ENGINEERING LABORATORY

MICHIGAN STATE COLLEGE

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Remarks:

 

nut-232 Sheet No. (Q g &

MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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MICHIGAN STATE COLLEGE
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MECHANICAL ENGINEERING LABORATORY

MICHIGAN STATE COLLEGE

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MECHANICAL ENGINEERING LABORATORY
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HUT-232

Sheet No.__éfl__/ 6

MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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nunzaz Sheet No. /éz

MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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“LIT-232

MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

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NLIT-232

Sheet No.

MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

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"LIT-232

Sheet NmML

MECHANICAL ENGINEERING LABORATORY

MICHIGAN STATE COLLEGE

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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MLlT-ZJZ Sheet No-
MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE
Rmnlumdmr TYPE "" /Z”X 8” 5 ” 0
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Remarks:

Hut-232 Sheet I‘m—m—

MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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OWQ'I ' I Date .19—

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MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE
RunningLongb‘T— TYPE‘ .18”): 8321. g! 3”x 8” 770.
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Remarks:

SbectNo. [704

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE
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Remarks:

nun-232 Shed No. J7/

MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

RundquW - [ZIIXX’I 57-4' m
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NLlT-ZJZ

Sheet No. / 7/A

MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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HUT-232 Shut N0. / 72

MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

Rundumdmflr TYPE - J3”! X" W5 ”X 11
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77m:— 5—13, Z1 75" P6 M302. V’s-Pa. 694 C9: C96
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2 2:32 4.13 .165 .123 ..215 2.0321577 1555 66.5
3 2:37 3.12 .12/ .07.: .160 1.766 1378’ 1345.570
4 2:40 2.35 . .070 .070 .120 . 1.533 1205 1175. 47.0
5 2:42 1.66 .064 .046 .014 1.287 1013 775' 41.0
6 2:45 1.06 .041 .03/ .053 1.030 807.4 725 32.5
72:4? 575.024 .017 .030 .7714 606.2 584 24.4
82:51 .386 .015 .01/ .019 .6213 42361472 1%:
9 2:54.255 .010 .007 .013 _ .5050 376.: 377 15.!
10 2:56 .145 .0055.004 .007 .380! 277.2. 25’? . 11.4

11 2:58 .056 .002. .001 .003 77.0 82.0 27.05 .2367 156.0?147 7.5

 

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2:16.129 .274 4.10 1531.5 .146 .269 65.5 .010 .225 .025,.069 .257
3'}? .07: .217 4.77 1331.5 .111 .203 50.5 .007 .167 .016 .052 .254
4'1'8 .075 .163 4.00 1156.! .013 .153 48.2. .005 .125 . .010 1.733 .250
:19 .057. .116 4.14 172.1 .007 .107 40.7 -004 -011 .107 L128 .253
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721.019 -043 4.0/ 511.9 .021 .03? 24.3 .0013 .0313 .005 .0117 .251
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Remarks:

MLIT-232

Sheet No. I 72A

MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

RunnIngLo‘of
Observan{ { Date , 19 __
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3 .262I (.../I I ~4.¢.( .0369 1444944.: I138.05,
4. .177 5:03 I .-$.:3 .0275 153.12. I131. 79 .1
5, ~ .145’I, 6.2! I ~43! .0203 137.93 I/a/1s4
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HUT-232

/73

Sheet No.

MECHANICAL ENGINEERING LABORATORY

MICHIGAN STATE COLLEGE

RumlmmaW‘
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8 3:39 .390 .020 ..010 .024 .024: 490.7 407 21.7
9 3:41 040.013 :.010 .015“ .499 387.0 271 17.0
10 3:43 .130 .007 .00: .00! .3606 283.6420: 12.4
11 3:4: .051 .003 .002 .004 77.0 72.0 29.05.2307 186.0170 7.7
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Remarks:

Sheet No. /7 3A

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE
RunningLogof
om{ { Date 19 _
., ~ I
5 7x14 161+IT' 73:50:15 I
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6 .077 I 6J9 I -4.37 .017 1/7.6SI III/.26
7 .049 I .9./L I -2.40 .00?! 117.32. I112.93
8 ..037 I541 I -5.1: .0007 102.77 I90.00
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MECHANICAL ENGINEERING LABORATORY

MICHIGAN STATE COLLEGE

amumumr 7169:; - It”): 0:" :7". f 3”); E’_’z:0.
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Remarks:

HUT-232 Sheet No, l 7¥A

MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

RunningLoaol
OWI I Date 19—
I
I
I
STZAIGH-T 77‘5“?“ +
6 I ””059 ADDED
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4 .19: 7.07 ~2.77 .000 91.30 04.91
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9 .0231 8.60 , -1.90 . .0056. 7512/ $00.82
10 .0129 7.7: -:z.:1. _ — — I —
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13
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Remarks:

Sheet No. /75 I

MLlT-232

MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

RunningLoaof {TEAjfillT 7..-“£7- IZQK” 57“. i 3'IKZ’I770,

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Remarks:

HLIT-ZJZ

Sheet No. /7_S_'A

MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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Sheet No.

MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

 

 

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Sheet No- [’7QA

MLlT-232

MECHANICAL ENGINEERING LABORATORY
MICHIGAN STATE COLLEGE

 

 

 

 

 

 

 

 

 

 

 

 

 

Remarks:

 

 

 

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