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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 of the Interior is responsible for the development and conservation of the Nation’s water resources in the Western United States.
The Bureau’s original purpose “*to provide for the reclamation of arid and semiarid lands in the West” today covers a wide range of interre- lated functions. These include providing municipaland industrial water supplies; hydroelectric power generation; irrigation water for agricul- ture; water quality improvement; flood control; river navigation; river regulation and control; fish and wildlife enhancement; outdoor recrea- tion; 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 govern- men ts, academic institutions, water-user organizations, and other concerned groups.
A WATER RESOURCES TECHNICAL PUBLICATION
Engineering Monograph No. 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, preserv- ing the environmental and cultural values of our national parks and historical places, and providing for the enjoyment of life through out- door 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 respon- sibility 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 PRINTING OFFICE
WASHINGTON : 1968
For sale by the Superintendent of Documents, U.S. Government Printing Office, Washington, D.C. 20402, or the Bureau of Reclamation, Attention 822A, Denver Federal Center, Denver, Colorado 80225.
CONTENTS
INTRODUCTION. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
APPLICATION................................................
DETERMINATION OF NORMAL STRESS DISTRIBUTION. . .
APPENDIX: THE BEGGS DEFORMETER . . . . . . . . . . . . . . . . . . . .
FIGURES
No.
1. Dimensions of conduits and location of points studied. Shapes A, B,andC............................................,...
2. Dimensions of conduits and location of points studied. Shapes D, E,andF...............................................
3. Dimensions of conduits and location of points studied. Shapes circular, square, and G. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
4. Coefficients for moment, thrust, and shear for uniform vertical load and uniform foundation reaction. Shapes A, B, and C . . . . . . . .
5. Coefficients for moment, thrust, and shear for uniform vertical load and triangular foundation reaction. Shapes A, B, and C . . . . . .
6. Coefficients for moment, thrust, and shear for concentrated vertical load and uniform foundation reaction. Shapes A, B, and C. . . .
7. Coefficiepts for moment, thrust, and shear for concentrated vertical load and triangular foundation reaction. Shapes A, B, and C . .
8. Coefficients for moment, thrust, and shear for triangular vertical load and uniform foundation reaction. Shapes A, B, and C. . . .
9. Coefficients for moment, thrust, and shear for triangular vertical load and triangular foundation reaction. Shapes A, B, and C . .
10. Coefficients for moment, thrust, and shear for vertical arch load and uniform foundation reaction. Shapes A, B, and C . . . . . . . . . . .
11. Coefficients for moment, thrust, and shear for VerticaLarch load and triangular foundation reaction. Shapes A, B, and C . ; . . . . . . . .
12. Coefficients for moment, thrust, and shear for dead weight of con- duit.ShapesA,B, andC. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
13. Coefficients for moment, thrust, and shear for uniform horizontal load on bothsides. Shapes’A, B, and C.. .*. . . . . . . . . . . . . . . . . .
14. Coafticients for moment, thrust, and shear for triangular horizontal loadonbothsides.ShapesA,B,andC . . . . . . . . . . . . . . . . . . . . . .
15. CJoefficients for moment, thrust, and shear for uniform internal radialload.ShapesA,B, andC.. . . . . . . . . . . . . . . . . . . . . . . . . .
16. Coefficients for moment, thrust, and shear for triangular internal radial load and uniform foundation reaction. Shapes A, B, and c . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . , . . . . . . . . * . . * . ., . . . .
PW 1
3
5
57
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..................................................
23
24
25
26
27
28
29
30
31
32
33
34
35
36
37
38
39
40
41
42
43
iv
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. . . . . . . . .
TABLE NO.
44
45
46
47
48
49
50
51
52
53
54
55
56 58
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 en- gineers who had training assignments in the sec- tion, assisted in the experimental work and com- putations. 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 acknowl- edged.
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 deter- mined for 15 different loading conditions.
1 See Appendix for description of this instrument.
The 15 loading conditions considered are as follows :
1. &I33 top with 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 horizontal both sides.
11. B horizontal both sides.
12. Uniform internal radial.
13. b internal radial with t3333 foundation.
14. b internal radial with YV foundation.
15. R external hydrostatic including dead load.
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 deter- mining 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 distribu- tion 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 dis- tributions 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 as- sumed 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
where
t rn=Gqqq (1)
r, is the radius to the neutral axis T is the internal radius r, is the external radius t is the wall thickness (rO-r> In is the log to the base e,
T ue=-+ MY,
t (r,+y& (2)
where
a0 is the normal stress in the tangential direction
M is the bending moment at the centroidal axis
3 Murphy, Glenn, Advanced Mechanics of Materials, McGraw-Hill Book Co., Inc., New York, 1946, pp. 217- 219.
T is the thrust at the centroidal axis y,, is the distance from the neutral axis to
the point of interest (positive outward) e is the distance from the centroidal axis
to the neutral axis.
As t decreases e approaches zero, and the ug dis- tribution 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 thick- ness curved beam due to bending moment may be determined by the equation:
Mt CT)= Krr (3)
where (Tb is the extreme fiber Stress M is the bending moment at the section t is the width of the section I is the moment of inertia of the section K is 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:
TABLE l.-Correction factors for different radii of curvature
t
42 r/3 r/6
K e
Inside fiber o;EP .
1.153 0.880 0. 0168r 1.105 0.912 0.008Or 1. 054 0.951 0. 0021r
6
3 ONW ‘8 ‘V S3dVHS
03lOlllS SlNlOd JO NOllWOl ONV SllfMN03 A0 SNOISN3WlCl
SISAlVNV SS3US U313WYOd30 SO038 llnQN03 13clWle 319NIS
66Of 'I LZLS'Z ILIZ’b iad OIJV
JlLZf ‘0 JSS6b‘O Jf699’0 01 ‘6
JbSOZ’O JZbLf ‘0 JblbS’O II ‘0
3Nl-l 90 HION IlNlOd
JOLL61’2 JfbZSf.2 JCZCOS’I Z
I
3NI-l 10 HI
3 3dWS 8 3dVHS
+nOqO (O~!J(blUUI~S
OfbE. I 1 OOEO’E 1 OLIL’b (zJ)oW’
I I 1 1
SHAPE D
For length of lines for Points 6 thru 7 ond 9 thru 14, se6 Sha’pc 8.
Symmetrical about I+----..._ vertical centerline-m
Svmmctrical about L,_
A ---------- D --_--_-_ Lea +j+AJ+& “Centraidal oxis LA-+- ’ SHAPE E SHAPE F
I It=flt=5lt=fl A 0.33333r 0.33333~ 0.33333 r
D I. 50000r I.33333r I. l6667r
Area(#) 4.4635 2.7773 I. Z895
SINGLE BARREL CONDUIT BEGGS DEFORMETER STRESS ANALYSIS
DIMENSIONS OF CONDUITS AND LOCATION OF POINTS STUDIED
SHAPES 0, E, AND F
CIRCULAR
t=+ t-i t=+
Arto(r*) 3.9t70 2.4433 1.1345
SQUARE
t-f t=f t=f
Arco(r*) 5.0000 3.llII 1.4444
Symmetrical obout vertical centerline--za A+----- -%.
SHAPE G
SINGLE BARREL CONDUIT BEGGS DEFORMETER STRESS ANALYSIS
DIMENSIONS OF CONDUITS AND LOCATION OF POINTS STUDIED SHAPES CIRCULAR, SOUARE, AN! G
FIGURE 4
+ Sign convantion
SINGLE BARREL CONDUIT BEGGS DEFORMETER STRESS ANALYSIS
COEFFICIENTS FOR MOMENT, THRUST, AND SHEAR
UNIFORM VERTICAL. LOAD- UNIFORM FOUNDATION REACTION
SHAPES A, 8, AND C
X- PEL-372
FlGUPE 5
a
L 9 m
SINGLE BARREL CONDUIT BEGGS DEFORMETER STRESS ANALYSIS
COEFFICIENTS FOR MOMENT, THRUST, AND SHEAR
UNIFORM VERTICAL LOAD-TRIANGULAR FOUNDATION REACTION
SHAPES A, B, AND C
X-PEL-373
FIGURE 6
SINGLE BARREL CONDUIT BEGGS DEFORMETER STRESS ANALYSIS
COEFFICIENTS FOR MOMENT, THRUST, AND SHEAR
CONCENTRATE6i&CAL LOAD -UNIFORM FOUNDATION REACTION
SHAPES A, 6, AND C
X-PEL-374
~~~, to.536 to.716 t1.361 to.444 -to.632 tl.21 I
SINGLE BARREL CONDUIT BEGGS DEFORMETER STRESS ANALYSIS
COEFFICIENTS FOR MOMENT, THRUST, AND SHEAR
CONCENTRATED VERTICAL LOAD -TRIANOVLAR FOUNDATION REACTION
SHAPES A, 6, AND C
5EP 8.lDlO X-PEL - 375
SINGLE BARREL CONDUIT BEGGS DEFORMETER STRESS ANALYSIS
COEFFICIENTS FOR MOMENT, THRUST, AN0 SHEAR
TRIANGULAR VERTICAL LOAD - UNIFORM FOUNDATION REACTION
SHAPES A, 8, AND C
X-PEL- 1034
14
SINGLE BARREL CONDUIT BEGGS DEFORMETER STRESS ANALYSIS
COEFFICIENTS FOR MOMENT, THRUST, AND SHEAR
TRIANSULAR VERTICAL LOAD - TRIANGULAR FOUNDATION REACTION
SHAPES A, 8, AND C
SEP. 20, Is*4 X-PEL-IO35
15
NOTE’ g represents the vea*ht per unit volume of soil cover on the arch of the conduit sect,on I” un,+s consistent with those of the rod,us r
SINGLE BARREL CONDUIT BEGGS DEFORMETER STRESS ANALYSIS
: 03 COEFFICIENTS FOR MOMENT, THRUST, AND SHEAR U-F
VERTICAL ARCH LOAD - UNIFORM FOUNDATION REACTION
SHAPES A, B, AND C
SEP. 28. 1964 X-PEL-1036
16
FIQURE I I
t- -a(r+t) ‘.
Ia ..i
! 10
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 FOR MOMENT, THRUST, AND SHEAR VERTICAL ARCH LOAD-TRIANGULAR FOUNDATION REACTION
SHAPES A, 0, AND C
NOTES c represents the weight per unit volume of concrete or other motertal m units consistent wth Ihose of the radius r. See Figure I for net area of shapes
SINGLE BARREL CONDUIT BEGGS DEFORMETER STRESS ANALYSIS
COEFFICIENTS FOR MOMENT, THRUST, AND SHEAR
DEAD WEIGNT OF CONDUIT + Sign convmtion SHAPES A, B, AND C
X-PEL-1037
18
FIGURE 13
SINGLE BARREL CONDUIT BEGGS OEFORMETER STRESS ANALYSIS
COEFFICIENTS FOR MOMENT, THRUST, AND SHEAR UNIFORM HORIZONTAL LOAD - BOTH SIDES
SHAPES A, 8, AND C
t - r 6
SINGLE BARREL CONDUIT BEGGS DEFORMETER STRESS ANALYSIS
COEFFICIENTS FOR MOMENT, THRUST, AND SHEAR
TRIANGULAR HORIZONTAL LOAD - BOTH SIDES
SHAPES A, E, AND C
X-PEL-379
SINGLE BARREL CONDUIT BEGGS DEFORMETER STRESS ANALYSIS COEFFICIENTS FOR MOMENT, THRUST, AND SHEAR
UNIFORM INTERNAL RADIAL LOAD
SHAPES A, 8, AN0 C
21
Wessun ditiribution along vertical C of conduit -:
Wessure dlstnbution along vertical e ot conduit. --,
SINGLE BARREL CbNDUlT BWGS DEFORMETER STRESS ANALYSIS
COEFFICIENTS FOR MOMENT, THRUST, AND SHEAR
TRIANGULAR INTERNAL RADIAL LOAD - UNIFORM FOUNDATION REACTION
SHAPES A, 8, AND C
NOTE: w represents the wright par unit volume of woier in units consistent with those of the radius P.
+ Sign convention
Pressure distribution obrq vwticol C of conduit-..
POINT N T s H T s M T S
7 F
NOTE : I represents the weight par unit volume of water In units consiat*nt with those of the radius r.
SINGLE BARREL CONDUIT BEGGS DEFORMETER STRESS ANALYSIS
+ Sqn convention
COEFFICIENTS FOR MOMENT, THRUST, AND SHEAR
TRIANGULAR INTERNAL RADIAL LOAD - TRIANGULAR FOUNDATION REACTION
SHAPES A, 0, AND C
23
Deod weight of m one-half of conduit
Dead 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 assumed to develop at the foundotion. For the assumption that the conduits float see Figure 49.
SINGLE BARREL CONDUIT BEGGS DEFORMETER STRESS ANALYSIS
COEFFICIENTS FOR MOMENT, THRUST, AND SHEAR
TRIANGULAR EXTERNAL HYDROSTATIC LOAD INCLUDINQ DEAD LOAD
SHAPES A, 0, AND C
x- PEL- 1039 -.I
24
I .-1
ftttttfftttftttt?f?ful- ” -I
SEP ea. 1964
FISURE 19
SINGLE BARREL CONDUIT BEGGS DEFORMETER STRESS ANALYSIS
COEFFICIENTS FOR MOMENT, THRUST, AND SHEAR
UNIFORM VERTICAL LOAD - UNIFORM FOUNDATION REACTION
SHAPES D, E, AND F
x- PEL- 1040
25
SINGLE BARREL CONDUIT BEGGS DEFORMETER STRESS ANALYSIS
COEFFICIENTS FOR MOMENT, THRUST, AND SHEAR UNIFORM VERTICAL LOAD - TRIANGULAR FOUNDATION REACTION
SHAPES D, E, AND F
x- PEL- 104 I
26
FIGURE el
+ Sign convention
SINGLE BARREL CONDUIT BEGGS DEFORMETER STRESS ANALYSIS
COEFFICIENTS FOR MOMENT, THRUST, AND SHEAR CONCENTRATED VERTICAL LOAD - UNIFORM FOUNDATION REACTION
SHAPES D, E, AND F
X-PEL-1042
27
t=j t = 5
I 2vcr + t)
SINGLE BARREL CONDUIT BEGGS DEFORMETER STRESS ANALYSIS
COEFFICIENTS FOR MOMENT, THRUST, AND SHEAR
CONCENTRATED VERTICAL LOAD - + Sign conventlo”
TRIANGULAR FOUNDATION REACTION
SHAPES D, E, AND F
FIQURE 22
X-PEL- 1043
+ Sign convention
FIGURE 23
SINGLE BARREL CONDUIT BEGGS DEFORMETER STRESS ANALYSIS
COEFFICIENTS FOR MOMENT, THRUST, AND SHEAR
TRIANGULAR VERTICAL LOAD - UNIFORM FOUNDATION REACTION
SHAPES D, E, AND F
X-PEL-1044
29
SINGLE BARREL CONDUIT BEGGS DEFORMETER STRESS ANALYSIS
COEFFICIENTS FOR MOMENT, THRUST, AN0 SHEAR
TRIANGULAR VERTICAL LOAD - TRIANGULAR FOUNDATION REACTION
SHAPES D. E, AND F
X-PEL-1045
30
Note: No vertical arch lood on Shape D.
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.
+ Sign convention s
Y POINT 7
T S M -a
T S nrl
H T s
11
SINGLE BARREL CONDUIT BEGGS DEFORMETER STRESS ANALYSIS COEFFICIENTS FOR MOMENT, THRUST, AND SHEAR
VERTICAL ARCH LOAD - UNIFORM FOUNDATION REACTION
SHAPES 0. E, AN0 F
X-PEL-IO46
31
Note: No vertlcol arch load on Shape 0.
FIGURE 26
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
SINGLE BARREL CONDUIT BEGGS DEFORMETER STRESS ANALYSIS
i D COEFFICIENTS FOR MOMENT, THRUST, AND SHEAR
i VERTICAL ARCII LOAD-TRIANGULAR FOUNDATION REACTION
c SHAPES D, E, AND F
I + Sign convention
SEP. es. ,964 X-PEL-1047
32
NOTES’ c represents the ueiqht per unit volume of concrete or other moterod in units consistent wth those of the radius r. See Figure 2 for net orea ot shows.
SINGLE BARREL CONDUIT BEGGS DEFORMETER STRESS ANALYSIS
COEFFICIENTS FOR MOMENT, THRUST, AND SHEAR
+ Slqn convantion
DEAD WEIGHT OF CONDUIT
SHAPES D, E, AND F
SEP. 2% 1964 X -PEL-1048
33
-y h “- I
SINGLE BARREL CONDUIT BEGGS DEFORMETER STRESS ANALYSIS
COEFFICIENTS FOR MOMENT, THRUST, AND SHEAR
UNIFORM HORIZONTAL LOAD - BOTH SIDES
SHAPES D, E, AND F
X-PEL- 1049
34
SINGLE BARREL CONDUIT BEGGS DEFORMETER STRESS ANALYSIS
COEFFICIENTS FOR MOMENT, THRUST, AND SHEAR TRIANGULAR IfORltONTAL LOAD - BOTH SIOES
SHAPES 0, E, AND F
X-PEL- 1010
35
t Sign Convention
FIGURE 30
SINGLE BARREL CONDUIT BEGGS DEFORMETER STRESS ANALYSIS
COEFFICIENTS FOR MOMENT, THRUST, AND SHEAR
UNIFORM INTERNAL RADIAL LOAD
SHAPES D, E, AND F
X-PEL- 1051
36
FIGURE 31
Pressure distribution along vertical k of conduit-.:
Pressure dirtributlon along vertical C of conduit--%.
NOTE: u represents the weight par unit volumr of voter in units consistent with those of the radius r.
+ Sign convention
SINGLE BARREL CONDUIT BEGGS DEFORMETER STRESS ANALYSIS
COEFFICIENTS FOR MOMENT, THRUST, AND SHEAR
TRIANGULAR INTERNAL RADIAL LOAD - UNIFORM FOUNDATION REACTION
SHAPES D, E. AND F
X-PEL-IO52
37
t = i t = f t=f Pressure distribution olonp
vertical t of oonduit..
Pressure dishlbution olonp vertical C of Conduit-.,
Pressure distribution along VWtiCOI 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 R)R MOMENT, THRUST, AND SHEAR
TRIANOULAR INmNAL RADIAL LOAD - TRIANGULAR FOUNDATION REACTION
SHAPES D, E, AND F
FIGURE 39
x-PEL-IO63
38
FIQIJRE 33
Dead Y on5-half
t-f,
t-i,
t-i.
‘ei ht of o conduit P
D5ad wight af one-halt of mndult
t-:* 5.SeIwr*
.t -f* 5.55. wr’
t = f. I.55OW’
D5od r5Wt of one-hall 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 develop at the foundation. For the olsumption that the conduits float see Figure 49.
SINGLE 1
ARREL CONDUIT BEGGS DEFORM TER STRESS ANALYSIS
COEFFICIENTS FOR MOMENT, THRUST, AND SHEAR
TRIANGULAR EXTERNAL HYDROSTATIC LOAD INCLUDINQ DEAD LOAD
SHAPES D, E, AND F
39
utttttrtltrltttttttt11 L --f
SINGLE BARREL CONDUIT BEGGS DEFORMETER STRESS ANALYSIS
CQEFFICIENTS FOR MOMENT, THRUST, AND SHEAR
UNIFORM VERTICAL LOAD - UNIFORM FOUNDATION REACTION + Sign convention
SHAPES CIRCULAR, SGUARE, AND G
X-PEL-I055
SINGLE BARREL CONDUIT BEGGS DEFORMETER STRESS ANALYSIS
COEFFICIENTS FOR MOMENT, THRUST, AN0 SHEAR
UNIFORM VERTICAL LOAD - TRIANGULAR FOUNDATION REACTION
SHAPES CIRCULAR, SQUARE, AND G
X-PEL-1056
41
FIGURE 36
SINGLE BARREL CONDUIT BEGGS DEFORMETER STRESS ANALYSIS
COEFFICIENTS FOR MOMENT, THRUST, AND SHEAR
CONCENTRATED VERTICAL LOAD - UNIFORM FOUNDATION REACTION
SHAPES CIRCULAR, SPUARE, AND 0
X-PEL- 1057
42
: a -
2
(I w a. - a is
7 --r-- ,
lLzziJ
f i
t ___ --- -‘-
L- I (( _ , ‘I: i
SINGLE BARREL CONDUIT BEGGS DEFORMETER STRESS ANALYSIS
COEFFICIENTS FOR MOMENT, THRUST, AND SHEAR
CONCENTRATED VERTICAL LOAD - TRIANOULAR FOUNDATION REACTION
SHAPES CIRCULAR, SQUARE, AND 0
X-PLL- 1058
43
SINGLE BARREL CONDUIT BEGGS DEFORMETER STRESS ANALYSIS
+ Sign convention
COEFFICIENTS FOR MOMENT, THRUST, AND SHEAR
TRIANGULAR VERTICAL LOAD - UNIFORM FOUNDATION REACTION
SHAPES CIRCULAR, SQUARE, AND 0
SEP. ee, 1964 X-PEL-IO59
FIGURE 39
SINGLE BARREL CONDUIT BEGGS DEFORMETER STRESS ANALYSIS
COEFFICIENTS FOR MOMENT, THRUST, AND SHEAR
TRIANGULAR VERTICAL LOAD - TRIANGULAR FOUNDATION REACTION
SHAPES CIRCULAR, SQUARE, AND G
X-PEL-1060
45
t-f t-L 3
t-S- 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.
FIQURE 40
SINGLE BARREL CONDUIT BEGGS DEFORMETER STRESS ANALYSIS
COEFFICIENTS FOR MOMENT, THRUST, AN0 SHEAR
VERTICAL ARCH LOAQ - UNIFORM FOUNDATION REACTION
SHAPES CIRCULAR, SQUARE. AND 6
SEP. Le. 1964 X-PEL-IO61
46
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 FOR MOMENT, THRUST, AND SHEAR
VERTICAL ARCH LOAD - TRIANDULAR FOUNDATION REACTION
SHAPES CIRCULAR, SQUARE, AND B
X-PEL-106R
47
FIQURE 42
NOTES: c represents the weight per unit VOlumC of concrete or other motwial in units consirtant with those ot the radius r. See FIgwe 3 for net or.x of sh.,,xs.
+ Sign conwntion
SEP. PI. I,d.
SINGLE BARREL CONDUIT BEGGS DEFORMETER STRESS ANALYSIS
COEFFICIENTS FOR MOMENT, THRUST, AND SHEAR
DEAD WElSHf OF CONDUIT
SHAPES CIRCULAR, SQUARE, AND 0
X-PEL-1063
4-a
-1 h p- -1 h p-
-04 h b- * -4 h )r-
SINGLE BARREL CONDUIT BEGGS DEFORMETER STRESS ANALYSIS
COEFFICIENTS FOR MOMENT, THRUST, AN0 SHEAR
UNIFORM HORIZONTAL LOAO - BOTH SIDES
SHAPES CIRCULAR, SQUARE, AND 0
x- PEL- IO64
49
FIQURE 44
SINGLE BARREL CONDUIT BEGGS DEFORMETER STRESS ANALYSIS
COEFFICIENTS FOR MOMENT, THRUST, AND SHEAR
TRIANQULAR HORIZONTAL LOAD - BOTH SIDES
SHAPES CIRCULAR, SQUARE, AND 0
50
I 0 I-t
, - ,.. I) 1 0 I-I
FIQURL -- 45
D SINGLE BARREL CONDUIT BEGGS DEFDRMETER STRESS ANALYSIS
COEFFICIENTS FOR MOMENT, THRUST, AND SHEAR
UNIFORM INTERNAL RADIAL LOAD + Sign convention
SHAPES CIRCULAR. SQUARE, AN0 Q
X-PLL- 1055
51
Prrrrum distribution along vertical e of conduit-.,
Pressure distribution along vertical 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
I BEGGS DEFORMETER STRESS ANALYSIS
m- COEFFlClENfS FOR MOMENT, THRUST, AND SHEAR
L TRIANGULAR INTERNAL RADIAL LOAD - UNIFORM FOUNDATION REACTION
q + Sqn convention SliAPES CIRCULAR, SOUARE, AND G
> r
SEP. er, 1964 X-PEL-1067
52
FIQURE 47
Pressure distribution along
Pressure distribution along vertical C of conduit-.,
Pressure distribution along vertlcol c of conduit-..
NOTE: w repmsante the weight per unit volume of rater in units conristrnt with those of the rodtur r.
SINGLE BARREL CONDUIT BEGGS DEFORMETER STRESS ANALYSIS
COEFFICIENTS FOR MOMENT, THRUST, AND SHEAR
TRIANGULAR INTERNAL RADIAL LOAD - TRIANGULAR FOUNDATION REACTION + Sinp convmtion
SHAPES CIRCULAR, SQUARE, AND G
SEP. er, 1004 X - PEL-IO68
53
hod wai ht of one-holf f COIldUll
D*Od wqht of one-half of conduit
t-f, 6.010 wr’ t - 5, 5.7.0 wr’
t-f, 1.75* wr’
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 FOR MOMENT, THRUST, AND SHEAR
TRIANWLAR EXTERNAL HYDROSTATIC LOAD INCLUDING DEAD LOAD
SHAPES CIRCULAR, SOUARE, AND Q
X-PEL-1069
54
SHAPE A M
POINT 7 T S
wr’
SHAPE E
CIRCULAR SOUARE
SHAPE 0
SUAPE F
SHAPE C
-1
SHAPE G
Top rtoction is ossumed of uniform intensity, v.
to be
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, AN0 SHEAR TAIANQULAR EXTERNAL HYDAOSTAtlO LOAD
INCLUDINS DEAD LOAD
CONDUITS ASSUMED TO FLOAT
ALL SHAPES
,EP. em, 1944
t- i
x- PEL- 1070
.
1-1 ~~ r -0.218 I +0.5301 0 II -0. IB3 I to.471 I 6 ~l--o.t 50 I z.412 r- a L I 1 II I I I, - - --I -...-I -
2 -0.196 to.512 -0.137 1 -0.164 1 to.455 1 -0.122 -0.135 I +0.39q -0.107
-0.265 11 -0.109 1 to.4061 -0.236 ll -0.090
-0.238 1
8 1 +0.2l I to.082 to.306 t 0. I79 to.073 to.272 to.149
9 II- ~t0.103~t0.242~t0.420~i+0.065~t0.215~+0.373 +0.069 1 IO I-0.024itO.3751
I II I-0.130 l+o.459 I + 0.357 H + 0.398
to.412
I2 -0.196 to.512
I3 I-O.218 I +0.530
t Sign convention
SINGLE BARREL CONDUIT BEGGS DEFORMETER STRESS ANALYSIS COEFFICIENTS FOR MOMENT, THRUST, AN0 SHEAR
HORIZONTAL PASSIVE PRESSURE
CIRCULAR SHAPE
56
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 dis- placement 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 meas- ured 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 dis- placements applied at the gage block. The dif- ference 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 equa- tions may be written for the redundant reactions at the cut section:
For a concentrated load
-.
For a distributed load
M,=PFn M
MI=: pe,dl M s
.
4 Beggs, G. E., “An Accurate Solution of Statically In- determinate 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. 282-
6 ‘Phillips, H. B., and Allen, I. E., “The Beggs De- formeter Theory and Technique,” Bureau of Reclamation, Denver, Colo., July 1965.
SFPF Sl=$ s
pes dl S S
TI==PF T
Tl= $spe, dl T
where
d, is the angular rotation applied at the cut by the moment plugs
ds is the displacement applied at the cut by the shear plugs
dT is the displacement applied at the cut by the thrust plugs
eM is the measured deflection at a load point, in the direction of the load, due to d,
es is the measured deflection at a load point, in the direction of the load, due to ds
eT is the measured deflection at a load point, in the direction of the load, due to dT
I is the load length MI is the redundant moment reaction at the
cut n is the scale factor (prototype to model) P is a load acting at a point on the prototype p is the load intensity on the prototype at
the deflection point $ is the redundant shear reaction at the cut T1 is the redundant thrust reaction at the
cut.
The 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 calibra- tion 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 De- formeter 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.
58GPO 850-512
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37 Hydraulic Model Studies for Morrow Point Dam
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10 Annual Report of Progress on Engineering Research-l 966
11 Pile Supported Structures in Lake Deposits
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