A WATER
RESOURCES TECHNICAL
PUBLICATION
ENGINEERING MONOGRAPH
No.1 4
Beggs Deformeter Stress Analysis of Single-Barrel Conduits UNITED STATES DEPARTMENT OF THE INTERIOR BUREAU OF RECLAMATION
Mission
of the Bureau
of Reclamation
The Bureau of Reclamation of the U.S. Department responsible for the development and conservation water resources in the Western United States.
of the Interior is of the Nation’s
The Bureau’s original purpose “*to provide for the reclamation of arid and semiarid lands in the West” today covers a wide range of interrelated functions. These include providing municipaland industrial water supplies; hydroelectric power generation; irrigation water for agriculture; water quality improvement; flood control; river navigation; river regulation and control; fish and wildlife enhancement; outdoor recreation; and research on water-related design, construe tion, materials, atmospheric management, and wind and solar power. Bureau programs most frequently are the result of close cooperation with the U.S. Congress, other Federal agencies, States, local governmen ts, academic institutions, water-user organizations, and other concerned groups.
A WATER
RESOURCES
Engineering
Monograph
TECHNICAL
No.
PUBLICATION
14
Beaus Deformeter Stress Analvsis vu
I
of Single-Barrel Conduits By H. B. Phillips and I. E. Allen Experimental Design Analysis Section, Technical Engineering Analysis Branch, Office of Chief Engineer, Denver, Colorado
United
States
Department
OF the Interior
BUREAU OF RECLAMATION
As the Nation’s principal conservation agency, the Department of the Interior has responsibility for most of our nationally owned public lands and natural resources. This includes fostering the wisest use of our land and water resources, protecting our fish and wildlife, preserving the environmental and cultural values of our national parks and historical places, and providing for the enjoyment of life through outdoor recreation. The Department assesses our energy and mineral resources and works to assure that their development is in the best interests of all our people. The Department also has a major responsibility for American Indian reservation communities and for people who live in Island Territories under U.S. Administration.
ENGINEERING MONOGRAPHS are prepared and used by the technical staff of the Bureau of Reclamation. In the interest of dissemination of research experience and knowledge, they a,re made available to other interested technical circles in Government and private agencies and to the general public by sale through the Superintendent of Documents, Government Printing Office, Washington, D.C.
First Printing: 1952 First Revised Edition: 1965 Second Revised Edition: 1968 Reprinted: 1986
U.S. GOVERNMENT WASHINGTON
PRINTING
OFFICE
: 1968
For saleby the Superintendentof Documents, U.S. Government Printing Office, Washington, D.C. 20402, or the Bureauof Reclamation,Attention 822A, DenverFederalCenter, Denver, Colorado 80225.
CONTENTS
PW
INTRODUCTION.
.............................................
APPLICATION................................................ DETERMINATION APPENDIX:
OF NORMAL
1 3
STRESS DISTRIBUTION.
THE BEGGS DEFORMETER
..
5
.. ..................
57
FIGURES No.
1. Dimensions of conduits and location of points studied. Shapes A,
2. 3. 4.
5. 6.
7. 8. 9. 10. 11.
12. 13.
14. 15. 16.
B,andC............................................,... Dimensions of conduits and location of points studied. Shapes D, E,andF............................................... Dimensions of conduits and location of points studied. Shapes circular, square, and G. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Coefficients for moment, thrust, and shear for uniform vertical load and uniform foundation reaction. Shapes A, B, and C . . . . . . . . Coefficients for moment, thrust, and shear for uniform vertical load and triangular foundation reaction. Shapes A, B, and C . . . . . . Coefficients for moment, thrust, and shear for concentrated vertical load and uniform foundation reaction. Shapes A, B, and C. . . . Coefficiepts for moment, thrust, and shear for concentrated vertical load and triangular foundation reaction. Shapes A, B, and C . . Coefficients for moment, thrust, and shear for triangular vertical load and uniform foundation reaction. Shapes A, B, and C. . . . Coefficients for moment, thrust, and shear for triangular vertical load and triangular foundation reaction. Shapes A, B, and C . . Coefficients for moment, thrust, and shear for vertical arch load and uniform foundation reaction. Shapes A, B, and C . . . . . . . . . . . Coefficients for moment, thrust, and shear for VerticaLarch load and triangular foundation reaction. Shapes A, B, and C . ; . . . . . . . . Coefficients for moment, thrust, and shear for dead weight of conduit.ShapesA,B, andC. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Coefficients for moment, thrust, and shear for uniform horizontal load on bothsides. Shapes’A, B, and C.. .*. . . . . . . . . . . . . . . . . . Coafticients for moment, thrust, and shear for triangular horizontal loadonbothsides.ShapesA,B,andC . . . . . . . . . . . . . . . . . . .. . . CJoefficients for moment, thrust, and shear for uniform internal radialload.ShapesA,B, andC.. . . . . . . . . . . . . . . . . . . . . . . . . . Coefficients for moment, thrust, and shear for triangular internal radial load and uniform foundation reaction. Shapes A, B, and c . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . , . . . . . . . . * . . * . ., . . . .
7 8 9 10 11 12 13 14 15 16 17 18 19 20 21
22 ... ill
NO.
17. Coefficients for moment, thrust, and shear for triangular internal radial load and triangular foundation reaction. Shapes A, B, andc~............................,..................... 18. Coefficients for moment, thrust, and shear for triangular external hydrostatic load including dead load. Shapes A, B, and C. . . . . 19. Coefficients for moment, thrust, and shear for uniform vertical load and uniform foundation reaction. Shapes D, E, and F. . , . . . . . 20. Coefficients for moment, thrust, and shear for uniform vertical load and triangular foundation reaction. Shapes D, E, and F. . . . . . 21. Coefficients for moment, thrust, and shear for concentrated vertical load and uniform foundation reaction. Shapes D, E, and F. . . . . . 22. Coefhcients for moment, thrust, and shear for concentrated vertical load and triangular foundation reaction. Shapes D, E, and F. . . . 23. Coefficients for moment, thrust, and shear for triangular vertical load and uniform foundation reaction. Shapes D, E, and F. . . . . . . . . . 24. Coefficients for moment, thrust, and shear for triangular vertical load and triangular foundation reaction. Shapes D, E, and F . . . . 25. Coefficients for moment, thrust, and shear for vertical arch load and uniform foundation reaction. Shapes D, E, and F. . . . . . . . 26. Coefficients for moment, thrust, and shear for vertical arch load and triangular foundation reaction. Shapes D, E, and F. . . . . . 27. Coefficients for moment, thrust, and shear for dead weight of conduit. Shapes D, E, and F. . . . . , . . . . . . . . . . . . . . . . . . . . . . . . 28. Coefficients for moment, thrust, and shear for uniform horizontal load on both sides. Shapes D, E, and F. . . . . . . . . . . . . . . . . . 29. Coefficients for moment, thrust, and shear for triangular horixontal loadonbothsides.ShapesD,E,andF.. . . .................. 30. Coefficients for moment, thrust, and shear for uniform internal radial load, Shapes D, E, and F. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 31. Coefficients for moment, thrust, and shear for triangular internal radial load and uniform foundation reaction. Shapes D, E, and F...................................................... 32. Coefficients for moment, thrust, and shear for triangular internal radial load and triangular foundation reaction. Shapes D, E, and F....,................................................. 33. Coefficients for moment, thrust, and shear for triangular external hydrostatic load including dead load. Shapes D, E, and F . . . . . . . 34. Coefficients for moment, thrust, and shear for uniform vertical load and uniform foundation reaction. Shapes circular, square, andG.................................................. 35. Coefficients for moment, thrust, and shear for uniform vertical load and triangular foundation reaction. Shapes circular, square, andG.................................................. 36. Coefficients for moment, thrust, and shear for concentrated vertical load and uniform foundation reaction. Shapes circular, square, and G.................................................. 37. Coefficients for moment, thrust, and shear for concentrated vertical load and triangular foundation reaction. Shapes circular, square, andG.................................................. iv
23 24 25 26 27 28 29 30 31 32 33 34 35 36
37
38 39
40
41
42
43
NO.
38. Coefficients for moment, thrust, and shear for triangular vertical load and uniform foundation reaction. Shapes circular, square, andG.................................................. 39. Coefficients for moment, thrust, and shear for triangular vertical load and triangular foundation reaction. Shapes circular, square, and G...................................................... 40. Coefficients for moment, thrust, and shear for vertical arch load and uniform foundation reaction. Shapes circular, square, and G . .. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 41. Coefficients for moment, thrust, and shear for vertical arch load and triangular foundation reaction. Shapes circular, square, andG.................................................. 42. Coefficients for moment, thrust, and shear for dead weight of conduit. Shapes circular, square, and G.. . . . . . . . . . . . . . . . . . . . . 43. Coefficients for moment, thrust, and shear for uniform horizontal load on both sides. Shapes circular, square, and G. . . . . . . . . . . . . 44. Coefficients for moment, thrust, and shear for triangular horizontal load on both sides. Shapes circular, square, and G. . . . . . . . . . . . . 45. Coefficients for moment, thrust, and shear for uniform internal radial load. Shapes circular, square, and G. . . . . . . . . . . . . . . . . . . . . . . . . 46. Coefficients for moment, thrust, and shear for triangular internal radial load and uniform foundation reaction. Shapes circular, squ~e,andG............................................ 47. Coefficients for moment, thrust, and shear for triangular internal radial load and triangular foundation reaction. Shapes circular, square, and G.......................................... 48. Coefficients for moment, thrust, and shear for triangular external hydrostatic load including dead load. Shapes circular, square, andG.................................................. 49. Coefficients for moment, thrust, and shear for triangular external hydrostatic load including dead load with conduits assumed to float.AUshapes......................................... 50. Coefficients for moment, thrust, and shear for horizontal passive pressure. Circular shape. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 51. Beggs Deformeter apparatus and shape B conduit model. . . . . . . . .
44
45
46
47 48 49 50 51
52
53
54
55 56 58
TABLE NO.
1. Correction factors for difTerent radii of curvature.
. .......... .....
5
INTRODUCTION
This monograph presents the results of the stress analysis, by means of the Beggs Deformeter apparatus,’ of nine shapes of single-barrel conduits. A partial analytical check was made using the least work method to determine the redundant reactions for all shapes due to a uniform vertical load and a uniform horizontal load. All personnel of the Experimental Design Analysis Section, including several rotation engineers who had training assignments in the section, assisted in the experimental work and computations. In particular, the assistance of W. T. Moody in computing the analytical solutions, and the work of H. E. Willmann, who prepared the drawings and also assisted in the experimental work and computations, is gratefully acknowledged. The nine shapes of conduits studied are those most widely used in Bureau of Reclamation structures. All except shape D and the square shape have semicircular top portions of uniform thickness. They can be further described as follows : 1. Shape A: horseshoe-shaped interior with a horizontal exterior base. 2. Shape B: circular-shaped interior with a horizontal exterior base. 3. Shape C: circular-shaped interior with a curved exterior base. 4. Shape D: circular-shaped interior with a square-shaped exterior. 5. Shape E: uniform thickness with a horizontal base. 6. Shape F: uniform thickness of horseshoe shape. 7. Shape G: transition between shape B and shape E with fillets of W r radius in lower interior corners. 8. Circular shape of uniform thickness. 9. Square shape of uniform thickness. Reaction coefficients for bending moment, thrust, and shear at selected locations along the centroidal axis of the conduits have been determined for 15 different loading conditions. 1 See Appendix
for description
of this instrument.
The 15 loading follows : 1. &I33
conditions
top with
considered
f3YJ3 foundation.
2. I1113 top with ‘m
foundation.
3.
1
top with
tflf3
foundation.
4.
I
top with
P-U
foundation.
5. hEr.
top with
Efm
foundation.
6. Q
top with
P-U
foundation.
7. P-Y
top with
Efa3
foundation.
8. 1/
top with
P-U
foundation.
9. Dead load with
PXI
foundation.
10. Uniform 11. B
horizontal
horizontal
12. Uniform
are as
both sides.
both sides.
internal
radial.
13. b
internal radial with
t3333 foundation.
14. b
internal
YV
15. R load.
external
radial with hydrostatic
foundation.
including
dead
Figures 1, 2, and 3 show cross sections of each shape, giving the dimensions and the location of points at which the reaction coefficients have been determined. Each shape was analyzed for three values of crown thickness, t, expressed in terms of the internal crown radius, r. These three values were t==rJ2, t=r/3, and t=r/6. A conduit of unit length was considered in the analysis. Bending moment, thrust, and shear coefficients were determined at the various locations shown, and are expressed in terms of unit intensity of loading and unit internal crown radius. Multiplying the reaction coefficient by the proper load factor gives the total bending moment, thrust, or shear at the centroid of the section under consideration.
1
APPLICATION
The reaction coefficients determined in the study are tabulated in figures 4 through 50 for the various shapes and loading conditions. The reaction coefficients are given for points on the right side of the conduits only, since the conduits and loadings are symmetrical about the vertical centerline. The shear reactions on the left side of the vertical centerline will have an opposite sign from those given for the points on the right side. Consistent units should be employed when using these data. Thus, if loads are expressed in pounds per square inch, all dimensions of the conduit must be expressed in inches. The bending moment will then be in inch-pounds per inch of conduit length and the thrust and shear in pounds per inch of conduit length. If the load is expressed in terms of pounds per square foot, the dimensions of the conduit must be expressed in feet, and the bending moment will be in foot-pounds per foot of conduit length and the thrust and shear in pounds per foot of conduit length. It will be noted that the bending moment in inch-pounds per inch is numerically equal to the bending moment in foot-pounds per foot. One should bear in mind that this analysis assumes no restraint to the deformation of the conduit. In some cases this restraint, or passive pressure, may be important. Some work on passive pressures on tunnel linings through rock has been done by R. S. Sandhu.2 By using his method for determining the intensity of the passive pressure, and using the moment, thrust, and shear coefficients 2 Sandhu, R. S., “Design of Concrete Linings for Large Underground Conduits,” Journal of the American Concrete Institute, December 1961, pp. 737-750.
for a circular conduit given by figure 50, the effect of restraint may be approximated. The foundation load distribution due to a vertical load on the conduit must be assumed, and is influenced by the modulus of elasticity of the foundation material. As the foundation modulus increases, the foundation load distribution approaches a concentration at the outside corners of the conduit, and as it decreases the load approaches a uniform distribution. For all vertical loading conditions except three, two distributions were assumed, viz., uniform, and triangular with zero at the center and maximum at the outside corners. For the dead load the assumed foundation reaction is minimum at the center varying linearly to a maximum at the outside corners, with the intensity at the center equal to the intensity of the weight of the conduit at the center of the base. For the triangular internal radial load the assumed foundation reactions were uniform, and triangular with zero at the outsides and maximum at the center. For the triangular external hydrostatic load; including dead load, the unit weight of the conduit material and the unit weight of water were assumed to be 150 and 62.4 pounds per cubic foot, respectively. With these assumptions the weight of the conduit for the t=r/6 case, except shape D, is less than the uplift, causing the conduit to float. The reaction is assumed to be uniformly distributed across the top. The coefficients for this assumption (conduit floating) are given in figure 49. In the other figures of this loading condition, tension is assumed to develop uniformly along the foundation.
8
DETERMINATION OF NORMAL STRESS DISTRIBUTION
In a curved beam the neutral axis will not be coincident with the centroidal axis, and the normal stress distribution on radial lines, due to moment, will not be linear. However, the radius to the neutral axis and the normal stress distribution may be determined by the following equations, derived from the Winkler-Bach theory for curved beams: 3
T y,, e
is the thrust at the centroidal axis is the distance from the neutral axis to the point of interest (positive outward) is the distance from the centroidal axis to the neutral axis.
As t decreases e approaches zero, and the ug distribution approaches linearity. a#, as computed by equation (2), is only for a constant thickness section. Where the section thickness is not constant, the distribution of stresses must be determined by some other method, such as photoelasticity. The extreme fiber stress in a constant thickness curved beam due to bending moment may be determined by the equation: Mt CT)=Krr
t rn=Gqqq
(1)
where is T is r, is t is In is r,
the the the the the
radius to the neutral axis internal radius external radius wall thickness (rO-r> log to the base e, T ue=-+ t
MY, (r,+y&
where (Tb is M is t is I is K is
the extreme fiber Stress the bending moment at the section the width of the section the moment of inertia of the section the factor by which the extreme fiber stress, assuming linear distribution, is modified to correct for curvature. The following equation for K was obtained by equating equations (2) and (3) : (4) The values of K and e for the t/r ratios used in this study are tabulated below:
(2)
TABLE l.-Correction
factors for different
where a0
M
(3)
radii
of curvature
K is the normal stress in the tangential direction is the bending moment at the centroidal axis
3 Murphy, McGraw-Hill 219.
Glenn, Advanced Mechanics Book Co., Inc., New York,
of Materials, 1946, pp. 217-
e
t Inside fiber 42 r/3 r/6
1.153 1.105 1. 054
o;EP 0.880 0.912 0.951
. 0. 0168r 0.008Or 0. 0021r 6
03lOlllS
SlNlOd
JO
3 ONW ‘8
‘V
NOllWOl
ONV
S3dVHS
SllfMN03
SISAlVNV SS3US U313WYOd30 llnQN03 13clWle 319NIS
A0
SNOISN3WlCl
SO038
OfbE. 66Of JlLZf
'I ‘0
JbSOZ’O
LZLS'Z
ILIZ’b
JSS6b‘O JZbLf
‘0
iad
I
OIJV
Jf699’0
01 ‘6
JblbS’O
II
‘0 I
3Nl-l JOLL61’2
90
HION
JfbZSf.2
3
IlNlOd JCZCOS’I
10
HI
8
3dVHS
Z
3dWS
+nOqO
3NI-l
(O~!J(blUUI~S
I
1 OOEO’E
1 OLIL’b
I 1
(zJ)oW’
1
Symmetrical about vertical centerline-m
A ---------SHAPE
D --_--_-_ Lea
D
SHAPE
I
+j+AJ+&
“Centraidal
about
LA-+SHAPE
It=flt=5lt=fl 0.33333r
0.33333~
0.33333 r
D
I. 50000r
I.33333r
I. l6667r
4.4635
2.7773
I. Z895
7
SINGLE BARREL CONDUIT BEGGS DEFORMETER STRESS ANALYSIS DIMENSIONS
OF
CONDUITS
AND
SHAPES
L,_
oxis
E
A
Area(#) For length of lines for Points 6 thru ond 9 thru 14, se6 Sha’pc 8.
Svmmctrical
I+----..._
LOCATION
0, E, AND
OF F
POINTS
STUDIED
F
’
Symmetrical obout vertical centerline--za
SQUARE
CIRCULAR
t=+ Arto(r*)
3.9t70
t-i
t=+
2.4433
1.1345
Arco(r*)
BEGGS DIMENSIONS
OF
SHAPE
t-f
t=f
t=f
5.0000
3.llII
1.4444
SINGLE BARREL CONDUIT DEFORMETER STRESS ANALYSIS CONDUITS
SHAPES
AND
CIRCULAR,
LOCATION SOUARE,
OF AN!
POINTS G
STUDIED
-%.
A+-----
G
FIGURE
SINGLE BARREL CONDUIT BEGGS DEFORMETER STRESS ANALYSIS COEFFICIENTS +
Sign
convantion
UNIFORM
VERTICAL.
FOR MOMENT, LOADSHAPES
THRUST,
UNIFORM A,
8,
AND
FOUNDATION
AND
SHEAR REACTION
C
X- PEL-372
4
FlGUPE
a L 9 m
SINGLE BARREL CONDUIT BEGGS DEFORMETER STRESS ANALYSIS COEFFICIENTS UNIFORM
VERTICAL
FOR MOMENT,
THRUST,
LOAD-TRIANGULAR SHAPES
A,
AND
FOUNDATION B,
AND
SHEAR REACTION
C
X-PEL-373
5
FIGURE
SINGLE BARREL CONDUIT BEGGS DEFORMETER STRESS ANALYSIS COEFFICIENTS CONCENTRATE6i&CAL
FOR MOMENT, LOAD SHAPES
THRUST,
-UNIFORM A,
6,
AND
FOUNDATION AND
SHEAR REACTION
C
X-PEL-374
6
~~~, to.536
to.716
t1.361
to.444
-to.632
tl.21
I
SINGLE BARREL CONDUIT BEGGS DEFORMETER STRESS ANALYSIS COEFFICIENTS CONCENTRATED
FOR MOMENT,
VERTICAL
SHAPES
5EP
8.lDlO
THRUST,
LOAD -TRIANOVLAR A,
6,
AND
AND
FOUNDATION
SHEAR REACTION
C
X-PEL
- 375
BEGGS
SINGLE BARREL CONDUIT DEFORMETER STRESS ANALYSIS
COEFFICIENTS TRIANGULAR
FOR MOMENT,
VERTICAL SHAPES
LOAD
A,
THRUST,
AN0
UNIFORM
FOUNDATION
8,
C
AND
SHEAR REACTION
X-PEL-
14
1034
SINGLE BARREL CONDUIT BEGGS DEFORMETER STRESS ANALYSIS COEFFICIENTS TRIANSULAR
FOR MOMENT,
VERTICAL
LOAD - TRIANGULAR
SHAPES
SEP.
20,
Is*4
THRUST,
A,
8,
AND
AND
FOUNDATION
SHEAR REACTION
C
X-PEL-IO35
15
NOTE’g represents the vea*ht per unit volume of soil cover the conduit sect,on with those of the
on the arch of I” un,+s consistent rod,us r
SINGLE BARREL CONDUIT BEGGS DEFORMETER STRESS ANALYSIS
:03
COEFFICIENTS
U-F
VERTICAL
ARCH
FOR MOMENT, LOAD SHAPES
SEP.
16
28.
1964
-
UNIFORM A,
B,
THRUST, FOUNDATION AND
AND
SHEAR
REACTION
C
X-PEL-1036
FIQURE
t‘.-a(r+t) ..i !10 Ia NOTE: g represents the weight per unit volume of soil cover on the arch of the conduit sectton in units consjstent with those of the radius r
SINGLE BARREL CONDUIT BEGGS DEFORMETER STRESS ANALYSIS COEFFICIENTS VERTICAL
ARCH
FOR MOMENT,
THRUST,
LOAD-TRIANGULAR SHAPES
FOUNDATION A,
0,
AND
C
AND
SHEAR REACTION
I I
NOTES c represents the weight per unit volume concrete or other motertal m units consistent wth Ihose of the radius r. See Figure I for net area of shapes
of
BEGGS
SINGLE BARREL CONDUIT DEFORMETER STRESS ANALYSIS
COEFFICIENTS
FOR MOMENT, DEAD
+ Sign
convmtion
THRUST,
AND
SHEAR
WEIGNT OF CONDUIT
SHAPES
A, B, AND C
X-PEL-1037
18
FIGURE
SINGLE BARREL CONDUIT BEGGS OEFORMETER STRESS ANALYSIS COEFFICIENTS UNIFORM
FOR MOMENT,
THRUST,
HORIZONTAL
LOAD
SHAPES
8,
A,
-
AND
BOTH C
AND SIDES
SHEAR
13
t - r6
SINGLE BARREL CONDUIT BEGGS DEFORMETER STRESS ANALYSIS COEFFICIENTS TRIANGULAR
FOR MOMENT, HORIZONTAL SHAPES
THRUST, LOAD
A,
E,
AND
-
BOTH
AND
SHEAR
SIDES
C
X-PEL-379
SINGLE BARREL CONDUIT BEGGS DEFORMETER STRESS ANALYSIS COEFFICIENTS
FOR MOMENT,
UNIFORM
THRUST,
INTERNAL
SHAPES
A,
RADIAL 8,
AN0
AND
SHEAR
LOAD C
21
Wessun vertical
Wessure vertical
ditiribution along C of conduit -:
dlstnbution along e ot conduit. --,
NOTE: w represents the wright par unit volume of woier in units consistent with those of the radius P.
SINGLE BARREL CbNDUlT BWGS DEFORMETER STRESS ANALYSIS + Sign
convention
COEFFICIENTS TRIANGULAR
INTERNAL
FOR MOMENT, RADIAL SHAPES
LOAD
THRUST, - UNIFORM
A, 8, AND C
AND
SHEAR
FOUNDATION
REACTION
POINT
Pressure vwticol
N
T
s
H
7
T
s
M
T
S
F
distribution obrq C of conduit-..
NOTE : I represents the weight par volume of water In units consiat*nt with those of the radius r.
unit
SINGLE BARREL CONDUIT BEGGS DEFORMETER STRESS ANALYSIS COEFFICIENTS + Sqn
convention
TRIANGULAR
INTERNAL
FOR MOMENT, RADIAL
LOAD
SHAPES
THRUST,
- TRIANGULAR A, 0,
AND
AND
SHEAR
FOUNDATION
REACTION
C
23
m
Deod one-half
Dead
weight of of conduit
WeiQht
of
0
NOTES: Y rWWS~“tr the WlQht per ““I+ volume of water in units consistent with those of the radws r The assumed WeiQht per unit volume of the conduit I?) IsOw/62.4.
l
Tenston is assumption
assumed that
to develop the conduits
at
the foundotion. For the float see Figure 49.
SINGLE BARREL CONDUIT BEGGS DEFORMETER STRESS ANALYSIS COEFFICIENTS
FOR MOMENT,
THRUST,
TRIANGULAR EXTERNAL HYDROSTATIC INCLUDINQ DEAD LOAD SHAPES
AND
SHEAR
LOAD
A, 0, AND C
x-
24
PEL-
1039 -.I
FISURE
I
19
.-1
ftttttfftttftttt?f?ful--I”
BEGGS
SINGLE BARREL CONDUIT DEFORMETER STRESS ANALYSIS
COEFFICIENTS UNIFORM
VERTICAL
FOR MOMENT, LOAD SHAPES
SEP
ea.
1964
-
THRUST,
UNIFORM D,
E,
AND
SHEAR
FOUNDATION AND
REACTION
F
x-
PEL-
1040
25
BEGGS
SINGLE BARREL CONDUIT DEFORMETER STRESS ANALYSIS
COEFFICIENTS UNIFORM
VERTICAL
FOR MOMENT, LOAD
-
SHAPES
THRUST,
AND
TRIANGULAR
FOUNDATION
D,
F
E,
AND
SHEAR REACTION
x- PEL-
26
104 I
FIGURE
el
SINGLE BARREL CONDUIT BEGGS DEFORMETER STRESS ANALYSIS COEFFICIENTS CONCENTRATED +
Sign
FOR MOMENT,
VERTICAL
LOAD
-
THRUST,
UNIFORM
AND
FOUNDATION
SHEAR REACTION
convention
SHAPES
D,
E,
AND
F
X-PEL-1042
27
FIQURE
t=j
I +t)
22
t = 5
2vcr
BEGGS
SINGLE BARREL CONDUIT DEFORMETER STRESS ANALYSIS
COEFFICIENTS CONCENTRATED +
Sign
VERTICAL
FOR MOMENT, LOAD
conventlo” SHAPES
-
THRUST,
TRIANGULAR D,
E,
AND
AND
FOUNDATION
SHEAR REACTION
F
X-PEL-
1043
FIGURE
BEGGS
SINGLE BARREL CONDUIT DEFORMETER STRESS ANALYSIS
COEFFICIENTS TRIANGULAR +
Sign
convention
23
FOR MOMENT,
VERTICAL
LOAD SHAPES
D,
THRUST,
AND
UNIFORM
FOUNDATION
E,
F
AND
SHEAR REACTION
X-PEL-1044
29
SINGLE BARREL CONDUIT BEGGS DEFORMETER STRESS ANALYSIS COEFFICIENTS TRIANGULAR
FOR MOMENT,
VERTICAL
THRUST,
LOAD - TRIANGULAR
SHAPES
D.
E,
AND
AN0
SHEAR
FOUNDATION
REACTION
F
X-PEL-1045
30
Note:
No
vertical
POINT
1101E: g rmprwentr the weight per unit VO~U~C of soil cover on the arch of the conduit section in units consister with those of the radius r.
7
arch
Y
lood
on
T
S
Shape
D.
M
T
S nrl
-a
H
T
s
11 SINGLE BARREL CONDUIT BEGGS DEFORMETER STRESS ANALYSIS COEFFICIENTS FOR MOMENT, THRUST, AND SHEAR VERTICAL
+
Sign
convention
ARCH
LOAD
- UNIFORM
SHAPES
0.
E,
FOUNDATION AN0
REACTION
F
s
X-PEL-IO46
31
FIGURE
Note:
No
vertlcol
arch
load
on
Shape
0.
NOTE: g represents the weight per unit volume of soil cover on the arch of the conduit section I” “nits c:onsis+en, with +hose of the rod,“* r
BEGGS iD
COEFFICIENTS
i
VERTICAL
c I
ARCII
FOR MOMENT, LOAD-TRIANGULAR SHAPES
+
Sign
SEP. es. ,964
32
SINGLE BARREL CONDUIT DEFORMETER STRESS ANALYSIS THRUST, FOUNDATION D,
E,
AND
AND
SHEAR REACTION
F
convention
X-PEL-1047
26
NOTES’ c represents the ueiqht per unit volume concrete or other moterod in units consistent wth those of the radius r. See Figure 2 for net orea ot shows.
of
BEGGS
SINGLE BARREL CONDUIT DEFORMETER STRESS ANALYSIS
COEFFICIENTS +
SEP.
2%
Slqn
1964
convantion
FOR MOMENT,
THRUST,
DEAD
OF
CONDUIT
E,
AND
WEIGHT
SHAPES
D,
AND
SHEAR
F
X -PEL-1048
33
-y
h “-
I
BEGGS
SINGLE BARREL CONDUIT DEFORMETER STRESS ANALYSIS
COEFFICIENTS UNIFORM
FOR MOMENT, HORIZONTAL SHAPES
THRUST,
LOAD D,
E,
AND
BOTH
AND
SHEAR
SIDES
F
X-PEL-
34
1049
SINGLE BARREL CONDUIT BEGGS DEFORMETER STRESS ANALYSIS COEFFICIENTS TRIANGULAR
FOR MOMENT, IfORltONTAL SHAPES
THRUST, LOAD
0, E,
AND
-
BOTH
AND
SHEAR
SIOES
F
X-PEL-
1010
35
FIGURE
BEGGS
SINGLE BARREL CONDUIT DEFORMETER STRESS ANALYSIS
COEFFICIENTS
FOR MOMENT,
UNIFORM t
Sign
INTERNAL
THRUST, RADIAL
AND
SHEAR
LOAD
Convention SHAPES
D,
E,
AND
F
X-PEL-
36
30
1051
FIGURE
Pressure vertical
Pressure vertical
31
distribution along k of conduit-.:
dirtributlon along C of conduit--%.
NOTE: u represents the weight par unit volumr of voter in units consistent with those of the radius r.
BEGGS
SINGLE BARREL CONDUIT DEFORMETER STRESS ANALYSIS
COEFFICIENTS TRIANGULAR +
Sign
convention
INTERNAL
FOR MOMENT, RADIAL SHAPES
LOAD D,
THRUST, -
E.
UNIFORM AND
AND
SHEAR
FOUNDATION
REACTION
F
X-PEL-IO52
37
FIGURE
t = i Pressure vertical
Pressure vertical
Pressure VWtiCOI
t = f
t=f
distribution olonp t of oonduit..
dishlbution olonp C of Conduit-.,
distribution along C of conduit-.,
NOTE: Y represents the weight per unit wotunw of rater in units consistent with thow of the radius r.
SINGLE BARREL CONDUIT BEGGS DEFORMETER STRESS ANALYSIS COEFFICIENTS TRIANOULAR
INmNAL
R)R MOMENT, RADIAL
THRUST,
LOAD - TRIANGULAR
SHAPES
D, E, AND
AND
SHEAR
FOUNDATION
REACTION
F
x-PEL-IO63
38
39
FIQIJRE
Dead on5-half
33
Y ‘ei ht of o P conduit
t-f, t-i, t-i.
D5ad one-halt
5.SeIwr*
t-:* .t
wight af of mndult
-f* t = f.
D5od one-hall
5.55.
wr’
I.55OW’
r5Wt of of conduit
w;155: w reprewnb the wlght p.r unit VOhmw of ratw In unite con5lrtent with tho55 of th. rodiu5 r. Th5 ouumod roight p51 unit voIum5 of t)u conduit I5 l5Ow/55.4.
l
Tension is assumed to olsumption that the
develop
conduits
at the foundation. For the float see Figure 49.
SINGLE ARREL CONDUIT BEGGS DEFORM1 TER STRESS ANALYSIS COEFFICIENTS
FOR MOMENT,
THRUST,
TRIANGULAR EXTERNAL HYDROSTATIC INCLUDINQ DEAD LOAD SHAPES
AND
SHEAR
LOAD
D, E, AND F
39
utttttrtltrltttttttt11 --fL SINGLE BARREL CONDUIT BEGGS DEFORMETER STRESS ANALYSIS CQEFFICIENTS UNIFORM +
Sign
VERTICAL
FOR MOMENT, LOAD
-
THRUST,
UNIFORM
AND
FOUNDATION
SHEAR REACTION
convention SHAPES
CIRCULAR,
SGUARE,
AND
G
X-PEL-I055
SINGLE BARREL CONDUIT BEGGS DEFORMETER STRESS ANALYSIS COEFFICIENTS UNIFORM
VERTICAL SHAPES
FOR MOMENT, LOAD
-
CIRCULAR,
THRUST,
TRIANGULAR SQUARE,
AN0
SHEAR
FOUNDATION AND
REACTION G
X-PEL-1056
41
FIGURE
SINGLE BARREL CONDUIT BEGGS DEFORMETER STRESS ANALYSIS COEFFICIENTS CONCENTRATED
FOR MOMENT,
VERTICAL SHAPES
LOAD CIRCULAR,
-
THRUST,
UNIFORM SPUARE,
AND
FOUNDATION AND
SHEAR REACTION
0
X-PEL-
42
1057
36
: a
--r----
7 -
___
2
f LlLzziJ
(I w a. a is
I
i
(( _ ,
, -‘-
t
i ‘I:
-
SINGLE BARREL CONDUIT BEGGS DEFORMETER STRESS ANALYSIS COEFFICIENTS CONCENTRATED
FOR MOMENT,
THRUST,
TRIANOULAR
VERTICAL
LOAD -
SHAPES
CIRCULAR,
SQUARE,
AND
SHEAR
FOUNDATION AND
REACTION
0
X-PLL-
1058
43
SINGLE BARREL CONDUIT BEGGS DEFORMETER STRESS ANALYSIS COEFFICIENTS TRIANGULAR +
Sign
VERTICAL
ee,
LOAD
-
THRUST,
UNIFORM
AND
SHEAR
FOUNDATION
REACTION
convention SHAPES
SEP.
FOR MOMENT,
1964
CIRCULAR,
SQUARE,
AND
0
X-PEL-IO59
FIGURE
39
SINGLE BARREL CONDUIT BEGGS DEFORMETER STRESS ANALYSIS COEFFICIENTS TRIANGULAR
VERTICAL SHAPES
FOR MOMENT, LOAD
-
THRUST,
TRIANGULAR
CIRCULAR,
SQUARE,
AND
SHEAR
FOUNDATION AND
REACTION
G
X-PEL-1060
45
FIQURE
t-f
t-L
t-S-
3
I
6
utttltffttflnmltms.: o.*l446(r
l t1..-a’
Note:
No
vertical
arch
1006
on
square
shopc.
NOTE: g represents ttm wight par unit volume of wil cover on the arch of the conduit section in units conrirteni with those of the rodiur r.
SINGLE BARREL CONDUIT BEGGS DEFORMETER STRESS ANALYSIS COEFFICIENTS VERTICAL
SHAPES
SEP.
46
Le.
1964
FOR MOMENT,
THRUST,
ARCH LOAQ - UNIFORM CIRCULAR,
AN0
FOUNDATION
SQUARE.
AND
SHEAR
REACTION 6
X-PEL-IO61
40
Note :
No
vertical
arch
load
on
square
shape.
-f 0 1(r+t)
i
nom:
g represents the n@ht PM unit volum. of ~11 COYW on the arch of +he conduit aaction in units consistent with those of the radius
r
SINGLE BARREL CONDUIT BEGGS DEFORMETER STRESS ANALYSIS COEFFICIENTS VERTICAL
ARCH SHAPES
FOR MOMENT, LOAD
THRUST,
- TRIANDULAR
CIRCULAR,
AND
FOUNDATION
SQUARE,
AND
SHEAR REACTION
B
X-PEL-106R
47
FIQURE
NOTES: c represents VOlumC of concrete in units consirtant radius r. See FIgwe 3 for
the weight per unit or other motwial with those ot the net
or.x
of
sh.,,xs.
SINGLE BARREL CONDUIT BEGGS DEFORMETER STRESS ANALYSIS COEFFICIENTS
FOR MOMENT, DEAD WElSHf
+
SEP. PI.
4-a
Sign
I,d.
conwntion
SHAPES
CIRCULAR,
THRUST,
AND
SHEAR
OF CONDUIT SQUARE,
AND
0
X-PEL-1063
42
-1
h p-
-04
h b-
*
-1
h p-
-4
h )r-
SINGLE BARREL CONDUIT BEGGS DEFORMETER STRESS ANALYSIS COEFFICIENTS UNIFORM SHAPES
FOR MOMENT, HORIZONTAL CIRCULAR,
THRUST,
LOAO
-
SQUARE,
AN0
BOTH
SHEAR
SIDES
AND
0
x-
PEL-
IO64
49
FIQURE
SINGLE BARREL CONDUIT BEGGS DEFORMETER STRESS ANALYSIS COEFFICIENTS
50
FOR MOMENT,
TRIANQULAR
HORIZONTAL
SHAPES
CIRCULAR,
THRUST, LOAD
-
SQUARE,
AND
BOTH AND
SHEAR
SIDES 0
44
FIQURL -- 45
I
I)
D
0
, -
1
0
I-t
,.. I-I
SINGLE BARREL CONDUIT BEGGS DEFDRMETER STRESS ANALYSIS COEFFICIENTS
FOR MOMENT,
UNIFORM +
Sign
INTERNAL
THRUST, RADIAL
AND
SHEAR
LOAD
convention
SHAPES
CIRCULAR.
SQUARE,
AN0
Q
X-PLL-
1055
51
Prrrrum vertical
Pressure vertical
distribution along e of conduit-.,
distribution along E of conduit.,
NOTE’ w reweeentr the weight per unit volume of voter in units consistent wlh those of the radius r.
)I+ SINGLE BARREL CONDUIT BEGGS DEFORMETER STRESS ANALYSIS
I
COEFFlClENfS
m-
TRIANGULAR L q
+
Sqn
convention
INTERNAL SliAPES
FOR MOMENT, RADIAL
LOAD
CIRCULAR,
THRUST, -
UNIFORM SOUARE,
AND
SHEAR
FOUNDATION AND
REACTION
G
> r SEP.
52
er,
1964
X-PEL-1067
FIQURE
Pressure
distribution
Pressure vertical
distribution along C of conduit-.,
Pressure vertlcol
w repmsante volume of rater with those of
NOTE:
47
along
distribution along c of conduit-..
the weight per unit in units conristrnt
the rodtur
r.
SINGLE BARREL CONDUIT BEGGS DEFORMETER STRESS ANALYSIS COEFFICIENTS TRIANGULAR + Sinp convmtion
SEP.
er,
1004
INTERNAL SHAPES
FOR MOMENT, RADIAL
LOAD -
CIRCULAR,
THRUST,
TRIANGULAR SQUARE,
AND
SHEAR
FOUNDATION AND
REACTION
G
X - PEL-IO68
53
hod wai ht of one-holf f COIldUll
D*Od wqht of one-half of conduit 6.010 wr’ t-f, t - 5, 5.7.0 wr’ 1.75* wr’ t-f,
MOTES:w r5pr555nts the w5ipht p5r unit volum* of water In units conatmt with those of th5 rodlur r. Ths owumed weight p5r unit voIum5 of th5 conduit I5 150~/6~.4. ,+ D
l
Tension is assumed ta develop at the foundation. Far the assumption that the conduits float rep Figure 49.
SINGLE BARREL CONDUIT BEGGS DEFORMETER STRESS ANALYSIS COEFFICIENTS TRIANWLAR SHAPES
FOR MOMENT,
THRUST,
AND
EXTERNAL HYDROSTATIC INCLUDING DEAD LOAD CIRCULAR,
SOUARE,
AND
SHEAR
LOAD Q X-PEL-1069
54
SHAPE POINT
7
M
A
SHAPE
T wr’
0
SHAPE
C
SHAPE
G
S
-1
SHAPE
SUAPE
E
F
Top rtoction of uniform
SOUARE
CIRCULAR
is ossumed to be intensity, v.
For loading diagram, t sign convention, ond the assumption that the conduits do not floot see Figures 16, 33, ond 48. Note:
Shape
D
does
not
floot
SINGLE BARREL CONDUIT BEGGS DEFORMETER STRESS ANALYSIS COEFFICIENTS
FOR MOMENT,
THRUST,
TAIANQULAR EXTERNAL HYDAOSTAtlO INCLUDINS DEAD LOAD CONDUITS
ASSUMED ALL
em,
SHEAR
LOAD
TO FLOAT
SHAPES t-
,EP.
AN0
i x- PEL-
1944
.
1070
1-1
r -0.218 ~~
II +0.5301
L
2
-0.196
0
1
to.512
-0.137 -0.265
II II
-0.
IB3
1 -0.164 11 -0.109
I to.471 I
II
1 to.455
1 -0.122
1 to.4061
6 -0.236
~l--o.t I, --
50 I z.412 --I -...-I
-0.135
I +0.39q
r- a -
-0.107
ll -0.090
-0.238
8
1+0.2l
9
~t0.103~t0.242~t0.420~i+0.065~t0.215~+0.373
1
IO
I-0.024itO.3751
I
II
I-0.130
I2
-0.196
to.512
I3
I-O.218
I +0.530
Sign
convention
t
I
to.082
l+o.459
to.306
t 0. I79
to.073
to.272
to.149 II- +0.069
H
I
+ 0.357 + 0.398 to.412
SINGLE BARREL CONDUIT BEGGS DEFORMETER STRESS ANALYSIS COEFFICIENTS
FOR MOMENT,
HORIZONTAL
PASSIVE
CIRCULAR
56
THRUST, PRESSURE SHAPE
AN0
SHEAR
1
APPENDIX: THE BEGGS DEFORMETER
This study has been made, using the Beggs Deformeter apparatus 4 6 e (figure 51). The basis of the method is a direct application of Maxwell’s Theorem of Reciprocal Deflections, which states that. for any two points on a structure, the ratio of the displacement at the fist point to the load causing it, applied at the second point, is equal to the ratio of the displacement at the second point to the load causing it, applied at the fist point. Displacements are measured in the load directions. In the general application of this method of stress analysis, an elastic scale model of the structure under consideration is deformed at a cut in the model by use of a special set of gage blocks and plugs. Three sets of plugs are used to apply a rotational, a normal, and a shearing displacement at the gage block. Microscopes equipped with filar eyepieces are used to measure the model deflections at points corresponding to the load points of the actual structure. Deflections are measured in the direction of the prototype loads. No loads are applied to the model. Deflections of the model are read at prototype load points for displacements applied at the gage block. The difference in microscope readings is a measure of the model deflection induced by the change at the gage block from the first position of the plugs to the second position of the plugs. From Maxwell’s Theorem the following equations may be written for the redundant reactions at the cut section:
-.
For a concentrated load
M,=PFn .
M
For a distributed load
MI=:
pe,dl M s
4 Beggs, G. E., “An Accurate Solution of Statically Indeterminate Structures by Paper Models and Special Gages,” Proceedings ACI, vol. XVIII, 1922, pp. 58-78. 5 McCullough, C. B., and Thayer, E. S., Elastic Arch iii&es, John Wiley and Sons, New York, 1931, pp. 2826 ‘Phillips, H. B., and Allen, formeter Theory and Technique,” Denver, Colo., July 1965.
I. E., “The Beggs DeBureau of Reclamation,
SFPF
Sl=$ S
TI==PF T
S
s
pes dl
Tl= $spe, T
dl
where
d, is the angular rotation ds is dT is eM is es is eT is I
is
MI is n p
is is is
$
is
P
T1 is The
applied at the cut by the moment plugs the displacement applied at the cut by the shear plugs the displacement applied at the cut by the thrust plugs the measured deflection at a load point, in the direction of the load, due to d, the measured deflection at a load point, in the direction of the load, due to ds the measured deflection at a load point, in the direction of the load, due to dT the load length the redundant moment reaction at the cut the scale factor (prototype to model) a load acting at a point on the prototype the load intensity on the prototype at the deflection point the redundant shear reaction at the cut the redundant thrust reaction at the cut.
only
unknowns
in
these
equations
are
MI, T,, and S,. In the actual operation of the Beggs Deformeter the arithmetic is simplified by the use of calibration factors based on the plug dimensions and the eyepiece scales. An influence line through points obtained by multiplying the deflection ordinates by the proper calibration factor gives directly the magnitude of the moment, thrust, or shear at the gage block position for a unit traveling load. It should be pointed out that the Beggs Deformeter method automatically takes into account the strain energy in a structure due to moment, thrust, and shear as well as haunch effects and other shape changes.
57
FIGURE
51.
-Beggs
Deformeter
apparatus
and
shape
B conduit
model.
58 GPO
850-512
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