40
Tables of Stresses in Three-Layer Elastic Systems A. JONES, "Shell" Research Ltd., Thornton Research Centre, Chester, England The tables of values of stresses arising in a three-layer elastic system loaded over a circular area, published by Acum and Fox, have been extended to cover a wider range of parameters. Values of the vertical stresses at both interfaces are given, and are accurate to within 1 percent. The calculations were performed on the Ferranti Mark I * computer at Koninklijke/Shell Laboratorium, Amsterdam. The work forms part of a program for the development of a method for the design of flexible roads. •IN GENERAL, road design involves the determination of the thicknesses and elastici- ties of the various layers in the road structure to insure that the stresses and strains developed are within permissible limits. The present analysis assumes that the design is based on a knowledge of the stresses at the interfaces between the layers on the axis of symmetry below a circular loaded area. The first analysis to take into account the different elastic properties of the various layers was given by Burmister {1) in 1943. In a series of subsequent papers (2) he derived expressions for the stresses and displacement in two- and three-layer systems. However, he did not publish any stress values and only a small number of values of the surface deflection at the centre of the loaded area for a two-layer system. Fox (3) pro- duced extensive tables of stresses in two-layer systems in 1948, and in 1951 Acum and Fox (4) produced tables for the normal and radial stresses in three-layer systems at the intersections of the axis of symmetry with the interfaces. The tables in this paper form an extension, to a much wider range of the parameters, of those of Acum and Fox. (Stress and displacement values for one given system were published by Schiffman (5) in 1957). The road system considered in this paper consists of three layers, as in Figure 1. The stresses that have been computed are listed in Table 1, where the numerical sub- scripts refer to the layer. Throughout the tables it is assumed that Poisson's ratio is equal to 0. 5 and that there is full friction at the interfaces. For convenience, the stresses are printed on the assumption that compression stress is positive. Values of these stresses are given In Appendix A for all combinations of the following parameter values: E1/E2 = ki = 0.2, 2.0, 20.0, 200.0 E2/E3 = k2 = 0.2, 2.0, 20.0, 200.0 a/h2 = ai = 0.1, 0.2, 0.4, 0.8, 1.6, 3.2 hi/h2 = H = 0.125, 0.25, 0.5, 1.0, 2.0, 4.0, 8.0 Each stress value is expressed as a fraction of the applied load. Stresses for all values of ai appear in a block and the blocks are arranged in groups of four in ascending order of kz; these groups are arranged in order of ki and finally in sets in order of H. The calculations were performed on the Ferranti Mark 1» computer at Koninklijke/ Shell Laboratorium, Amsterdam. The machine program was written to calculate 36 stress values at the same time; viz., 6 stresses for each of 6 values of ai. The infinite range of integration (see Appendix B) was tnmcated at such a point that the contribution from the omitted portion was negligible. The finite part of the range was then split into a number of equal intervals and the integrals were then evaluated over each interval 176

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Page 1: Tables of Stresses in Three-Layer Elastic Systemsonlinepubs.trb.org/Onlinepubs/hrbbulletin/342/342-008.pdf · with some notes on the assumptions involved in setting up the problem

Tables of Stresses in Three-Layer Elastic Systems A. JONES, "Shell" Research Ltd. , Thornton Research Centre, Chester, England

The tables of values of stresses arising in a three-layer elastic system loaded over a circular area, published by Acum and Fox, have been extended to cover a wider range of parameters. Values of the vertical stresses at both interfaces are given, and are accurate to within 1 percent. The calculations were performed on the Ferranti Mark I * computer at Koninklijke/Shell Laboratorium, Amsterdam.

The work forms part of a program for the development of a method for the design of flexible roads.

•IN GENERAL, road design involves the determination of the thicknesses and elastici­ties of the various layers in the road structure to insure that the stresses and strains developed are within permissible limits. The present analysis assumes that the design is based on a knowledge of the stresses at the interfaces between the layers on the axis of symmetry below a circular loaded area.

The first analysis to take into account the different elastic properties of the various layers was given by Burmister {1) in 1943. In a series of subsequent papers (2) he derived expressions for the stresses and displacement in two- and three-layer systems. However, he did not publish any stress values and only a small number of values of the surface deflection at the centre of the loaded area for a two-layer system. Fox (3) pro­duced extensive tables of stresses in two-layer systems in 1948, and in 1951 Acum and Fox (4) produced tables for the normal and radial stresses in three-layer systems at the intersections of the axis of symmetry with the interfaces. The tables in this paper form an extension, to a much wider range of the parameters, of those of Acum and Fox. (Stress and displacement values for one given system were published by Schiffman (5) in 1957).

The road system considered in this paper consists of three layers, as in Figure 1. The stresses that have been computed are listed in Table 1, where the numerical sub­scripts refer to the layer.

Throughout the tables i t is assumed that Poisson's ratio is equal to 0. 5 and that there is ful l friction at the interfaces. For convenience, the stresses are printed on the assumption that compression stress is positive.

Values of these stresses are given In Appendix A for all combinations of the following parameter values:

E 1 / E 2 = k i = 0.2, 2.0, 20.0, 200.0 E 2 / E 3 = k2 = 0.2, 2.0, 20.0, 200.0 a/h2 = ai = 0.1, 0.2, 0.4, 0.8, 1.6, 3.2 hi/h2 = H = 0.125, 0.25, 0.5, 1.0, 2.0, 4.0, 8.0

Each stress value is expressed as a fraction of the applied load. Stresses for all values of ai appear in a block and the blocks are arranged in groups of four in ascending order of kz; these groups are arranged in order of k i and finally in sets in order of H.

The calculations were performed on the Ferranti Mark 1» computer at Koninklijke/ Shell Laboratorium, Amsterdam. The machine program was written to calculate 36 stress values at the same time; viz. , 6 stresses for each of 6 values of ai. The infinite range of integration (see Appendix B) was tnmcated at such a point that the contribution from the omitted portion was negligible. The finite part of the range was then split into a number of equal intervals and the integrals were then evaluated over each interval

176

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177

CIRCULAR LOADED AREA pi^gg

M i l l s"' ^^ h | LAYER I

LAYER 2

LAYER 3

Infinite

-2a- MODULUS OF ELASTICITY = E,

INTERFACE I

MODULUS OF ELASTICITY = E2

INTERFACE 2

MODULUS OF ELASTICITY = E j

I I t

AXIS OF SYMMETRY

Figure 1. Structure of layered system.

TABLE 1 NOTATION FOR STRESSES GIVEN IN APPENDIX A

Stress First Interface

Second Interfece

Vertical Vertical and radial (upper layer) Vertical and radial (lower layer)

Z i

Z i - a_ r i

Z i rz

za °„ ' Za Tz

Z2 r s

separately using a Gauss quadrature formula. Some difficulty was encountered near the origin due to the fact that the integrand had an essential singularity on the negative real axis, this was overcome by subdividing the first interval.

The following checks (which are perfect apart from a constant factor) were built into the computer program.

Z i r i k i (a, Z i (T ) (first interface) rz

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178

*^Z2 ~ ~ ^^Zz " * rs (second interface)

In most cases the two sides of these equations agreed to five significant digits but where this was not so the disagreement was stil l less than 1 percent. Al l numbers in the tables, however, are correct only to within one digit in the last decimal place printed.

As a further check some results were obtained for comparison with those of Acum and Fox. These are presented in Appendix C with the corresponding values from Acum and Fox's paper in brackets.

A typographical error was found in the published solution of Acum and Fox and was corrected before the tables were calculated.

A brief mathematical description of the problem is given in Appendix B, together with some notes on the assumptions involved in setting up the problem and the correct expressions for the stresses.

ACKNOWLEDGMENTS The author wishes to record his gratitude for the assistance given by his colleagues

in the production of the tables. He also wishes to thank the Management of Koninklijke/ Shell Laboratorium for the use of the computer, and the Directors of "Shell" Research Limited for permission to publish this paper.

REFERENCES 1. Burmister, D. M . , "The Theory of Stresses and Displacements in Layer Systems

and Applications to Design of Airport Runways." HRB Proc., 23: 126-149 (1943). Discussion, pp. 144-148.

2. Burmister, D. M . , "The General Theory of Stresses and Displacements in Layered Systems." J. Appl. Phys., 16: No. 2, pp. 89-96; No. 3, pp. 126-127; No. 5, pp. 296-302 (1945).

3. Fox, L . , "Computation of Traffic Stresses in a Simple Road Structure." Depart­ment of Scientific and Industrial Research, Road Res. Tech. Paper 9 (1948).

4. Acum, W. E. A . , and Fox, L . , "Computation of Load Stresses in a Three-Layer Elastic System." Geotechnique, 2: 293-300 (1951).

5. Schiffman, R. L . , Proc. 4th Internat. Conf. on Soil Mechanics and Foundation Engineering, London (1957).

6. Sneddon, I . N . , "Fourier Transforms." McGraw-Hill (1951).

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179

Appendix A

H o 0.125

k, > 0.2

a- 0- 0"- -0*- O" "XT • i •« T^ •1 r «a at rs

k, a 0.2 O. I o * 6 6 O 4 5 0 . 1 2 4 3 8 0 . 6 2 X 3 8 0 . 0 1 5 5 7 0 . 0 0 3 3 2 0.0x659 0* a 0 . 9 0 2 4 9 0 . 1 3 5 4 6 0 . 6 7 7 2 8 0 . 0 6 0 2 7 0 . 0 1 2 7 8 0.0639X 0* 4 0 . 9 5 2 9 5 o » 1 0 4 2 8 0 . 5 2 1 4 1 0 . 2 1 2 8 2 0 . 0 4 4 3 0 0 . 2 2 X 5 0 o.B 0 . 9 9 5 2 0 0.090ZI 0 . 4 5 0 5 3 0.56395 0.10975 0.54877 Z . 6 I . 0 0 0 6 4 0 . 0 8 7 7 7 0 . 4 3 8 8 4 0 . 8 6 2 5 3 » • 1 3 7 5 5 0 . 6 8 7 7 7 3 . 8 0 . 9 9 9 7 0 0 * 0 4 1 2 9 0 . 2 0 6 4 3 0.94143 0 . I O I 4 7 0.50736

2.0

O. X 0 . 6 6 0 4 8 0 . 1 2 2 8 5 0 . 6 X 4 2 4 0 . 0 0 8 9 2 0 . 0 1 6 9 3 0 . oo9 46 0 . 2 0 . 9 0 X 57 0 . 1 2 9 1 6 0 . 6 4 5 8 2 0 . 0 3 4 8 0 0 . 0 6 5 5 8 0 . 0 3 2 7 9 0 . 4 0 . 9 5 1 2 0 0 . 08 i 15 0 . 4 0 5 7 6 0 . X 2 6 5 6 0 . 2 3 2 5 7 0 . 1 1 6 2 9 0 . 8 0 . 9 9 2 3 5 0 . 0 X 8 2 3 0 . 0 9 X X 3 0 . 3 7 3 0 7 0 . 6 2 8 6 3 0 . 3 1 4 3 2 1 . 6 0 . 9 9 9 X 8 - o» 0 4 X 3 6 - 0 . 2 0 6 8 0 0 . 7 4 0 3 3 0 . 9 8 7 5 4 0 . 4 9 3 7 7 3 . 3 I . 0 0 0 3 2 - 0 . 0 3 8 0 4 - 0 . X 9 0 7 5 0 . 9 7 x 3 7 0 . 8 2 X 0 2 0 . 4 1 0 5 X

20.0

0 . I 0 . 6 6 2 3 5 0 . 1 2 0 3 2 0 . 6 0 1 6 I 0 . 0 0 2 5 6 0 . 0 3 6 6 7 0 . ooi3 3 O . 2 0 . 9 0 4 X 5 0 . X 1 7 8 7 0 . 5 8 9 3 3 0 . OIOX I 0 . 1 4 3 3 6 0 . 0 0 7 17 0 . 4 0 . 9 5 1 3 5 0 . 0 3 4 7 4 0 . X 7 3 7 0 0 . 0 3 8 3 8 0 . 5 2 6 9 1 0 . 0 2 6 3 5 0 . 8 o . 9 8 7 7 8 - 0 . X4872 - 0 . 7 4 3 5 8 0 . 1 3 0 4 9 X . 6 X 7 2 7 0 . o3o36 X . 6 0 . 9 9 4 0 7 -• 0 . 5 0 5 3 3 - 2 . 5 2 6 5 0 0 . 3 6 4 4 2 3 ' 589- 'r4 0 . 179'J7 3 . 3 O . 9 0 8 2X - 0 . 8 0 9 9 0 - 4 . 0 5 0 2 3 0 . 7 6 6 6 9 5' 1 5 4 0 9 0 . 2 5 7 7 0

200.0

0 . X 0 . 6 6 2 6 6 0 . X X720 0 . 5 8 5 9 9 0 . 0 0 0 5 7 0 . 0 5 4 X 3 0 . 0 0 0 2 7 0 . 2 0 . 9 0 3 7 0 o. 1 0 4 9 5 0 . 5 2 4 7 7 0 . 0 0 2 2 6 0 . 2 1 3 1 4 0 . 0 0 1 0 7 0 . 4 0 . 9 4 7 1 9 - 0 . 0 1 7 0 9 - 0 . 0 8 5 4 3 0.oo83 I 0 . 8 0 4 0 0 0 . 0 0 4 0 2 0 . 8 0 . 9 9 X 0 5 - 0 . 3 4 4 2 7 - 1 . 7 2 1 3 4 0 . 0 3 2 5 9 2 . 6 7 9 3 4 0 . 0 X 3 4 0 Z . 6 0 . 9 9 X 4 6 - X . 2 X X29 - 6 . 0 5 6 4 3 0 . X X034 7 . 3 5 9 7 8 0 . 0 3 6 8 0 3 . 3 0 . 9 9 3 3 2 - 2 . 8 9 2 8 2 - I 4 . 4 6 408 0 . 3 2 6 5 9 1 6 . 2 2 8 3 0 0 . 08 1X4

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180

H 0.125

2.0

o. I O. 3 o. 4 0 . 8 1.6 3 '3

o .43055 o. 78688 o. 98760 I . 0 1 0 2 8 I . 0 0 6 4 7 O.993 22

O.71614 I . O I 5 6 1 0 .83924 0 .63961 0 .65723 o.38 165

o .35807 o.507O0 o .41962 o.31981 o .32862 o .10093

2a

0 . 0 1 6 8 2 0. 06 5 11 o .33005 0 .60886 o. 90959 o .94322

B i ra

o .00350 o.01348 o .04669 o .11484 o.13726 o. 09467

ka o 0.2 o .01750 o.06741 0. 23346 0 . 5 7 ' r l 3 0 .636 30 0 . 4 7 3 3 5

2.0

0.1 0 . 4 2 9 5 0 0 .706 22 0 . 35303 0. 00896 0 .01716 0 . 00858 0* 2 0 .78 424 0 .97956 0 . 4393Q 0. 03493 0 .066 47 0 . 03324 0 . 4 0 .98044 0 .70970 0. 35483 0 . 13667 0 .23531 0. 11766 0 . 3 0 . 9 9 4 3 4 0 .22319 0. 1116 4 0 . 36932 0 .63003 0 . 31501 1.6 0 .99364 - o .19983 -" 0 . 09995 0 . 72113 0 .97707 0. 48853 3 . 2 0 .99922 - 0 .28916 - 0 . 14461 0. 96148 0 .8 4030 0 . 42015

20.0

0. I 0. 43022 0 .69333 0. 34662 0 . 0 0 2 2B 0. 03467 0 . 0017 3 0. 2 o. 78414 0 .92o36 0. 46048 0 . 0 0 8 9 9 0 . 13541 0 .00677 0 . 4 0. 97493 0. 46 58 3 0 . 23297 0 .03392 0 . 49523

496 13 0 .02476

0 .8 0 . 97806 - 0 .66535 - 0 . 33270 0 . 1 1 3 5 0 1. 49523 496 13 0 .07481

1.6 0 . 9692 1 - 3 . 8 3 8 5 9 - 1. 41430 0 . 3 1 2 6 3 3« 28512 0 .16 426 3« 2 0 . 98591 *- 5 .27906 - 2 . 63954 0 . 6 8 4 3 3 5» 05953 0 . 35298

200.0

0.1 0 . 4 2 0 3 5 0 .67488 0 .33744 0. 00046 0 .048 43 0 .00024 0. 2 0 .78 367 0 .85397 0 .42698 0 . 00183 0. 19043 0 . 0 0 0 9 5 0 . 4 0 . 9 7 3 6 9 0 . 2 1 1 6 5 0 .10582 0 . 00711 0. 71221 0 .003 56 0 . 8 0 . 9 7 2 9 5 - i » 6 5 9 5 4 — 0 .82977 o. 02597 2 . 32652 0 .01163 1.6 0 .95546 - 6 . 4 7 7 0 7 - 3 » 2 3 8 5 5 0 . 08700 6 . 26638 0 .03133 3 » 2 0 .96377 - 1 6 . 6 7 3 7 6 - 8 ,33691 o. 26292 14. 25621 0 .07128

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181

H 0.125

20.0

«« 8< r a S t S i rj k « a 0.2

o . I 0. 146 48 1 .80805 0 .09040 0 . 0 1 6 4 5 0 .00322 0 .01611 O. 2 o» 39260 3 '7S440 0 .18772 0 . 06 407 0 .01249 0 . 0 6 2 4 4 o . 4 0 .80302 5 .11847 0 .25592 0 . 2 3 1 3 5 0 .04421 o . 2 2 1 0 5 0 . 8 I . 0 6 5 9 4 3 .38600 0 .16930 0 .64741 0 . I 1 4 6 8 0 . 5 7 3 4 2 1.6 I . 0 2 9 4 2 I . 3 1 6 0 3 0 .09080 1 .00911 0 .13687 0 .68436 3 » 3 0 .99817 I . 7 5 1 0 1 0 .08756 0 .97317 0 .07578 0 . 3 7 8 9 0

2.0

0. X 0. 14529 1.81178 0. 09059 18344

o . 0 0 8 1 0 0 .01542 o . 00771 0. 2 0 . 38799 3 .76886 0 .

09059 18344 0 . 0 3 1 7 0 0 .06003 0 . 03002

0. 4 0 . 78651 5 .16717 0 . 25836 0 .116 50 0 . 2 1 6 4 0 0 .60493

0 . 10820 0 .8 t . 032 18 3» 43631 0 . 17182 0 .34941

0 . 2 1 6 4 0 0 .60493 0 . 30247

1.6 0. 99060 I . 1 5 2 1 1 0 . 05701 0 . 6 9 0 1 4 0 . 9 3 4 8 7

0 .97146 0 . 48573 3 . 2 0 . 99393 - 0 .068 94 - 0 . 00345

0 . 6 9 0 1 4 0 . 9 3 4 8 7 0 .88358 0 . 44179

ka - 20.0

0 .1 0 . 14447 1. 8 06 6 4 0 . 09033 0 .00182 0 .02985 0 . 0 0 1 4 9 0 . 2 0 . 38469 3*74573 0. 18729 0 .00716 0 .X1697 0 . 0 0 5 8 5 0 . 4 0. 77394 5 . 0 5 4 8 9 0 . 25274 0 . 0 2 7 1 0 0 .43263 0 .0216 3 0. 8 0 . 986 10 2 .92533 0 . 14627 0 .09061 1.33736 0 . 0 6 6 8 7 1.6 0 . 93712 - 1 .27093 - 0 . 06355 o . 2 4 5 2 8 2 .99215 o . 1 4 9 6 1 3 « 2 0 . 96330 - 7 .35384 - 0 . 36761 0 . 5 5 4 9 0 5 .06489 0 . 2 5 3 2 4

k« - 200.0

0. I 0. 1 44 22 1.78941 0 .08947 0 . 00033 0 . 0 4 0 1 0 0 . 0 0 0 2 0 0 . 2 0 . 38388 3 .68097 0 . 1 8 4 0 5 0. 00131 0 .15781 o . 0 0 0 7 9 0. 4 0 . 77131 4 .80711 0 .24036 0 . 00505 0 .59391 0 .00297 o . 3 0. 97701 I . 9 0 8 2 5 0 .09541 0 . 01830 I . 0 5 7 0 9 o . 0 0 9 7 9 1. 6 0. 91645 - 5 .28803 - 0 . 2 6 4 4 0 0 . 06007 5 . 2 5 H O 0 .02626 3 . 2 o . 9266 2 - 2 1 . 5 2 5 4 6 - 1 .07627 0. 18395 12 ,45058 0 . 0 6 2 2 5

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182

2l

H = 0.125

k , B 200.0

8a r j k , a 0.2

0 . I 0 . 0 3 6 9 4 2 . 8 7 5 6 4 4 4 2 8 5

0 . 0 1 4 3 8 o . 0 1 1 3 7 0 . 0 0 2 0 1 0 . 0 1 0 0 5 0 . 2 0 . 1 2 3 2 7 7«

8 7 5 6 4 4 4 2 8 5 0 . 0 3 7 2 1 0* 0 4 4 7 3 0 . 0 0 7 8 8 0 . 0 3 9 4 0

0 . 4 o . 3 6 3 2 9 1 5 . 4 I 0 3 I 0 . 0 7 7 0 5 0 . 1 6 7 8 5 0 . 0 2 9 1 3 0 . 1 4 5 6 6 0 . 8 0 . 8 2 0 5 0 1 9 . 7 0 2 6 1 0 . 0 9 8 5 1 o« 5 3 1 4 4 0 . 0871,', 0 . 4 3 5 6 8 1 . 6 1 . 1 2 4 4 0 7» 0 2 3 8 0 0 . 0 3 5 1 2 1 . 0 3 7 0 7 0 . 1 3 7 0 5 0 . 6 8 5 2 4 3 . 3 0 . 9 9 5 0 6 2 . 3 5 4 5 9 0 . 0 1 1 7 7 I . 0 0 4 0 0 0 . 0 6 5 9 4 0 . 3 2 9 7 I

k « 2.0

0 . 1 0 . 0 3 4 8 1 3 . 0 2 2 5 9 0 . 0 I 5 I I 0 . 0 0 5 4 0 0 . 0 0 9 6 9 0 . 0 0 4 8 5 0 . 2 0 . 1 1 4 9 1 3 , 0 2 4 5 2 0 . 0 4 0 1 2 0 . 0 2 1 6 7 0 . 03G I 2 0 . 0 1 9 0 6 0 . 4 o . 3 3 3 1 8 1 7 . 6 4 1 7 5 0 . 0 8 8 2 1 0 . 0 8 2 29 0 . 1 4 2 8 6 0 . 0 7 1 4 3 0 . 8 0 . 7 2 6 9 5 2 7 . 2 7 7 0 1 0 . 1 3 6 3 9 0 . 2 7 3 0 7 0 . 4 5 3 0 8 0 . 326 0 4 1 . 6 1 . 0 0 2 0 3 2 3 . 3 8 6 3 3 o. 1 1 6 9 3 • 0 . 6 3 9 1 6 o . 9o36 1 0 . 4 5 4 3 0 3 . 3 I . 0 0 8 28 1 1 . 8 7 0 1 4 0 . 0 5 9 3 5 0 . 9 2 5 6 0 0 . 9 1 4 6 9 0 . 4 5 7 3 5

k a = 20.0

0 . 1 o . 0 3 3 3 6 3 . 1 7 7 6 3 o . 0 1 5 8 9 0 . 0 0 1 23 0 . 0 1 9 8 0 0 . 0 0 0 9 9 0 . 2 0 . 1 0 9 2 8 8 , 6 6 0 9 7 0 . 0 4 3 3 0 0 . 0 0 5 0 9 0 . 0 7 8 2 7 0 . 0 0 3 9 1 o . 4 0 . 3 1 0 9 4 2 0 . 1 2 2 5 9 0 . 1006 I 0 . 0 1 9 7 2 0 . 2 9 8 8 7 0 . 0 1 4 9 4 0 . 8 0 . 6 5 9 3 4 3 6 . 2 9 9 4 3 0 . 1 8 1 5 0 0 . 0 7 0 4 5 1 . 0 r 6 9.« 0 . 0 5 0 8 5 1 . 6 o . 8 7 9 3 1 4 9 . 4 0 8 5 7 0 . 2 4 7 0 4 0 . 2 0 9 6 3 2 . 6 4 3 1 3 0 . 1 3 3 16 3 . 2 0 . 9 3 3 0 9 5 7 . 8 4 3 6 9 o . 28 02 3 0 . 4 9 9 3 3 4 . 8 9 8 9 5 0 . 3 4 4 9 5

200.0

0 . 1 0 . 0 3 3 0 7 3 . 2 6 9 8 7 0 . 0 1 6 3 5 0 . 0 0 0 2 5 o . 0 2 8 0 9 0 . 0 0 0 1 4 O . 2 0 . 1 0 8 1 0 9* 0 2 6 6 9 0 . 0 1513 o . 0 0 0 9 8 o . 1 1 1 3 6 0 . 0 0 0 5 6 0 . 4 0 . 3 0 6 3 9 2 1 . 5 6 4 8 2 0 . 1 0 7 8 2 0 . 0 0 3 8 6 0 . 4 3 0 3 5 0* 0 0 2 15 0 . 3 0 . 6 4 3 3 3 4 1 . 3 9 8 7 8 0 . 2 0 9 4 9 0 . 0 1 4 5 5 I . 5 3 0 7 0 0 . 0 0 7 6 5 1 . 6 0 . 8 4 1 1 0 6 9 . 6 3 1 5 7 0 . 3 4 8 16 0 . 0 5 0 1 1 4» 5 6 7 0 7 0 . 0 2 2 8 4 3 » 3 0 . 8 6 8 0 7 1 2 0 . 9 5 9 3 I 0 . 6 0 4 8 I 0 . 1 5 7 1 9 1 1 . 4 2 0 4 5 o . 0 5 7 10

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183

H

ki

0.25

0.2

<r -o-Si r , 2i rg 8a ra 2a r j

ka a Or2

o . 1 o . 2 7115 0 .05598 0 .27990 0 . 0 x 2 5 9 0 .00274 0 . 0 x 3 7 0 0. 2 Q.65 xog 0.126 28 0 .63x38 0 .04892 0 .0106 0 0 . 0 5 3 0 2 0. ,1

*t o . 9 0 4 0 4 0. X42X9 0 .71096 0 .17538 0 .03744 0 .X8722 0 . 8 0 .95659 0 . 1 2 3 0 0 0 .6 1499 0 .48699 0 . 0 9 8 3 9 0. 49196 X . 6 0 .99703 0 . X 0 5 3 4 0 .5 2669 0 . 8 1 2 4 9 0 .139x7 0 .69586 3* 2 0 .99927 0 .0506 3 0 .25317 0 .92951 0 .111x4 0 . 5 5 5 6 9

2.0

0. X 0 .27 X 03 0. 05477 0 .27385 0. 6063 X

0 . 0 0 7 3 9 0 .0x409 0 .05484

0 . 00704 0. 2 0 . 6 6 0 1 0 0. X 2X 36

0 .27385 0. 6063 X 0 . 0 2 8 9 3

0 .0x409 0 .05484 0. 02742

0 . 4 0 . 9 0 X 20 o . 12390 0 .6 X949 0 .10664 0 . 1 9 7 8 0 0 . 09890 0 .8 0 .94928 0. 06482 0 .324x0 0 . 3 2 6 1 7 0 ,56039 0 . 28019 x . 6 0 . 9 9 0 2 9 - 0 . 00519 - 0 .02594 0 .69047 0. 96 216 0 . 4 0 xo3 3 . 2 X . 0 0 0 0 0 - 0. 0 2 2 X 6 - 0 .1108 0 0 .95608 0 .87221 0. 43610

20.0

0.1 0 .26945 0. 05192 0. 25960 0. 00222 0 . 03116 0. oox 56 0. 2 0 .66161 0. I 1209 0 . 50040 0 . 00877 0. 12227 0. 0061 X 0. 4 0 . 90102 0. 08622 0 . 43111 0 . 03354 0 . 45504 0 . 02275 0.8 0 .94012 - 0. 07351 — 0. 36756 0 . 11653 X . 44285 0. 07214 x . 6 0 .97277 - 0. 40234 - 2 . 01169 0 . 33693 3. 3700 X 0 . 16850 3.2 0 .99075 - 0. 71901 - 3' 59542 0. 73532 5 . X0060 0 . 25503

k a a 200.1

0. X 0 .27072 0 . 04956 0. 24778 0 . 00051 o . 01704 0. 00024 0 . 2 0 . 6 5909 0. I 0066 0. 50330 0 . 00202 0. 18557 o . 00093 0 . 4 0 .89724 0. 04243 0 . 21242 0 . 00791 0. 70524 0. 00353 0.8 0 .93596 - 0. 2407 1 - 1. 20357 0 . 02g3 X 2 . 40585 0 . 01203 1.6 0 . 9 6 3 7 0 - X . 00743 - 5' 03714 0. I 0193 6 . 8248 I 0 . 03412 3. 2 0 .97335 " 2 . 54264 - 1 2 . 71320 0 . 30707 15 . 45931 0. 07730

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184

R

k |

0.25

2.0

8« n B« ra *• rs ka n 0.2

O. 1 0. 15577 0 .28658 0 .14339 0 .01348 0 ,00277 0 , 0 1 3 8 4 O. 2 0 . 4 3 3 1 0 0 .72176 0 . 36088 0 .05259 0 .01075 0 , 0 5 3 7 7 0 . 4 0 .79551 1.03476 0 .51738 0 , 1 9 0 9 4 0 ,03842 0 , 1 9 2 1 I O . d 1.00871 0 .88833 0 .44416 0 . 5 4 5 7 0 0 .10337 0 .51687 1.6 1 ,02425 0 .66438 0 .33219 0 . 9 0 5 6 3 0 .14102 0 . 7 0 5 1 0 3 . 2 0 . 99617 0 .41539 0 .20773 0 . 9 3 9 1 8 0 .09804 0 , 4 9 0 2 0

0. X 0 . 15524 0 .28362 o. 14181 0 . 0 0 7 1 0 0 .01353 0* 2 0. 428 09 0 . 7 0 2 2 5 0 . 35112 0 .0278 3 0 ,05278 0 . 4 0. 77939 0 .966 34 o. 48317 0 ,10306 0 .X9178 0 . 8 0. 06703 0 .66885 0 . 3344.2 0 .31771 0 .55211 1.6 o. 98156 0 .17331 0. 08665 0 . 6 6 7 5 3 0 . 9 5 0 8 0 3 . 2 0. 99840 - 0 .05691 - 0. 02846 0 .93793 0 , 8 9 3 9 0

0. 1 o. 15436 0 .27580 0. 13790 0 . 0 0 1 7 9 0 .02728 0 . 2 0 . 4246 2 0 .67115 0 .33557 0 .00706 0 .10710 0 . 4 0. 766 47 0 . 3 446 2 0 .42231 0 .02697 0 .39919 o . d 0. 92757 0.219^1 0 .10976 0 . 0 9 2 8 5 1* 26565 1.6 0 . 91393 - 1 .22411 - 0 .61205 0 .26454 2 .94860

4 .89878 3 . 2 0 . 95243 - 3 . 0 4 3 2 0 - 1 .52160 0 . 6 0 7 5 4 2 .94860 4 .89878

0 . 1 o. 15414 0 . 26776 0. 13388 0 .00036 0 ,03814 0* 2 0. 42365 0. 63873 0 . 31937 0 . 0 0 1 4 3 0 . 1 5 0 4 0 0 . 4 0 . 76296 0* 71620 0 . 35810 0 . 0 0 5 5 7 0 .57046 0 .8 0 . 91600 - 0 . 28250 - 0 . 14125

54928 0 .0206 4 1 .92636

1.6 0. 88406 - 3 . 098 56 - 1. 14125 54928 0 . 0 7 0 1 4 5 '35936

3 .2 0 . 897 12 - 9 . 18214 - 4' 59107 0 . 2 1 6 9 2 12 .64318

ka « 2.0

o .00677 o. 02639 o .09589 o .27605 0 , 4 7 5 4 0 0 .44695

k« • 20.0

o ,00136 o .00536 0 .01996 0 .06328 0 . 1 4 7 4 3 0 . 2 4 4 9 4

ka " 200.0

o .00019 o .00075 o .00285 o .00963 0 . 0 2 6 8 0 0 .06322

Page 10: Tables of Stresses in Three-Layer Elastic Systemsonlinepubs.trb.org/Onlinepubs/hrbbulletin/342/342-008.pdf · with some notes on the assumptions involved in setting up the problem

185

H B 0.25

k f s 20*0

o . I O . 2

0 . 3 X . 6 3*2

21

o . 0 4 5 9 6 o . I 5126 o . 4 1 0 3 0 o . 8 5464 I . 1 2 0 1 3 o . 9 9 6 7 6

8 t r ,

0 . 0 1 4 5 0 1 .76675 3 . 5 9 6 5 0 4 . 58845 2 . 31165 1 .24415

at r t

o . 0 3 0 7 2 o . 0 8 8 3 4 o . 17983 o . 2 2 9 4 2 o . 1 1 5 5 3 o . 0 6 2 2 1

o . 0 1 1 0 7 0 . 0 4 3 5 7 o . 1 6 3 3 7 0 . 5 1 6 4 4 1 .0106 I 0 . 9 9 1 6 8

O . 0 0 2 0 2 o . 0 0 7 9 3 o . 02931 o . 0 8 7 7 I o . 1 4 0 3 9 o . 0 7 5 8 7

k g a 0.2 o . 0 1 0 1 1 o . 0 3 9 6 4 o . 14653 o . 4 3 8 5 4 0 . 7 0 1 9 4 0 . 3 7 9 3 4

2.0

0* I 0 . 0 4 3 8 1 0 . 6 3 2 1 5 0 . 0316 2 0 . 0 0 5 3 0 o . 0 0 9 6 2 0 . 0 0 4 8 I o » a ot14202 1 .9 3766 0 . 09188 0 . 0 2 0 9 1 0 . 0 3 7 8 1 0 .0189X 0 . 4 0 . 3788 2 3 . 8 6 7 7 9 0 . 19339 0 . 0 7 9 3 3 0 . 1 4 1 5 9 0 . 0 7 0 7 9 0 . 8 0 . 7 5 9 0 4 5 . 5 0 7 9 6 0 . 27540 0 . 2 6 2 7 8 0 . 4 4 7 1 0 0 . 2 2 3 5 5 1.6 0 . 9 8 7 4 3 4 . 2 4 2 8 1 0 . 21213 0 . 6 1 6 7 3 0 . 9 0 1 1 5 0 . 4 5 0 5 8 3 » 2 I • 0 0 0 6 4 1 .97494 0 . 09876 0 . 9 1 2 5 8 0 . 9 3 2 5 4 0 . 4 6 6 27

k a s 20.0

0 . 1 0 . 042 36 13708

0 . 6 5 0 0 3 0 . 03250 0 . 00123 0 . 0 1 9 3 0 0 . 00096 0 . 2 0 .

042 36 13708 1 .90693 0 . 09535 0 . 00488 0 . 0 7 6 2 3 o . 00381

0 . 4 o . 35716 4 . 1 3 9 7 6 0 . 20699 o . 01383 0 . 2 9 0 7 2 o . 01454 0 . 8 0 . 68947 6 . 4 8 9 4 8 0 . 32447

34782 0 . 0 6 7 4 1 0 . 9 8 5 6 5 o . 04928

1.6 0 . 85490 6 . 9 5 6 3 9 0 . 32447 34782 0 . 20115 2 . 5 5 2 3 1 0 . 12762

3 ' 2 0 . 90325 6 . 0 5 8 5 4 0 . 30393 0 . 48647 4 . 7 6 2 3 4 o . 238 12

k a 3 2C0.0

0 . 1 0 . 0 4 2 0 4 0 . 6 5 7 3 2 0 . 03287 0 . 0 0 0 2 4 0 . 02711 0 . 00014 0 . 2 0 . 13584 1 .93764 0 . 09688 0 . 0 0 0 9 5 0 . 10741 0 . 00054 0 . 4 0 . 3 5 2 3 7 4 . 2 6 0 0 4 0 . 21300 0 . 0 0 3 7 2 0 . 41459 0 . 00207 0 . 8 0 . 6 7 2 8 6 6 . 9 4 8 7 1 0 . 34743 0 . 0 1 3 9 9 1 . 46947 0 . 00735 1.6 0 . 8 1 2 2 3 8 . 5 5 7 7 0 0 . 42789 0 . 0 4 8 30 4 . 36521 o . 0218 3 3 . 2 0 . 8 2 3 9 0 1 0 . 6 36 14 0 . 53181 0 . 1 5 3 7 8 1 0 . 93570 0 . 05468

Page 11: Tables of Stresses in Three-Layer Elastic Systemsonlinepubs.trb.org/Onlinepubs/hrbbulletin/342/342-008.pdf · with some notes on the assumptions involved in setting up the problem

186

H = 0.25

k< s 200.0

a i <r - c r or — c a i 2 i r a 8 a Z a r a Z a r s

k a B 0, 0 . I o . 0 1 1 39 o ,S6o ; 1 0 . 00.,33 •5 .00539 0 • 0 0 0 9 0 o » 00451 0 . 2 0 . 0 4 1 8 0 2 . 7 1 3 5 4 0 . 0 1 3 5 7 0 . 0 2 3 3 4 0 . 0 0 3 5 7 0 . 0 1 7 8 4 0 . 4 0 . 14196 6 . 8 3 0 2 1 0 . 0 3 4 1 5 0 . 0 9 0 2 4 0 . 0 1 3 6 5 0 . 0 6 8 2 4 0 . 3 0 . 4 2 6 0 3 13 . 19664 0 .06 598 0 . 2 1785 0 . 0 . ;6s 4 0 . 2 3118 I . 6 0 . 9 4 5 2 0 I 3 ' 7 9 I 34 0 . 06 3 96 0 . 8 3 3 7 1 0 . 101^91 0 . 5 2 0 5 5 3 ' 2 1 .10738 2 . 7 2 9 0 1 0 . 0136 5 I , 1 0 2 5 9 0 . 0 8 0 0 8 0 . 4 3 0 3 7

2.0

0. I 0 . 00909 0 . 9 6 5 5 3 0 . 0048 3 0 . 0 0 2 5 9 0 . 00407 0 . 00203 0 . 2 0 . 0 3 2 6 9 3 . 1 0 7 6 3 0 . 0 I 5 5 ''r 0 . 0 1 0 2 7 0 . 016 11 0 . oo3 06 0 . 4 0. I 008 4 8 . 3 7 8 5 2 0 . 04189 0 . 0 4 0 0 0 0 . 06221 0 . 03110 0 . 8 0 . 3 0 4 7 7 1 8 . 9 5 5 3 4

3 1 . 1 8 9 0 9 0 . 09478 0 . 1 4 5 1 3 0 . 31860 0 . 10930

I . 6 0 . 6 6 7 8 6 1 8 . 9 5 5 3 4 3 1 . 1 8 9 0 9 0 . 15595 0 . 4 2 9 4 0 0 . 58553 0 . 29377

3 ' 2 0 . 98447 2 3 . 9 8 5 0 0 0 . 14493 0 . 8 4 5 4 5 0 . 3 n i o i 0 . -,4595

20.0

0 . I 0 . 00776 :. 08738 0 . 00544 0 . 0006 5 0 . oo36 I 0 . 00043 0 . a 0 . 02741 3* 59448 0 . 01797 0 . 00257 0 . 03421 0 . 0017 I 0 . r c . 0803., 1 0 . 30023 0 . 05155 0 . 0101 ."r 0 . 13365 0 . 0066 3 0 . 3 0 . 23137 2 6 . 4 1442 0 . 13207 0 . 038 4'r 0. 49135 0 . 02457 I . 6 0 . 46835 5 7 ' 46409 0 . 28732 0 . I 3 I - r 8 I . 53833 0 . 07692 3 ' 2 0 . 71083 99 • 29034 0 . 4964s 0 . 373'r2 3* 6096 4 0 . 18048

k a = 200.0

0 . I 0 . 00744 I . 19099 0 . 00596 0 . 00014 0 . 01311 0 . 00007 0 • 2 0 . 026 16 4* ooo5 S 0 . 02005 0 . 00056 0 . 05223 0 . 00026 0 . 4 0 . 08 141 I I . 96 405 0 . 05982 0 . 00224 0 . 20551 0 . 00103 0 . 3 0 . 21203 3 2 . 97364 0 . 16487 0 . 0 08 7 I 0 . 77534 0 . 00388 I . 6 0 . 40876 8 2 . 77997 0 . 41390 0 . 0 3 2 3 2 . 6 3 96 £ 0 . 01320 3 ' 2 0 . 56613 1 8 9 . 37439 0 . 04687 0 . 11049 7 . 60287 0 . 03801

Page 12: Tables of Stresses in Three-Layer Elastic Systemsonlinepubs.trb.org/Onlinepubs/hrbbulletin/342/342-008.pdf · with some notes on the assumptions involved in setting up the problem

187

H B 0.5

k , o 0.2

cr <r <r -cr <r -0" a t 81 r a a a r a B a r s

= 0,2 0 . I 0 . 07943 0 . 01705 0 .08 527 0 . 00914 0 . 00206 0 . 0 1 0 3 0 0 . 2 0 . 27189 0 . 05724 0 . 2 8 6 2 1 0* 03577 0 . 00804 0 . 0 4 0 2 0 0 . 4 0 . 66375 0 . I 3089 0 . 6 5 4 4 4 0 . 13135 0 . 02924 0 . 146 22 0 . 3 0 . 91143 0 . 15 514 0 . 7 7 5 7 1 0 . 33994 0 . o3 36 9 0 . ^ 1 8 4 3 1.6 0 . 9^334 0 . 13050 0 . 6 6 2 4 8 0 . 72 106 0 . 13729 0 . 6 8 6 4 7 3 » 2 0 . 99310 0 . 06976 0 . 3 4 8 7 9 0 . 39599 0 . 12674 0 . 6 3 3 7 1

k a s 2.0

0. : 0 . 07006 0 . 0 : 6 1 7 0 . o 3 o 8 5 0 . 00557 0 . 01074 0 . 0 0 5 3 7 0 . 2 0 . 27046 0 . 05375 0 . 2 5 3 7 7 0 . 02190 o . 0 2 06 0 . 0 2 1 0 3 0*4 0 . 65347 0 . 11770 0 . 5 8 8 4 8 0 . 08222 0 . 15534 0 . 0 7 7 6 7 0 . 8 0 . 39579 0 . 11252 0 .56 258 0 . 26 429 0 . 47045 0 . 2 3 5 2 3 1.6 0 . 9^217 0 . 0 ',897 0 . 2 4 486 0 . 6 0 3 5 7 0 . 90072 0 . 4 5 0 3 6 3« 2 0 . 99189 0 . 01380 0 . 06900 o . 91215 0 . 94385 0 . 4 7 1 9 2

k a 0 20.0

0 . I 0 . 0706 2 0 . 01439 o » 07196 0 . 00175 0* 02415 0 . 0 0 1 2 I 0 . 2 0 . 26873 0 . 0466 9 0 . 2 3 3 4 5 0 . 00692 0 . 095 19 0 . 0 0 4 7 6 0 . 4 0 . 65188 0 . 09018 0 . 4 5089 0 . 02676 0 . 36008 0 . 0 1 8 0 0 0 . 8 0 . 87401 0 . 01269 0 . 0 6 3 4 7 o . 09552 I . 19151 0 . 0 5 9 5 8 r . 6 0 . 39563 - 0 . — I . 2 1 6 8 0 0 . 28721 2 . 05409 0 . 1 4 7 7 0 3 . 2 0* 95392 - 0 . 53220 — 2 . 6 6 1 0 0 0 . 66445 4* 86789 0 . 2 4 3 3 9

k a » 200.0

0 . 1 0 . 07820 0 . 01243 0 . 06 21 3 0* 0 0 0 4 1 0 . 03682 0 . 0 0 0 x 3 0 . 2 0 . 26803 0 . 03912 0 . 19558 0 . 00163 0 . 14576 0 . 0 0 0 7 3 0 . 4 0 . 6 4904 0 . 06006 0 . 3 0 0 2 9 0 . 006 43 0 . 56051 0 . 0 0 2 8 0 0 . 3 0 . 86 406 — 0 . 10447 - 0 . 5 2 2 3 4 0 . 02436 I . 0677 I 0 . 0 0 9 8 4 1.6 0 . 86677 - 0 . 67154 - 3 .35768 0 . 08 5 40 5* 77669 0 . 0 2 8 8 8 3*2 0 . 89703 - I . 8 6 1 2 6 — 9 .30628 0 . 26 46 7 i 3 « 63423 0 . 0 6 8 1 7

Page 13: Tables of Stresses in Three-Layer Elastic Systemsonlinepubs.trb.org/Onlinepubs/hrbbulletin/342/342-008.pdf · with some notes on the assumptions involved in setting up the problem

188

H 0.5

2.0

or H T <r -or Zi r t Z a zu r t

k a B 0.2 0 . 1 O . 2 0 . 4 0 . 8 1.6 3 ' 2

0 . 0 4 4 0 6 0 . 15978 0 . 4 4 5 2 3 0 .3 3298 I . 0 5 4 6 2 0 . 9 9 9 6 7

0 . 0 8 3 9 8 0 . 2 8 9 0 4 0 . 7 2 3 1 3 1.036 03 0 . 8 3 4 7 5 0 . 4 5 1 1 9

0 . 0 4 1 9 9 o . 1 4 4 5 2 0 . 3 6 1 5 6 0 . 5 1 8 0 2 0 . 4 1 7 3 7 0 . 2 2 5 6 0

0 . 0 0 9 0 3 0 . 0 3 5 5 1 0 . 1 3 3 1 4 0 . 42190 0 . 8 5 5 2 9 0 , 9 4 5 0 6

0 . 0 0 1 8 1 0 . 0 0 7 1 1 0 . 0 2 6 3 4 0 . 0 7 9 9 2 O '13973 0 . 10667

0 . 0 0 9 0 6 0 . 0 3 5 5 4 0 . 1 3 1 7 2 0 . 3 9 9 6 2 0 . 6 9 8 6 3 0 . 5 3 3 3 6

2.0

0 . 1 0 . 04330 0 . 0 8 2 5 0 0 . 04125 0 . 0 0 4 6 5 0 . 00873 0 . 0 0 4 3 9 0 . 2 0 . 15325 0 . 28318 0 . 14159 0 . o i 3 36 o . 03454 , 0 . 0 1 7 2 7 0 . 4 0 . 42077

75633 0 . 7 0 1 1 9 0 . 35060 0 . 0 6 974 0 . 1295 0 . 0 6 4 7 7

0 . 8 o . 42077 75633 0 . 9668 1 0 . 48341 0 . 2 3 2 5 6 0 . 41187 0 . 2 0 5 9 4

1.6 0 . 93447 0 . 7 0 7 2 6 0 . 35363 o . 5 6 2 9 8 0 . 85930 0 . 4 2 9 6 5 3 . 2 0 . 9 8 8 0 1 0 . 3 3 8 7 8 o . 16939 0 . 8 8 6 5 5 0 . 96353 0 . 4 8 1 7 6

20.0

0 . 1 0 . 0 4 1 9 3 0 . 0 8 0 4 4 0 . 04022 13787

0* 00117 0 . 01778 0 . 00089 0 . 3 0 . 1 4 8 0 8 0 . 2 7 5 7 4 0 .

04022 13787 0 . 0 0 4 6 4 . 0 . 07027 0 . 00351

0 . 4 o . 4 0 0 8 6 0 . 6 7 1 7 4 0 . 33587 0 . 0 1 7 9 9 0 . 263 17 0 . 01341 0 . 8 0 . 6 9098 0 . 8 6 1 9 1 0 . 43095 0 . 0 6 476 0 . 91168 0 . 04553 1.6 0 . 7 9 3 3 8 0 . 3 9 5 8 8 0 . 19794 0 . 19803 2 . 38377 0 . 11919 3 . 2 0 . 8 5 9 4 0 - 0 . 4 1 0 7 8 - 0 . 20539 0 . 4 9 2 3 3 4 . 47022 0 . 22351

k a B 200.0

0 . 1 0 . 04160 0 . 0 7 8 6 4 0 . 03932 0* 00024 0 . 0 3 5 1 5 0 . 0 0 0 1 3 0 . 2 0 . 14676 0 . 2 6 8 53 0 . 13426 0 . 00005 0 . 0 9 9 6 8 0 . 0 0 0 5 0 0 . 4 0 . 39570 0 . 6 4 3 0 3 0 . 32152 o . 00374 0 . 3 8 4 9 7 o . 0 0 1 9 2 0 . 8 0 . 67257 0 . 7 4 9 4 7 0 . 37474

0138 1 0 . 01416 1 .30766 0 . 0 0 6 8 4

1.6 o . 74106 - 0 . 0 2 7 6 1 — 0 . 37474 0138 1 0 . 04972 4 . 0 8 9 3 7 0 . 0 2 0 4 5

3 . 2 0 . 75176 - 1 .33545 - 0 . 94273 0 . 15960 1 0 . 2 5 6 3 1 0 , 0 5 1 3 3

Page 14: Tables of Stresses in Three-Layer Elastic Systemsonlinepubs.trb.org/Onlinepubs/hrbbulletin/342/342-008.pdf · with some notes on the assumptions involved in setting up the problem

189

H 0.5

20.0

a t ' 2 , . 2 | Ti 2 | T a ' 2 a 0"

8 a r a

O . 1 0 . 2 o . 4 0 . 8 1.6 3 . 2

0 . 0 1 3 5 1 0 . 0 5 0 7 9 0 . 1 6 9 7 2 0 . 4 7 1 9 1 0 . 9 7 4 5 2 I . 0 9 9 1 1

0 .16 526 0 . 5 8 9 1 8 1 .66749 3 . 2 3 1 2 1 3 . 5 4 3 5 3 1 .27334

0 .oo3 26 0 . 0 2 9 4 6 0 . 0 8 3 3 7 0 . 1 6 1 5 6 0 . 1 7 7 4 3 0 . 06367

0 . 0 0 5 9 6 0 . 02 36 1 0 . 0 9 1 1 0 0 . 3 1 9 0 4 0 . S 2 6 0 9 1 .08304

0 . 0 0 0 9 8 0 . 0 0 3 8 6 0 . 0 1 4 7 4 0 . 0 4 9 6 7 0 . 1 1 2 7 9 0 . 0 9 5 2 7

O . I 0 . 2 0 . 4 0 .3 1.6 3 . 2

0 . 0 1 1 2 2 0 . 0 4 1 7 2 o . 1 3480 0 . 3 5 1 7 5 o . 70221 o . 9 7 420

o . 1 7 9 9 7 0 . 6 ",779 1.898 17 4 . 0 9 5 9 2 6 . 2 2 0 0 2 5 . 4 1 8 2 8

o . 0 0 9 0 0 o . 0 3 2 3 9 o . 0 9 4 9 1 o . 2 0 4 8 0 o . 3 1 1 0 0 o . 3 7 0 9 1

o . 0 0 2 5 9 O . O I 0 2 3 0 . 0 3 9 9 3 o . 14419 o . 4 2 1 0 6 0 . 8 2 2 5 6

o . 0 0 4 4 0 o . 0 1 7 4 4 o . 06722 o . 2 3 4 7 6 0 . 6 2 0 4 6 0 , 9 3 3 3 1

2 a r» k a " 0.2 o . 0 0 4 8 8 o . 0 1 9 2 9 0 . 0 7 3 6 9 o . 3 4 8 3 4 0 . 5 6 3 9 5 0 . 4 7 6 3 7

k a = 2.0 o . 0 0 2 2 0 o . 0 0 8 7 2 0 . 0 3 3 6 1 o . 1 1 7 3 3 o . 3 1 0 2 3 o . 4 6 9 1 6

k a a 20.0

0 . 1 0 . 00990 0 . 19872 0 . 0 0 9 9 4 O . 2 0 . 0 36 48 0 . 72264 0 . 0 3 6 1 3 0 . 4 0 . 11443 2 . 19520 0 . 1 0 9 7 6 0 . 8 0 . 27934 5 .24726 0 . 3 6 2 3 6 1.6 o . 50790 1 0 . 3 0 2 1 2 0 . 5 1 5 1 1 3 . 3 0 . 70903 1 6 . 3 8 5 2 0 0 . 8 1 9 2 6

o . 0 0 0 6 3 0 . 0 0 2 5 1 o . 0 0 9 8 8 0 . 0 3 7 3 1 o . 1 2 6 5 4 0 . 3 5 8 0 7

o . 0 0 9 X I 0 . 0 3 6 2 0 0 . 1 4 1 1 6 0 . 5 1 5 8 5 1 . 5 9 3 4 1 3 . 6 9 1 0 9

o . 0 0 0 4 6 o . 0 0 1 8 1 o . 0 0 7 0 6 0 . 0 2 5 7 9 o . 0 7 9 6 7 0 . 1 8 4 5 5

k a B 200.0

o . 1 O . 2 0 . 4 0 .8 1.6 3*2

o . 0 0 9 6 0 o . 03526 0 . 10070 o . 3 6 I 49 o . 45078 o . 5 7 0 7 4

o . 2 1 4 4 0 0 . 7 8 4 9 3 2 . 4 4 4 3 0 6 . 2 3 4 2 4

1 4 . 1 1 4 0 0 2 9 . 9 5 8 1 5

o . 0 1 0 7 2 o . 0 3 9 2 5 O . 1 2 3 2 I

0 . 3 1 1 7 2 0 . 7 0 5 7 4 1 . 4 9 7 9 1

0 . 0 0 0 1 3 o . 0 0 0 5 4 o . 0 0 2 1 4 o . o o 3 31 0 . 0 3 0 7 0 o . 1 0 4 7 0

0 . 0 1 3 5 5 0 . 0 5 3 9 5 0 . 2 1 1 9 5 o . 7 9 5 8 3 2 . 6 7 5 7 8 7 . 6 1 4 5 7

o . 0 0 0 0 7 o . 0 0 0 2 7 0 . 0 0 1 0 6 o . 0 0 3 9 8 0 . 0 1 3 3 8 o . 0 3 O 0 7

Page 15: Tables of Stresses in Three-Layer Elastic Systemsonlinepubs.trb.org/Onlinepubs/hrbbulletin/342/342-008.pdf · with some notes on the assumptions involved in setting up the problem

190

H . 0.5

k i a 200,0

O . I O . 2 o. 4 0 . 8 1 . 6 3 ' 3

o. 00363 o . 0 1 4 1 4 o .05356 o . 1 8 1 0 7 0 . 5 3 4 6 5 1 .04537

o .22388 o .81903 2 . 5 3 5 5 8 6 , 1 1 4 3 9

T O . 8 2 7 0 5 9 . 3 4 3 1 3

o .00112 o . 0 0 4 1 0 0 . 0 1 2 6 3 o. 03057 0 . 0 5 4 1 4 o . 0 4 6 7 1

o.00356 0 . 0 I 0 2 1 o» 04014 o .15048 o . 4 8 2 0 1 1 . 0 0 6 7 1

or -C 8 a r a

o.0003 3 o . 0 0 1 3 0 o .00506 0 . 0 1 8 4 4 0 . 0 5 3 9 9 o .08634

8 a Tj

k a a 0.2 o.0016 3 o.006 ;8 0 . 0 2 5 2 9 o . 0 9 2 3 1 o.36 993 o . 4 3 1 2 1

k « 2.0

o. I O . 3 o. 4 0 . 8 1.6 3 . 3

o .002 15 o » o o S 2 6 0 . 0 2 9 4 6 o .09508 0 . 2 7 1 3 5 0 . 6 2 3 9 9

o. 26620 o. 98773 3 . 1 9 5 8 0 8 . 7 1 9 7 3

2 0 . 1 5 7 6 5 3 4 . 3 5 2 2 9

o .00133 o . 0 0 4 9 4 o .01598 o . 0 4 3 6 0 o .10079 o .17126

o . 0 0 0 9 4 0 . 0 0 3 7 3 0 . 0 1 4 7 4 o . 0 5 6 2 2 o .19358 o .52913

o .00138 o .00509 o .01996 0 . 0 7 4 3 4 o.338 33 0 . 5 4 9 3 1

o .00064 o . 0 0 3 5 4 o .00998 0 . 0 3 7 1 7 o . 1 1 9 1 9 o. 27466

k a <• 20,0

O . I O . 3 0 . 4 0 . 8 1.6 3 . 3

o . 00149 o . 0 0 5 6 4 o . 0 1 9 1 1 0 . 0 5 5 7 4 o . 1 3 9 4 6 . 0 . 3 0 2 4 7

o .31847 I . 1 9 5 0 8 4« 03732

1 3 . 0 0 8 3 5 3 3 . 7 7 0 2 8 7 7 . 6 3 9 4 3

o .00159 o .00598 O . 0 3 0 1 4 o .06004 o. 16 38 5 0 . 3 8 8 1 5

0 . 0 0 0 3 3 o . 0 0 0 9 4 o . 0 0 3 7 2 0 . 0 1 4 5 3 0 . 0 5 3 9 9 o. 18091

o .00257 o .01025 o .04047 0 , 1 5 4 5 3 0 , 5 3 8 3 6 1.56 409

o .00013 o , 0 0 0 5 1 O , 0 0 3 0 2 0 . 0 0 7 7 3 o .02693 o . 0 7 8 3 0

200.0

O . I O . 3 o. 4 0 . 8 1.6 3 « a

o , 00133 o , 0 0 4 9 8 o . 01649 0 . 0 4 5 5 3 o . 1 0 2 0 9

o , 3 7 0 6 5 1 .40493 4 . 8 6 3 1 5

1 5 . 3 3 9 0 3 45*93954

0 . 1 8 3 5 8 1 2 8 , 1 3 0 5 1

o . o o i 3 5 o,00703 o .03431 o .07670 o.33970 0 . 6 4 0 6 5

o .00005 O . 0 0 0 2 3 0.ooo36 o . 0 0 3 4 0 0 . 0 1 3 1 5 0 , 0 4 8 5 4

o .00387 0 . 0 1 5 4 4 o. 06 1 18 0 , 23698 0 . 8 6 3 4 5 2 . 8 0 8 7 7

o . 0 0 0 0 2 o ,00008 0 . 0 0 0 3 1 o .00118 o ,00432 o , 0 1 4 0 4

Page 16: Tables of Stresses in Three-Layer Elastic Systemsonlinepubs.trb.org/Onlinepubs/hrbbulletin/342/342-008.pdf · with some notes on the assumptions involved in setting up the problem

191

H » 1.0

k i a 0.2

o. I O . 3

0 . 4 0 . 8 1.6 3 « a

o . 0 2 0 9 0 o. 08023 o. 27493 0 . 6 7 3 3 0 0 . 9 2 5 9 5 o. 95853

0 . 0 0 4 6 4 0 . 0 1 7 7 3 o .05976 o .13813 o .15978 o .09723

0 . 0 2 3 2 0 0 . 0 8 8 6 5 0 . 3 9 8 7 8 0 . 6 9 0 9 2 0 . 7 9 8 8 8 0 . 4 8 6 1 2

o . 0 0 5 4 1 0 . 0 2 1 3 8 0 . 0 8 1 2 5 0 . 26887 0 . 6 0 2 2 9 0 . 8 2 1 9 4

B a r a

o.00128 o .00503 o .01903 o .06193 0 . 1 3 0 0 2 o .14348

8 a r j

k a a 0.2 o. 006 38 o .02515 o .09516 o . 3 0 9 6 0 0 . 6 5 0 1 0 0 . 7 1 7 4 3

Ca a 2.0

0 . 1 O . 0 3 0 4 5 0 . 0 0 4 1 0 0 . 3 0 . 0 7 8 4 5 0 . 0 1 5 6 1 0 . 4 0 . 3 6 8 1 6 0 . 0 5 1 6 6 0 . 8 0 . 6 5090 0 . 11111 1.6 0 . 8 8 1 7 1 0 . 10364 3 . 3 0 .94X 53 0 . 06 967

o. 02053 o. 07805 o.25838 0 . 5 5 5 5 5 0 . 5 1 8 1 9 0 . 3 4 ^ 3 5

o .00356 0 . 0 1 4 1 0 0 . 0 5 4 3 7 0 . 1 8 8 4 2 0 . 4 8 9 5 7 0 .8 1663

0 . 0 0 6 8 7 o .02713 o . 1 0 3 5 1 o. 34703 o.79986 0 . 9 9 7 5 7 '

o.00343 0.01357 0.05175 o. 17351 0.39993 0.49879

k . 20.0

0 . 1 0 . 3 o. 4 0 . 8 1.6 3 . 2

o . 0 1 9 8 1 0 . 0 7 5 8 7 o .35817 o . 6 1 5 4 4 0 . 7 8 8 8 4 0 . 8 3 9 3 6

o.00300 o .01145 0 . 0 3 5 / 0 0 . 0 5 1 6 3 O . 0 7 3 l 3 o .25569

o .01529 o .05736 o .17702 o .35817 o. 36091 1 .37847

O . 0 0 1 1 8 o .0047 1 o .01846 o.o63 39 o. 31770 O . 5 3 6 1 3

0 . 0 1 5 9 1 o. 06 31 o o.24396 0 . 8 6 1 1 4 3 . 3 6 0 5 4 4 . 2 8 1 6 9

0 . 0 0 0 8 o p . 0 0 3 1 0 O . 0 1 2 3 0 o .04306 0 . 1 1 8 0 3 O . 2 1 4 0 8

k a a 200.0

o. 1 O . 3 0 . 4 0 . 8 1.6 3 » 3

0 . 0 1 9 5 3 0 . 0 7 4 7 3 o. 35368 0 . 5 9 8 5 3 0 . 7 3 3 8 7 o .70248

0 . 0 0 3 1 4 o .00777 o.03076 o.005 38 0 . 3 8 0 5 0 o .90965

o.oio63 o .0388 3 o .10383 o . 0 3 6 9 0 I , 4 0 2 5 0 4 , 5 4 8 3 6

o .00028 o . 0 0 1 1 o 0 . 0 0 4 3 6 0 . 0 1 6 7 9 O . 0 6 02 O o.191O9

o .03412 o .09587 o .37417 I . 3 6 9 3 0 4 .2380s

1 0 . 3 6 5 0 7

o . 0 0 0 1 s o .00048 o .00187 0 . 0 0 6 S 5 0 . 0 2 1 1 9 0 . 0 5 1 8 3

Page 17: Tables of Stresses in Three-Layer Elastic Systemsonlinepubs.trb.org/Onlinepubs/hrbbulletin/342/342-008.pdf · with some notes on the assumptions involved in setting up the problem

192

H • 1.0

k « a 2.0

o , 1 O . 2 0 . 4 0 . 8 1.6 3 . 2

0 . 0 1 2 4 1 o . 0 4 8 1 6 o . 17203 0 . 4 8 6 1 3 0 . 9 1 3 1 2 1 . 0 4 6 7 1

S t r ,

o . 0 2 1 8 6 0 . 08 396 o . 2 3 3 6 6 0 . 7 1 6 8 4 o . 97206 0 . 6 0 0 9 1

« « r a

o . 0 1 0 9 3 o . 0 4 1 9 8 o . 1 4 4 3 3 o , 3 5 8 4 2 o . 4 8 6 0 3 o . 3 0 0 4 6

o . 0 0 4 9 0 0 . 0 1 9 4 3 o . 0 7 4 9 6 0 , 2 6 1 9 3 o . 676 1 1 0 . 9 5 9 8 5

« i r a

o . 0 0 0 9 6 o . 0 0 3 7 8 o . 0 1 4 4 8 o . 0 4 9 2 4 o . 1 1 5 5 8 o . 1 2 5 2 7

« • r s

k a . 0.2 o . 0 0 4 7 8 o . 0 1 8 9 0 o . 0 7 2 4 1 o . 2 4 6 2 0 0 . 5 7 7 9 0 0 , 6 2 6 37

k a 2.0

o . I o . 3 o . 4 0 .8 1.6 3»3

o . o108 3 o . 0 4 1 7 6 o . 1 4 6 6 5 o . 3 9 9 4 2 0 . 7 1 0 3 3 0 . 9 2 1 1 2

0 . 0 2 1 7 0 0 . 0 8 337 0 . 2 8 4 9 1 0 , 7 1 3 4 1 1 ,02680 o . 9 0 4 8 2

o . 0 1 0 9 0 o . 0 4 1 6 9 o . 1 4 2 4 6 o , 3 5 6 7 0 o . 5 1 3 4 0 0 , 4 5 2 4 1

0 . 0 0 2 4 1 o , 0 0 9 5 8 0 , 0 3 7 2 4 o , 13401 o , 38690 0 , 7 5 8 0 5

o . 0 0 4 5 3 0 . 0 1 7 9 7 o . 0 6 9 3 4 0 . 2 4 2 5 0 0 . 6 3 6 3 1 0 . 9 7 5 0 9

0 . 0 0 2 2 7 o . 0 0 8 99 o . 0 3 4 6 7 o . 1 2 1 2 5 o . 3 1 8 15 0 . 4 8 7 5 4

O . I

O . 2 o . 4 0 .8 1.6 3 . 3

. 00963 , 03697 ,12805 33363 52721 6 5 5 3 0

o . 0 2 2 4 9 o . 08618 o . 2 9 6 4 0 o , 7 6 2 9 2 1 .25168 1 .70723

0 . 0 1 1 2 4 o . 0 4 3 0 9 o . 14820 o . 38146 0 , 6 2 5 8 4 0 . 8 5 3 6 1

o . 0 0 0 6 I o . 0 0 2 4 1 o , 0 0 9 5 0 o . 0 3 5 7 8 o , 1 2 0 0 7 o , 33669

o , 0 0 9 2 0 0 , 0 3 6 5 4 o , 14241 0 , 5 1 8 1 5 1 ,56503 3 , 5 1 1 2 8

k a » 20.0

o , 00046 o . 0018 3 o , 00712 0 , 0 3 5 9 1 0 ,07S2 5 o . 1 7 5 5 6

k a - 200.0

o . I o . 2 o . 4 0 . 8 1.6 3 . 2

o . 0 0 9 2 5 o . 0 3 5 6 1 o . 1 2 3 4 8 o , 3 1 4 2 2 o , 4 6 8 9 7 0 , 5 1 1 6 1

o . 0 2 3 3 9 o . 0 9 0 1 8 o . 3 1 4 7 0 0 . 8 3 2 7 4 I . 5 3 5 2 1 2 . 7 6 4 2 0

o . 0 1 1 7 0 o , 0 4 5 0 9 o . 15735 o . 4 1 6 3 7 o , 76760 1 ,38210

0 , 0 0 0 1 3 o , 0 0 0 5 1 o , 00202 o . 0 0 7 8 3 o , 0 2 8 7 4 0 , 0 9 7 5 I

0 , 0 1 3 1 9 0 , 0 5 2 5 2 o , 20609 0 , 7 6 9 5 5 2 , 5 3 1 0 0 6 , 9 9 2 8 3

o » 00007 o , 0 0 0 2 6 0 . 0 0 1 0 3 o , 0 0 3 8 5 o . 0 1 2 6 5 o , 0 3 4 9 6

Page 18: Tables of Stresses in Three-Layer Elastic Systemsonlinepubs.trb.org/Onlinepubs/hrbbulletin/342/342-008.pdf · with some notes on the assumptions involved in setting up the problem

193

R n 1.0

k | a 20.0

cr z% rt 8 ( r a > i S t r s

k t " 0.2 O . I 0 .00417 o . 0 4 0 5 0 0 .00202 0 .00271 0 . 0 0 0 3 9 0 . 0 0 1 9 5 0 . 2 0 . O I 6 4 I 0 .15675 o . 0 0 7 8 4 o . 0 1 0 8 0 0 .00155 0 .00777 0 . 4 o . 0 6 2 1 0 0 .55548 0 .02777 o . 0 4 2 4 1 0 .006 06 0 .03028 0.8 0 . 2 1 0 5 7 1 .53667 0 .0768 3 0 .15308 0* 02198 0 . X 0 9 9 I 1.6 0 . 5 8 2 i 3 2 . 7 7 3 5 9 0 .13868 0 . 4 9 7 0 5 0 .06 327 0 . 3 1 6 3 5 3 .2 1 .06296 2 .55195 0 . 1 2 7 6 0 I . 0 0 2 1 7 0 .09906 0 . 4 9 5 2 5

k t « 2.0

O . I 0 . 0 0 2 6 3 0 .04751 0 .00233 0 . 0 0 1 0 0 0 .0016 0 0 .0008 0 0. 2 0 . 0 1 0 2 9 0 .18481 0 .00924 0 .00397 0 .00637 o . 0 0 3 1 9 o . 4 0 . 0 3 8 1 0 0 .66727 0 .03336 0 . 0 1 5 6 5 0 .02498 0 . 0 1 2 4 9 0 .8 0 .12173 I . 9 7 4 2 8 0 .09871 0 .05938 0 .09268 0 . 0 4 6 3 4 1.6 0 .31575 4 .37407 0 . 2 1 8 7 0 0 .20098 0 .29253 o . 1 4 6 2 6 3 . 2 0 .66041 6 . 9 7 6 9 5 0 . 3 4 8 8 5 0 .53398 0 .65446 0 .32723

20.0

0.1 0. 00103 0 . 05737 0 . 00287 0 .0002 4 0 .00322 0 .00016 0. 2 0 . 00751 0 . 22413 0* 01121 0 .00098 0 .01283 o . 0 0 0 6 4 0. 4 0 . 03713 0 . 83430 0 . 04121 0 . 0 0 3 8 7 0 .05063 0 .00353 0 . 3 0 . 08037 2 . 59672 0 . 1298 4 0 .01507 0 .19267 0 .0096 3 1.6 0 . 17 961 6 . 77014 0 . 33851 0 . 0 5 5 4 9 0 .66326 0 .03316 3 . 3 0 . 3435S 15 . 23252 0 . 76163 0 . 1 8 3 4 4 1 .88634 0 . 0 9 4 3 2

200.0

0 . 1 0 . 0 0 1 76 0 . 0 6 7 3 3 0 . 00337 0 . 0 0 0 0 6 0 .00478 o . 0 0 0 0 a O . 3 0 . 00683 0 . 2640X 0 . 0 x 3 2 0 0 . 0 0 0 2 3 o . 0 1 9 0 8 0 . O O O X 0 0 . 4 o . 02443 0 . 9 8 3 4 6 0 . 04917 0 . 0 0 0 8 8 0 . 0 7 5 5 7 0 .00033 0 . 8 0* 06983 3 ' 2 3 1 6 4 0 . 16158 0 . 0 0 3 4 8 0 . 3 9 X94 0 . 0 0 1 4 6 1.6 0 . 14191 9 .28148 0 . 46407 0 . 0 x 3 3 9 1.05385 0 . 0 0 5 3 7 3 .2 o . 22655 2 4 . 8 5 2 3 6 X . 24262 0 . 0 4 9 X x 3 .37605 0 . 0 x 6 8 8

Page 19: Tables of Stresses in Three-Layer Elastic Systemsonlinepubs.trb.org/Onlinepubs/hrbbulletin/342/342-008.pdf · with some notes on the assumptions involved in setting up the problem

194

H • 1.0

k f a 200.0

or cr -<r <r O" -O" Z | r i S i r a « a Z a r a Z a r s

k a a 0.2 O . I o . o o i 17 0 . 0 5 5 0 7 0 . 0 0 0 2 8 0 . 0 0 0 9 7 0 . 0 0 0 1 0 0 . 0 0 0 5 I O . 3 0 . 0 0 4 6 4 0 . 2 1 4 6 7 0 . 0 0 1 0 7 0 . 0 0 3 8 8 0 . 0 0 0 4 1 0 . 0 0 2 0 3 0 . 4 0 . 018 14 0 . 7 8 1 9 1 0 . 0 0 3 9 1 0 . 0 15 38 0 . 0 0 1 6 0 0 . 0 0 8 0 1 0 . 8 0 . 06766 3 . 3 8 0 5 5 0 . 0 1 1 9 0 0 . 0 5 9 5 2 0 . 0 0 6 0 7 0 . 0 3 0 3 7 1.6 0 . 3 2 9 9 4 5 . 5 7 9 4 5 0 . 0 2 7 9 0 0 . 2 12 14 0 . 0 2 0 2 8 0 . 1 0 1 4 0 3 . 2 0 . 6 2 7 1 0 9 . 3 9 5 2 9 0 . 0 4 6 4 8 0 . 6 0 0 5 6 0 . 0 4 8 4 7 0 . 2 4 2 3 6

k a a 2.0

0. I 0 . 00049 0 . 0 6 8 8 3 0 . 0 0 0 3 4 0 . 00029 0 . 00035 0 . 2 0 . 00195 0 . 2 6 9 6 6 0 . 0 0 1 3 5 o . O O I 16 0 . 001 38 0 . 4 0 . 007 46 1 . 0 0 1 3 1 0 . 0 0 5 0 1 0 . 00460 0 . 00545 0 . 8 0 . 026 47 3 . 2 4 9 7 1 0 . 0 1 6 2 5 0 . 01797 0 . 02093 I . 0 0 . 08556 8 . 9 2 4 4 2 0 . 0 4 4 6 2 0 . 066 7 I 0 • 07335 3. 2 0 . 35186 2 0 . 8 3387 0 . 1 0 4 1 7 0 . 22047 0 . 21288

o . 0 0 0 1 7 o . 0 0 0 6 9 o . 0 0 2 7 3 0 . 0 1 0 4 6 o . 0 3 6 6 8 o . 1 0 6 4 4

20.0

0 . 1 0 . 00037 0 . 08469 0 . 00042 0 . 0 0 0 0 7 0 . 0006 2 0 . 0 0 0 0 3 0 . 2 0 . 001 04 0 . 33312 0 . 00167 o » 00028 0 . 00248 0 . 0 0 0 1 3 0 . 4 0 . 00384 1 . 25495 0 . 006 2 7 o » 001 10 0 . 0098 5 0 . 0 0 0 4 9 0 .8 0 . 0 13 36 4 . 26 100 0 . 02 1 30 0 . 0 0 4 3 6 0 . 03825 0 . 0 0 1 9 1 1 . 6 0 . 03379 1 3 . 91S09 0 . 06459 0 . 0 1 6 8 3 0 . 13989 0 . 0 0 6 99 3 .3 0 . 08859 3 6 . 04291 0 . 18021 0 . 06 16 7 0 . 45544 0 . 0 2 2 7 7

200.0

e. 1 0 . 0 0 0 3 I 0 . 1007 5 0 . 00050 0 . 00002 0 . ooo3 7 0 . 00000 0 . 2 0.00083 0 . 39741 0 . 00199 0 . 00006 0 . 00347 0 . 0000 2 0* 4 0 . 0 0 2 9 8 I . 51234 0 . 00756 0 . 00025 0 . 01 38 1 0 . 00007 0 . 3 0 . 0 0 8 9 3 5 ' 28939 0 . 02645 0 . 00100 0 . 05403 0 . 00027 1.6 0 . 0 2 0 6 5 I ? ' 01872 0 . 08 509 0 . 00393 0 . 20250 0 . 00101 3 . 2 0 . 0 4 1 5 4 5 2 . 236 15 0 . 26118 0 . 01505 0 . 70098 0 . 00350

Page 20: Tables of Stresses in Three-Layer Elastic Systemsonlinepubs.trb.org/Onlinepubs/hrbbulletin/342/342-008.pdf · with some notes on the assumptions involved in setting up the problem

195

H 2.0

0.2

<r ^ 2 l

2 « n 81 r a 2 a 2 a r a 2 a rj k a • 0.2

O . I 0 . 0 0 5 4 0 0 . 0 0 1 2 1 0 . 0 0 6 0 4 0 . 0 0 2 4 a 0 . 0 0 0 6 0 0 . 0 0 3 0 3 O . 2 0 . 0 2 1 3 8 0 . 0 0 4 7 7 0 . 0 2 386 0 . 0 0 9 6 4 0 . 0 0 3 4 0 0 . 0 1 3 0 2 0 . 4 0 . 0 8 2 0 9 0 . 0 1 8 2 1 0 . 0 9 1 0 6 0 . 0 3 7 7 0 0 . 0 0 9 3 9 0 . 0 4 6 9 5 o . 8 0 . 2 8 1 5 0 0 . 0 6 1 0 6 0 . 3 0 5 3 1 0 . 1 3 8 3 3 0 . 0 3 4 2 2 0 . I 7 I I 2 1.6 0 . 68908 0 . 1 3 6 6 0 0 . 6 8 2 9 9 0 . 4 0 8 30 0 . 0 9 8 2 6 . 0 . 4 9 1 3 1 3 .2 0 . 9 3 1 0 3 0 . 1 2 8 9 9 0 . 6 4 4 9 3 0 . 7 3 4 9 6 0 . 1 5 7 0 5 0 . 78523

k a B 2.0

0 . 1 0 . 00502 0 . 00098 0 . 0 0 4 9 4 0 . 0 0 x 8 0 0 . 0 0 3 3 9 0 . o o x 70 0 . 2 0 . 01986 0 . 00389 0 . 0 1 9 5 3 0 . 0 0 7 x6 0 . o x 350 0 . 0 0 6 7 5 o . 4 0 . 076 30 0 . 01485 0 . 0 7 4 4 9 0 . 0 2 8 15 0 . 0 5 2 8 8 0 . 0 2 6 4 4 0 . 8 0 . 26196 0 . 04977 0 . 2 4 8 7 5 o . 1 0 5 2 3 o . X 9 4 6 7 0 . 0 9 7 3 3 1.6 0 . 63535 0 . 10924 0 . 5 4 6 4 1 0 . 3 3 0 7 5 0 , 5 7 8 1 X o . 2 8 9 0 5 3 . 2 0 . 87025 0 . 12296 0 . 6 1 4 6 2 0 . 6 8 3 3 3 I . 0 0 x 9 9 0 . 5 0 x 0 0

k a B 20.0

0 . X 0 . 00444 0 . 0 0 0 5 6 0 . 0028 2 0 . 0006 5 0 . 0 0 8 2 5 0 . 0004X 0 . 2 0 . 0x756 0 . 0 0 2 2 1 0 . 01x05 0 . 00260 o . 0 3 2 8 6 0 . 00x64 0 . 4 0 . 06706 0.oo3 X9 0 . 04097 o . 01030 0 . X 2 9 3 3 0 . 00647 0 . 8 0 . 2256 X 0 . 0 2 4 3 1 0 . 12153 0 . 03956 0 . 4 8 5 9 5 , 0 . 02430 1.6 0 . 51929 0 . 0 3 0 7 0 0 . 15352 0 . 13743 1 .55804 0 . 07790 3 . 2 0 . 6 5 7 0 0 — 0 . 0 0 9 2 6 — 0 . 04632 0 . 37409 3 . 3 9 8 8 3 0 . 16994

k a B 200.0

0 . 1 0 . 00414 0 . 0 0 0 3 2 0 . 0 0 1 6 0 0 . o o o x 5 0 . 01234 o . 00006 0 . 2 o . 01635 0 . 0 0 x 2 4 o . 0 0 6 2 1 0 . 0 0 0 5 8 o . 04922 0 . 0002 5 0 . 4 0 . 06 231 0 . 0 0 4 3 6 0 . 0 2 1 8 0 0 . 0 0 2 3 1 0 . 19450

74256 0 . 00097

0 .3 0 . 20757 0 . 0 0 9 5 5 0 . 0 4 7 7 4 0 . 0 0 9 0 5 0 . 19450 74256 o . 0037 1

X . 6 0 . 45550 - 0 . 0 2 1 7 2 - 0 . 1 0 8 6 I 0 . 0 3 3 6 3 2 . 52847 0 . 01264 3 . 2 0 . 48642 - 0 . 1 5 5 8 9 - 0 . 7 7 9 4 4 0 . 1 1 1 0 5 6 . 69835 o . 03349

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196

H •

k , -

2.0

2.0

<r <r <r -cr 0- - 0 : S i r t S t r a S a S a r a S a r s

k a a 0. O . I 0 , 0 0 3 56 0 . 0 0 5 4 5 0 . 0 0 2 7 2 0 , 0 0 3 16 0 . 0 0 0 4 1 0 , 0 0 2 0 3 0 , 2 0 , 0 1 4 1 5 0 . 0 2 1 5 5 0 . 0 : 0 7 8 0 ,oo36I 0 . 0 0 1 6 2 0 , 0 0 8 09 o, 4 0 . 0 5 4 9 3 o,08 266 0 . 0 4 1 3 3 0 , 0 3 3 8 6 0 . 0 0 6 34 0 . 0 3 1 7 2 0 ,8 0 , 1 9 6 6 1 0 . 2 3 226 0 . 1 4 1 1 3 0 . 1 2 7 0 2 0 . 0 3 3 4 9 0 . 1 1 7 4 4 1,6 0 , 5 5 3 0 6 0 . 6 7 8 4 4 0 . 3 3 9 2 2 0 , 4 0 3 7 6 0 . 07109 o . 3 5 5 4 5 3 . 2 0 , 9 6 6 47 0 . 7 9 3 9 3 0 . 3 9 6 9 6 0 , 8 3 1 9 7 0 . 1 2 5 8 3 0 . 6 2 9 1 3

k a a 2.1

O , 1 0 . 0 0 2 50 0 . 0 0 5 5 5 0 . 0 0 2 7 8 0 . 0 0 1 0 0 0.ooi83 0 . 0 0 0 9 4 O , 2 0 . 0 0 9 9 1 0 . 0 2 1 9 9 0 . 0 1 0 9 9 0 . 0 0 3 9 7 0 . 0 0 7 50 0 . 0 0 3 7 5 0 . 4 0 . 0 3 8 3 2 0 . o3 46 5 0 . 0 4 2 3 1 0 . 0 1 5 6 9 0 . 0 2 9 5 0 0 . 0 1 4 7 5 0 ,3 0 . 1 3 5 1 6 0 . 2 9 3 6 5 0 . 1 4 6 8 3 0 , 0 5 9 7 4 0.11o3 0 0 . 0 5 5 4 0 1,6 0 . 366^4 0 . 7 5 0 8 7 0 . 3 7 5 4 2 0 , 2 0 1 4 5 0 . 3 5 5 1 5 0 , 1 7 7 5 7 3 . 3 0 . 6 7 3 8 4 I . 1 7 2 9 4 0 . 5 8 6 4 7 0 , 5 1 1 5 6 0 , 7 7 4 3 4 0 , 3 8 7 17

k a a 20.0

0 . 1 0 . o o i 3 I 0 . 006 52 0 . 00326 0 . 0 0 0 3 5 0 . 00378 0 . 0 0 0 1 9 0 . 3 0 . 007 16 0 . 02586 0 . 01293 0 . 0 0 0 9 0 0 . 01507 0 . 0 0 0 7 5 0 . 4 0 , 027 46 0 . 10017 0 . 05007 0 . 0 0 3 9 4 0 . 05958 0 . 0 0 2 9 8 0 . 8 0 . 09396 0 . 35641 0 . 17821 0 . 0 1 5 3 5 0 , 22795 0 . 0 1 1 4 0 1.6 0 , 33065 I . 0078 5 0 . 50392 0 , 0 5 5 99 0 , 73347 0 . 0 3 9 1 7 3 « 3 0 , 37001 2 . 16033 I . 08017 0 . 1 7 8 4 3 2 . 13215 0 . 1 0 6 6 I

k a » 200,0

0, 1 o. 00164 00647

0 . 00778 0 . 00389 0 . 00005 0 . 00542 0 . 00003 0 , 2 0 ,

00164 00647 0 . 03090 0 . 01544 0 . 0002 1 0 . 02163 0 , 000 11

0 , 4 0 , 02470 0 . 12030 0 . 06 014 0 . 0008 5 0 . 08 578 0 , 00043 0 , 3 0 , 08 3 26 0 . 43693 0 . 21847 0 . 00335 0 . 33214 0 . 00166 1 , 6 0 . 19224 I . 32870 0 . 66434 0 . 0 I 28 3 I . 19190 0 . 00 5 96 3« 2 0 . 2 5 5 26 3 ' 4066 4 1 . 70332 0 . 0 46 I 2 3 . 67558 0 . 01838

Page 22: Tables of Stresses in Three-Layer Elastic Systemsonlinepubs.trb.org/Onlinepubs/hrbbulletin/342/342-008.pdf · with some notes on the assumptions involved in setting up the problem

197

H

k i

2.0

20.0

' 8 l S i n O" - o r

S i r « S t S t r a

O . 1 0. ool 34 0. 00968 0 .00048 o .00108 0* 00014 O . 3 o. 00533 0 . 03839 0 .00192 0 . 0 0 4 2 9 0. 00055 o. 4 0. 021 00 0 . 14845 0 .00741 0 . 0 1 7 0 2 0. 00216 0 .8 o. 07950 0. 52414 0 .02621 0 .06 576 0. 008 20 X . 6 0. 266 1 3 1 . 41720 0 .07085 0 .23186 0. 02740 3 . 2 0 . 67883 2 . 38258 0 .11913 0 .6 3006 0. 06384

r j S t

k a B 0.2 o.ooo63 0 . 0 0 2 7 3 o. 01078 0 .04101 o.13698 o .31919

k t 2.0

0 .1 0 . 00059 o . 01219 0 .0006 I 0 .00033 0 .00051 0. 00035 0 . 2 0. 0033 5 0 . 04843 0 .00242 0 . 0 0 1 3 0 0 .00203 0. 00101 0 . 4 0. 00922 0. 18857 0 .00943 0 .005 18 0 .00803 0. 00401 0 .8 o . 03412 0. 68383 0 .03419 0 .02022 0 .03093 0. 01547 1.6 o . 10918 3 . 04134' 0 .10207 0 .07444 0 .10864 0. 05432 3 . 2 0 . 39183 4 . 60426 0 .33021 0 .23853 0 .30709 0. 15354

k . B 20.0

0. 1 0. 00033 0 . 01568 0 .00078 0 .00008 0 . 0 0 0 9 4 0. 00005 0 . 3 0 . 00130 0 . 06236 0 .00312 0. 00031 0 .00374 0. 00019 0 . 4 0. 00503 0. 24425 O . 0133 I 0 . 0 0 1 2 3 0 .01486 0. 0007 4 0 .8 0 . 01783 0 . 90594 0 .04530 0 .0048 5 0 . 0 5 7 8 9 0. 00389 1.6 0 . 05013 2 . 91994 0 . 1 4 6 0 0 0 .01863 0 . 2 1 1 9 0 0 . 01060 3 .2 0. 11331 7. 95104 0 .39755 0 .06728 0 .67732 0. 03387

200.0

0.1 0. 00027 o. 01937 0. 00096 0 . 0 0 0 0 2 0 .00131 o. 00001 0. 3 0 . 00196 0 . 07675 0. 00384 0 . 0 0 0 0 7 0 .00524 0. 00003 0. 4 0 . 00406 0 . 30182 0. 01509 0 .00028 0 .02085 0. 00010 0 . 3 0 . 01397 I . 13555 0. 05673 0 .oo l10 0 . 0 8 1 8 0 0. 00041 1.6 0. 03538 3 . 83254 0 . 19163 0 .00431 0 .30676 0. 00153 3 . 2 0. 06183 11. 55403 0 . 57770 oi01644 1 .04794 0. 00524

Page 23: Tables of Stresses in Three-Layer Elastic Systemsonlinepubs.trb.org/Onlinepubs/hrbbulletin/342/342-008.pdf · with some notes on the assumptions involved in setting up the problem

198

H » 2.0

k i » 200.0

cr . 0" - a <r <r <r 2 l 2 i Ti a t r a 2 2 2 a r a za r s

k . B 0.2 0 . I 0 . 0 0 0 3 6 0 . 0 1 3 5 0 0 . 00007 0 . 0 0 0 3 3 0 . 0 0 0 0 3 0 . 0001 5 O . 2 0 . 00144 0 . 0 5 3 6 6 0 . 00027 0 . 0 0 1 3 0 0 . 0 0 0 1 2 0 . 00058 o . 4 0 . 0 0 5 7 2 0 . 2 0 9 1 1 0 . 00105 0 . 0 0 5 1 8 0 . 0 0 0 4 6 0 . 00232 0 . 8 0 . 0 2 2 3 1 0 . 7 6 0 3 5 0 . 00380 0 . 0 2 0 3 8 0 . 0 0 1 8 0 0 . 0090 I 1.6 0 . 08 215 2 . 2 9 6 42 0 . 01148 0 . 0 7 6 7 5 0 . 0 0 6 49 0 • 03244 3 . 2 0 . 2 6 576 5 . 2 8 5 3 9 0 . 0 2 6 4 3 0 . 2543. ; 0 . 01912 0 . 0956 3

ka s 2.0

0 . 1 0 . 0 0 0 1 1 0 . 0 1 7 3 7 0 . 00009 0 . o o o o 3 0 . 0 0 0 0 9 0 . 00004 0 . 2 0 . 0 0 0 4 5 0 . 0 6 9 1 3 0 . 00035 0 . 0 0 0 3 3 0 . 0 0 0 3 6 0 . 00018 o . 4 0 . 0 0 1 7 9 0 . 3 7 1 0 3 0 . 00136 0 . 0 0 1 3 I 0 . 0 0 1 4 2 0 . 0007 I 0 . 8 0 . 0 0 6 8 5 1.008 o3 0 . 00504 0 . 0 0 5 2 0 0 . 0 0 5 5 3 0 . 00377 1.6 0 . 0 2 4 4 1 3 . 2 7 5 9 0 0 . 016 38 0 . 0 3 0 0 3 0 . 0 2 0 4 3 0 . 0 I 03 I 3 . 2 0 . 08 061 9 . 0 2 1 9 5 0 . 04511 0 . 0 7 3 ^ 3 0 . 0 6 6 38 0 . 03319

k . » 20.0

0 . 1 0 . 0 0 0 0 5 0 . 0 2 1 6 0 0 . 0001 I 0 . 0 0 0 0 3 0 . 0 0 0 1 4 0 . 0000 r 0* 2 0 . 0 0 0 x8 0 . 0 8 6 0 4 0 . 00043 0 . 0 0 0 0 7 0 . 0 0 0 5 8 0 . 00003 0 . 4 0 . 0 0 0 7 X 0 . 3 3 8 6 6 0 . 0016 9 0 . 0 0 0 3 0 0 . 0 0 2 3 9 0 . 00011 0 . 8 0 . 0 0 2 6 I 1.27835 0 . 006 39 0 . 0 0 1 1 9 0 . 0 0 9 0 1 0 . 00045 1.6 0 . 0 0 8 19 4 . 3 5 3 1 1 0 . 02 177 0 . 0 0 46 7 0 . 0 3 3 9 0 0 . 00170 3-2 0 . 02341 1 3 . 2 6 8 7 3 0 . 06634 0 . 0 1 7 8 4 0 . 11666 0 . 00583

k . = 200.0

O . 1 0 . 00003 0 . 0 2 5 8 7 0 . 0001 3 0 . 0 0 0 0 0 0 . 0 0 0 1 9 0 . 00000 O . 2 0 . 0 0 0 1 2 0 . 1 0 3 1 0 0 . 0005 3 0 .OO003 0 . 0 0 0 7 5 0 . 00000 0 . 4 0 . 00047 0 . 4 0 6 76 0 . 00203 0 . 0 0 0 0 7 0 . 0 0 3 0 0 0 . 0 0 0 0 3 0 . 8 0 . 0 0 1 6 5 1 . 5 4 9 5 1 0 . 00775 0 . 0 0 0 2 6 0 . 0 1 1 8 3 0 . 00006 1.6 0 . 00445 5 . 4 3 7 0 5 0 . 02719 0 . 0 0 1 0 4 0 . 0 4 5 1 5 0 . 00033 3 ' 2 o . 0 0 9 2 9 17 .583 10 0 . 08794 0 . 0 0 4 0 9 0 . 16 I 07 0 . 0008 I

Page 24: Tables of Stresses in Three-Layer Elastic Systemsonlinepubs.trb.org/Onlinepubs/hrbbulletin/342/342-008.pdf · with some notes on the assumptions involved in setting up the problem

199

H 4*0

0.2

a i cr a- <r cr z t r i » i r a S a * » r a • a r s

k a a 0.2 0 . I 0 . 0 0 1 3 9 0 . 00028 0 . 00141 0 . 00086 0 . 0 0 0 2 3 0 . 0 0 1 1 4 0 . 2 0 . 0 0 5 5 5 0 . 00112 0 . 0056 2 0 . 00345 0 . 0 0 0 9 1 0 . 0 0 4 5 4 0 . 4 0 . 02 1 98 0 . 004 0 . 0 2 2 3 0 0 . 01371 0 . 0 0 3 6 0 0 . o i S o i 0 . 8 0 . 08435 0 . 016 3 0 0 . 06 428 0 . 05323 0 . 0 1 3 9 4 0 . 0 6 9 6 8 1.6 0 . 28870 0 . 05529 0 . 27647 0 . 19003 0 . 0 4 9 0 9 0 . 2 4 5 4 5 3-2 0 . 7 0 0 7 4 0 . 11356 0 . 56778 0 . 51882 0 . 1 2 6 7 0 0 . 6 3 3 5 2

k a a 2.0

0. I 0 . 0 0 1 3 3 0 . 00026 0 . OOI 31 0 . 0007 1 0 . 0 0 1 30 0 . 0 0 0 6 5 0 . 2 0 . 0 0 4 9 1 0 . 001 04 0 . 0052 I 0 . 00283 0 . 0 0 5 1 8 0 . 0 0 2 5 9 0 . 4 0 . 0 1 9 4 2 0 . 0 0 4 12 0 . 02059 0 . 01126 0 . 0 2 0 5 7 0 . 0 1 0 2 8 0 .3 0 . 0 7 4 4 7 0 . 01574 0 . 07 56 9 0 . 04333 0 . 0 7 9 7 7 0 . 0 3 9 8 9 1.6 0 . 2 5 4 4 9 0 . 05311 0 . 26554 0 . 1 5 9 0 ; 0 . 3 8 3 5 7 0 . 1 4 1 7 8 3 . 3 0 . 6 2 0 7 4 0 . 1252-; 0 . 62622 0 . 4545 5 0 . 7 5 6 5 1 0 . 3 7 8 2 5

k a a 20.0

0. I 0 .000c 7 0 . 0 0 013 0 . 00090 0 . 0 0 0 2 3 0 . 0 0 3 2 5 0 . 0 0 0 1 6 0* 2 0 . 0 0 3 46 0 . 00072 0 . 00353 0 . 00111 0 . 0 1 2 9 0 0 . 0 0 0 6 5 0 . 4 0 . 0 1 3 6 7 0 . 00283 0 . 01.1,17 0 . 00443 0 . 0 5 1 5 9 0 . 0 0 3 5 8 0 . 8 0 . 0 5 2 0 7 0 . 0 100 9 0 . 05444 0 . 0 1 7 4 1 0 . 2 0 1 3 4 0 . 0 1 0 0 7 1.6 0 . 17367 0 . 03790 0 . 18949 0 . 06 5 3 5 0 . 7 3 3 2 3 0 . 0 3 6 6 6 3-2 o- 3^955 0 . 108^ I 0 . 54303 0 . 2000 5 2 . 1 3 6 6 6 0 . I 063 3

k a a 200.0

0 . I 0 . 0 0 0 6 9 0 . 00019 0 . 00097 0 . 00000 0 . 0 0 4 8 7 0 . 0 0 0 0 3 0 . 2 0 . 0 0 2 7 4 0 . 00078 0 . 0038 9 0 . 0002 ] 0 . 0 1 9 4 7 0 . 0 0 0 1 0 0 • A 0 . 0 1 0 7 9 0 . 00309 0 . 01544 0 . 00095 0 . 0 7 7 5 2 0 . 0 0 0 3 9 o.S 0 . 0 4 0 7 4 0 . 01199 0 . 05995 0 . 00378 0 . 3 0 4 3 2 0.00153 1.6 0 . I 311 7 0 . 04352 0 . 21753 0 . 01456 I.13373 0 . 0 0 5 6 7 3 . 2 0 . 2 6 403 0 . 14445 0 . 72224 0 . 05 16 1 3 . 59608 0 . 0 1 7 9 8

Page 25: Tables of Stresses in Three-Layer Elastic Systemsonlinepubs.trb.org/Onlinepubs/hrbbulletin/342/342-008.pdf · with some notes on the assumptions involved in setting up the problem

200

H 4.0

2.0

a i « i r i

cr -o* 2 t r t S t r t S t

k , - 0.2 0 . 1 0 . 001 03 0 . 00123 0. 0006 4 0 . 00078 0 . 00014 0 . 00071 O. 2 0 . 00411 0 . 005 11 0 . 00256 0 . 00312 0 . 00057 0 . 00284 0 . 4 0 . 01631 0 . 0 3 0 2 3 0 . o i o i 1 0 . 01241 0 . 00226 0 . 01129 0 . 3 0 . 06319 0 . 07722 0 . 0386 I 0 . 04842 0 . 00877 0 . 04 3^ 4 1.6 0 . 32413 0 . 2595s 0 . 12977 0 . 17617 0 . 03133 0 . 15666 3 ' 2 0 . 6 06 5 4 0 . 58704 0 . 29352 0 . 50917 0 . o3 500 0 . 42501

k t 2.0

0 . 1 0 . 00057 0 . 001 47 0 . 00074 0 . 0003. ; 0 . 0006 5 0 . 00032 0 . 2 0 . 00223 0 . 00587 0 . 00293 0 . 00137 0 . 00260 0 . 00130 0 . 'f 0. 00005 0 . 02324 0 . 01162 0 . 00544 0 . 01032 0 . 00516 0 . 8 0 . 03500 0 . 08957 0 . 04479 0 . 02135 0 . 04031 0 . 02015 1 . 6 0 . 12354 0 • 31315 0 . 1 5 6 0 0 0 . 07972 0 . 14735 0 . 07368 3 . 2 0 . 3 412 1 0 . 3 1908 0 . 40054 0 . 0 . 43632 0 . 21816

k a » 20.

o . I 0 . 00030 0 . 00201 0 . 001 0 I 0 . ooooS 0 . 00 1 28 0 . 00006 0 . 2 0 . 00119 0 . 00803 0 . 0 0,;. 0 2 0 . 00034 0 . 00510 0 . 00036 0 . 4 0 . 0 0 46 0 0 . 03191 0 . 01596 0 . 00134 0 . 03032 0 . 00 102 0 . 8 0 . 01700 0 . 12427 0 . 06 21 3 0 . 00533 0 . 07991 0 . 00400 1 . 6 0 . 06045 0 . 45100 0 . 22550 0 . 02049 0 . 29901 0 . 01500 3 ' 2 0 . I 4 P 7 9 I . 36437 0 . 68214 0 . 07294 0 . 07701 0 . 04885

k t » 200.

0 . 1 0 . 00023 0 . 0026 3 0 . 00131 0 . 00002 0 . 001 '3 0 0 . 00001 0 . 2 0 . 00091 0 . 01050 0 . 00535 0 . 00007 0 • 00720 0 . 00004 0 . *t 0 . 00360 0 . 04179 0 . 02000 0 . 00020 0 . 02870 0 . 0001 0 . 8 0 . 01360 0 . 1S3O0 0 . o3 190 0 . 0 0 1 1 5 0 . I I 3 3 4 0 . 00057 1 . 6 0 . 04409 o . 60898 0 . 30449 0 . 00451 0 . 43351 0 . 002 16 3 . 2 0 . 00323 1 . 988 99 0 . 99449 0 . 01705 1 . 49306 0 . 00747

Page 26: Tables of Stresses in Three-Layer Elastic Systemsonlinepubs.trb.org/Onlinepubs/hrbbulletin/342/342-008.pdf · with some notes on the assumptions involved in setting up the problem

201

H - 4 .0

kf • 20.0

cr <r -cr or <r -or 0* >ar Si ra «« r t «• r»

k i » 0 .2 0. I 0 .00042 0 .00233 0 .00012 0. 00037 0 .00004 0 .00021 0. 2 0. 0 0 16 5 0 .009 3 2 0 .00047 0. 00148 0 .00017 0 .0008 5 0. 4 0 .0066 3 0 .03602 0 .0018 5 0 > 00533 0 .00068 0 . 0 0 3 4 0 0. 8 0 . 02603 0 .14242 0 .00713 0. 02319 0 .00266 0 .01331 I . 6 0. 097 13 0 • 4 9 0 2 6 0 .02491 0. 087 58 0 .0098 3 0 .04914 3» 3 0. 31040 I . 3 1 6 2 7 0 . 06 58 I 0. 28747 0 .02990 0 .14951

k i « 2.0

0. r 0 .00013 0 .00312 0 .00016 0. 0001 0 0 .00015 0 . 0 0 0 0 7 0. 2 0 .00054 0 .01245 0 .00063 0. 00039 0 .00059 0 . 0 0 0 3 9 0. 1

*(• 0 . 0 0 2 14 0 .04944 0 .00247 0. 00154 0 .002 35 0 .00117

o. 8 0 .oo3 37 0 .19247 0 .0096 2 0 . 006 I 0 0 .00924 0 .0046 3 I . 6 0 . 0 3 1 0 0 0 . 6 0 7 4 9 0 .03487 0. 02353 0 .03488 0 .01744 3« 2 0. I 01 40 2 .09049 0 .10453 0. 08444 0 .11553 0 .05776

20.0

0. 1 0. 00005 0. 00 -,13 0. 0002 1 0. 00002 0. 0 0 0 3 5 0. 00001 0 . 3 0. 0 0 0 3 1 0. 016 5 I 0. ooo3 3 0. 00009 0 . 00099 0. 00005 0 .4 0 . ooo3 3 0. 06 569 0. 00338 0. 00035 0 . 00396 0 . 0 0 0 3 0

0. 8 0. 00321 0. 25739 0. 01387 0. 00x38 0. 01565 0 . 00078 1.6 0. 01130 0 . 056 2 3 0. 0470 I 0 . 00542 0. 05993 0. 00300 3* 2 0. 03258 3» 1098 0 0 . 15549 0. 0206 1 0. 20906 0 . 01045

k« a 200.0

0. I 0. 00003 0. 00515 0 . 0 0 0 3 0 0. 00000 0. 00033 0 . 00000 0 .3 0. 0 00 1/. 0. 0 3 0 56 0 . 00103 0. 00002 0. 00131 0. 00001 0. 4 0 . 0005.1 0. 08 I 9 I 0. 0041 0 0. 00008 0 . 00524 0. 00003 0 .3 0. 0 0 2 06 0. 32231 0. 01613 0* 00030 0. 0207 7 0. 00010 1.6 0 . 0068 3 1. 21587 0. 06 07 9 0. 00120 0. 08034 0 . 00040 3*2 0 . 0 15 90 4. i v395 0. 30720 0. 00468 0. 2896 1 0 . 00145

Page 27: Tables of Stresses in Three-Layer Elastic Systemsonlinepubs.trb.org/Onlinepubs/hrbbulletin/342/342-008.pdf · with some notes on the assumptions involved in setting up the problem

202

H - 4 .0

kf a 200.0

<r -cr or -<r cr tr -or St r i « t r s

kt » 0.2 0* 0. O O O I 0 0 .00334 0 .00002 0. 00010 0 . 00001 0 .00004 0. 2 0. O 0 O / f 2 0 .01333 0 .00007 0* 00039 0* 00003 0 .00016 0. 4 0. 0 0 1 6 7 0 .05295 0 .00026 0. 00157 0 . 00013 0 .0006 5 0* 8 0. 00663 0. 2 oS 2 I 0. 00103 0* 006 25 0. 0005 I 0 .00256 I . 6 0 . 02562 0 . 74824 0 . 0 0 3 7 4 0. 02427 0. 00195 0 .00975 3« 2 0 .09166 2. 25 046 0 .01125 0. 08 799 0 . 0 0 6 6 0 0 .03298

ka s 2.0

0. I 0. 00003 0 .00437 0 .00002 0 . 00002 0. 00002 0 .00001 0. 2 0 . 0001 I 0 .017 'A 0 .00009 0 . 00009 0. 00009 0 .00005 0 . 4 0. O O O . ! 2 0 .06947 0 .00035 0 .00036 0. 00036 0 .00018 o. 8 0 .00168 0 .27221 0 .00136 0. 00142 0 . 001 44 0 .00072 1.6 0 .006 46 1 .01140 0 .00506 0* 00560 0. 00553 0 .00277 3» 2 0 . 0 2 3 3 2 3 .28913 0 .01645 0 . 02126 0* 01951 0 .0097 5

ka « 20.0

0. I 0 .00001 0 .00545 0 .00003 0. 00000 0. 00003 0 . 0 0 0 0 0 0* 2 0 .00003 0. 02178 0 .00011 0 . 0 0 0 0 2 0. 00014 0 .00001 0. 4 0. 0001 3 0. 08673 0 .00043 0 . oooo3 0. 00054 0 .00003 0 . 8 0 . 0 0 0 5 0 o« 3413 I 0 .00171 0. 0003 I 0. 00215 0 .00011 I . 6 0 .00136 1 .28773 0 .00644 0. 00124 0 . 00833 0 . 0 0 0 4 2 3' 2 0 .006 I 2 4 .38974 0 .02195 0 . 00483 0. 03010 0 . 0 0 1 5 0

ka a 200.0

0. I 0 . 0 0 0 0 0 0 .006 52 0 . 0 0 0 0 3 0 . 00000 0. 00004 0 . 0 0 0 0 0 o. 2 0 . 00002 0 .026 06 0 .00013 0 . 00000 0. 00017 0 . 0 0 0 0 0 o. 4 0 .00007 0 .10389 0 . 0 0 0 5 2 0* 00002 0. ooo38 0 . 0 0 0 0 0 0 . 8 0 .0002 5 0. 40997 0 . 0 0 2 0 5 0. 00007 0 . 00269 0 .00001 1.6 o« 000S6 r . 5 6 2 8 4 o .0078 I 0. 00027 0. 01049 0 . 0 0 0 0 5 3* 2 0 . 0 0 2 2 5 5 . 48870 0 .027^4 0. 001 07 0. 03866 0 . 0 0 0 1 9

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203

R 8.0

0 .2

<r OB -<r 1 ri 2i r« I t r t

ka s 0 .2 0 . I O . 2 0 . 4 0 . 8 1 . 6 3 . 2

0 . 0 0 0 3 5 0 . 0 0 1 4 2 0 . 0 0 5 6 6 0 . 0 2 2 4 0 0 . 0 8 5 8 9 0 . 2 9 3 1 8

0 . 0 0 0 0 6 0 . 0 0 0 2 3 0 . 0 0 0 9 0 0 . 0 0 3 5 4 0 . 0 1 3 3 5 0 . 0 4 2 7 0

0 . 0 0 0 2 8 0 . 0 0 1 1 3 0 . 0 0 4 4 9 0 . 0 1 7 6 9 0 . 0 6 6 7 3 0 . 2 1 3 5 0

0 . 0 0 0 2 7 0 . o o i o S 0 . 0 0 4 3 2 0 . 0 1 7 1 1 0 . 0 6 6 10 0 . 2 3 1 8 2

0 . 0 0 0 0 7 0 . 0 0 0 2 8 0 . 0 0 1 1 3 0 . 0 0 4 4 9 0 . 0 1 7 2 5 0 . 0 5 9 0 7

0 . 0 0 0 3 6 0 . 0 0 1 4 2 0 . 0 0 5 6 7 0 . 0 2 2 4 6 0 . 0 8 6 24 0 . 2 9 5 3 3

2.0

0 . 1 0 . 0 0 0 3 0 0 . 0 0 0 0 8 0 . 0 0 0 3 8 0 . 0 0 0 2 3 0 . 0 0 0 4 1 0 . 0 0 0 2 1 0 . 2 0 . 0 0 1 2 0 0 . 0 0 0 3 0 0 . 0 0 1 5 2 0 . 0 0 0 9 1 0 . 0 0 1 6 5 0 . 0 0 0 8 3 0 . 4 0 . 0 0 4 7 9 0 . 0 0 1 2 1 0 . 0 0 6 0 6 0 . 0 0 3 6 4 0 . 0 0 6 6 0 0 . 0 0 3 3 0 0 . 8 0 . 0 1 8 9 4 0 . 0 0 4 8 0 0 . 0 2 3 9 9 0 . 0 1 4 4 6 0 . 0 2 6 1 6 0 . 0 1 3 0 8 1 . 6 0 . 07 271 0 . 0 1 8 41 0 . 0 9 2 0 6 0 . 0 5 6 0 1 0 . 1 0 0 8 0 0 . 0 5 0 4 0 3 . 2 0 . 2 4 9 3 3 0 . 0 6 3 0 7 0 . 3 1 5 3 4 0 . 1 9 8 2 8 0 . 3 5 0 0 8 0 . 1 7 5 0 4

ka a 20.0

0 . I 0 . 0 0 0 1 6 0 . OOOIO 0 . 0 0 0 4 9 0 . 0 0 0 0 9 0 . 0 0 1 0 5 0 . 0 0 0 0 5 0 . 2 0 . 0 0 0 6 5 0 . 0 0 0 4 0 0 . 0 0 1 9 8 0 . 0 0 0 3 7 0 . 0 0 4 2 X o . 0 0 0 2 I 0 . 4 0 . 0 0 2 6 0 0 . 0 0 1 5 8 0 . 0 0 7 9 0 0 . 0 0 1 4 9 0 . 0 1 6 7 9 0 . 0 0 0 8 4 0 . 3 0 . 0 1 0 2 6 0 . 006 29 0 . 0 3 1 4 3 o» 0 0 5 9 4 0 . 0 6 6 6 4

0 . 2 5 8 7 1 0 . 0 0 3 3 3

I . 6 0 . 0 3 9 2 6 0 . 0 2 4 6 3 0 . I 2 3 I 4 0 . 0 2 3 2 0 0 . 0 6 6 6 4 0 . 2 5 8 7 1 0 . 0 1 2 9 4

3 . 2 0 . 1 3 3 3 5 Q. 0 9 1 2 3 0 . 4 5 6 1 5 0 . 0 8 5 1 0 0 . 9 2 4 7 8 o . 0 ',6 2 4

200.0

0 . 1 0 . 0 0 0 0 9 0 . 0 0 0 1 5 0 . 0 0 0 7 4 0 . 0 0 0 0 2 0 . 0 0 1 6 2 0 . 0 0 0 0 1 O. 2 o . 0 0 0 3 6 o . 0 0 0 5 9 0 . 0 0 2 9 4 0 . 0 0 0 0 8 0 . 0 0 6 48 0 . 0 0 0 0 3 0 . 4 0 . 0 0 1 4 5 0 . 0 0 2 3 5 0 . 0 1 1 7 6 o . 0 0 0 3 2 0 . 0 2 5 8 7 0 . 0 0 0 1 3 0 . 8 0 . 0 0 5 7 3 0 . 0 0 9 3 3 0 . 0 4 6 9 0 0 . 0 0 1 3 7 0 . 1 0 2 8 7 0 . 0 0 0 5 1 1 . 6 0 . 03 1 6 0 0 . 0 3 7 1 0 0 . 1 8 5 4 9 0 . 0 0 5 0 3 0 . 4 0 2 38 0 . 0 0 2 0 1 3 . 2 0 . 0 6 9 3 8 0 . I 4 2 3 6 0 . 7 1 1 3 0 0 . 0 1 9 1 2 1. 4 8 0 9 7 0 . 0 0 7 4 0

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204

H 8 .0

2.0

at cr cr «i St z%

k. a 0 .2

O . I 0 . 0 0 0 2 8 0 .00028 0 .00014 0 .00024 0 . 0 0 0 0 4 0 . ooo^a 0 . 2 0 . 0 0 1 1 3 0. 0 0 1 I I 0 .00056 0 .00096 0 . 0 0 0 1 7 0 . 0008 7 0. 4 0 .00451 0•00444 0 .00222 0 . 0 0 3 8 4 0 .0006 9 0 . 00347 0 .8 0 .01706 0 .01752 0 .00S76 0 . 0 1 5 2 2 0 .00275 0. 01373 1.6 0 . 0 6 8 9 5 0 .06662 0 .03331 0 . 0 5 9 0 0 0 . 0 1 0 6 0 0. 05298 3*2 0 .24127 0 .22014 0 .11007 0 . 2 0 9 4 9 0 . 036 0 3 0. 18466

ks » 2.0

0. I 0 . 0 0 0 1 3 0 .00039 0 . 0 0 0 2 0 0 . 0 0 0 1 0 o» 00020 0 . 0 0 0 1 0 O . 2 0 .00053 0 .00157 0 .00079 0 .00041 0 .00078 0. 00039 0 . 4 0 .00213 0 .006 28 0 . 0 0 3 1 4 0 .00164 0 .003 11 0. 0 0 1 5 6 0 .8 0 .008 44 0 .0248 7 0 .01244 0 .006 5 3 0 .01237 0. 006 i3 1.6 0 . 0 3 2 6 9 0 .09597 0 . 0 4 7 0 8 0 .02556 0 .04802 0. 0 2 0 1 3*3 0. 115 4 0 0 .3 36 06 0 .16803 0 . 0 0 4 0 5 0 .17188 0. 08594

k« a 20.0

0. I 0 . 0 0 0 0 5 0 .0006 I 0 . 0 0 0 3 0 0 .00002 0 .00037 0 . 00002 0. 2 0 . 0 0 0 1 9 0 .00242 0 . 0 0 1 2 1 0 . 0 0 0 1 0 0 .00149 0 . 00007 0. 4 0 .00076 0 .00967 0 . 0 0 ;8 .'f 0 . 0 0 0 4 0 0. 005 96 0* 00030 0 . 3 0 .00300 0.038.; 5 0 .01922 0 . 0 0 1 5 9 0 .02369 0* 00113 1.6 0. 0 11 5 4 0 . I 5010 0 .07505 o» 006 30 0 .09274 0. 0 0.v6 4 3*2 0. OJ.003 0. 5.;942 0. 27,^71 0 . 0 2 4 0 9 0 .34233 0. 01712

k< B 200.0

0. I 0 .00003 0.ooo3 2 0 .00041 0 . 0 0 0 0 1 0 .00052 0. 00000 0. 2 0 . 0 0 0 1 I 0 .00333 0. 00164 0 .00002 0 .00206 0. 0 0 0 0 1 0 . 4 0 .00042 0 . 0 1 3 I 0 0 .006 5 5 o.ooooS 0 . 0 0 8 2 5 0 . 00004 0. 3 0 .00167 0 .05210 0 .02608 0 .00034 0 .03287 0. 00016 1.6 01 00629 0 .20491 0. 10245 0 .00135 0 .12933 0. 0006 5 3*2 0 . O 2 0 ' ; o 0 .76 76 9 0 .38384 0 . 0 0 5 2 7 0 .48719 0 . 00244

Page 30: Tables of Stresses in Three-Layer Elastic Systemsonlinepubs.trb.org/Onlinepubs/hrbbulletin/342/342-008.pdf · with some notes on the assumptions involved in setting up the problem

205

H " 8.0

k i s 20.0

a i <r cr -<r a i St 81 r a Sa r a £a r j ka a 0 .2

0 . I O . O O O I 3 0 .00056 0 .00003 0 .00011 0 .00001 0 .00006 O . 2 o . 0 0 0 4 7 0 .00223 0 . O O O I I 0 . 00044

0 .00176 0 .00005 0 . 0 0 0 3 5

o . 4 0 . 0 0 1 9 0 0 ,00889 0 .00044 0 .00044 0 .00176 0 . 0 0 0 3 0 0 . 0 0 0 9 9

0 .8 0 .00754 0 .03523 0 .00176 o .00701 0 .00079 0 . 0 0 3 9 3 1.6 0 .03947 0 .13569 0 .00678 0 .02746 0 .00306 0 .01528 3 ' 2 0 . 1o317 0 .47240 0 .02 36 2 0 . 1 0 1 5 0 .01105 0 . 0 5 5 2 4

ka 2.0

0.1 0. 0000 3 0 .00079 0. 00004 0 .00003 0. 00004 0 .00002 0. 2 0. 0001 3 0 .00316 0. 00016 0 .00011 0. 00016 0 .00008 0 . 4 0. 00050 0 . 0 1 3 6 0 0 . 0006 3 0 .00043 0. 00064 0 .00032 0. 8 0. 00200 0 .05007 0. 00250 0 . 0 0 1 7 0 0. 00253 0 .00127 1.6 0. 00786 0 .19496 0. 00975 0 .000 7 3 0. 00993 0 .00496 3 . 2 0 . 02944 0 .70709 0* 03535 0 . 0 3 5 7 9 0. 036 78 0 . 0 1 8 3 9

ka a 20.

0 . 1 0 . 00001 0 .00106 0. 00005 0 .00001 0 .00006 0 . 0 0 0 0 0 0. 2 0. 00004 0 .0042 5 0 . 00021 0 . 0 0 0 0 3 0. 00035 0 .00001 0. 4 0. 00014 0 .01696 0. 0008 5 0 . 0 0 0 0 9 0. 001 00 0 . 0 0 0 0 5 0 . 3 0 . 000 56 0. 06 7 51 0. 00338 0 .00037 0. 00393 0 . 0 0 0 2 0 1.6 0. 002 17 o. 26 466 0 . 01323 0 .00147 0. 01565 0 .00078 3 ' 2 0. 00791 0. Q3 4 50 0. 04922 0 .00576 0. 05892 0 .00295

ka = 200.(

0 . 1 0. 00000 0 . 00133 0'. 00007 0 . 0 0 0 0 0 0. 00008 0 . 0 0 0 0 0 0 . 2 0 . 00002 0 .00531 0 . 00037 0 . 0 0 0 0 0 0. 00032 0 •00000 0. 4 0. 00006 0 .02122 0. 00106 0 . 0 0 0 0 2 0. 00123 0 .00001 0 .8 0 . 00025 0 .08453 0 . 00 ;33 0.ooooS 0. 00509 0 . 0 0 0 0 3 1.6 0 . 00096 0 .33268 0. 0166 3 0 .00032 0. 02009 0 . 0 0 0 1 0 3'2 0 . 00319 1.256 1 4 0. 0638 1 0 . 0 0 1 2 5 0. 0766 0 0 .00038

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206

H - 8.0

k, . 200.0

cr <r or mcr <r -cr •1 >i Bt r a *t ka » 0.

O. I 0. 00003 0.ooo3 3 0. 00000 0 . 0 0 0 0 3 0.ooooo 0 . 00001 O . 2 0. 0001 I 0 .00330 0 . 00002 0 .00011 0 .00001 0. 00005 0 . 4 0 . 00046 0 . 0 1 3 2 0 0 . 00007 0•00044 0 .00004 0 . oooi3 0 . 8 0 . 00182 0 .05242 0. 00036 0 . 0 0 1 7 5 0 .00014 0. 0007 2 1.6 0 . 00720 0 .20411 0. 00102 0 .00693 0 .00056 0 .0028 2 3 . a o. 02751 0 .74013 0 . 00370 0 .026 56 0 .002 I 2 0. 01050

ka > 2 .

0.1 0. O O O O l 0 .00109 0. 00001 0 .00001 0 .00001 0. ooooo O* 2 0 . 00003 0 .00438 0 . 00002 0 . 0 0 0 0 2 0 . 0 0 0 0 2 0 . 00001 0 . 4 o. 00010 0 .01748 0. 00009 0 . 0 0 0 0 9 0 . 0 0 0 0 9 0 . 00005 0 . 8 o» 0004 I 0 .06956 0 . 00035 0 .00033 0 .00037 0 . oooi3 1.6 0 . 00162 0 .27 26 2 0 . 00136 0 . 0 0 1 4 9 0 .00145 0 . 00073 3 « 3 0 . 006 2 5 I . 01322 0 . 00507 0 . 0 0 5 8 4 0 .00547 0 . 00273

ka a 20.

0. I 0. 00000 0. 00136 0. 00001 0 .ooooo 0 .00001 o. OOOOO 0 . 2 0. 00001 0 . 005 46 0. 00003 0 .00001 0 .00003 0. ooooo 0*4 0* 00002 0 .02181 0. 00011 0 . 0 0 0 0 2 0 .0001 3 0. 00001 0. S 0. 00010 0 .08687 0. 00043 0 .00008 0. 0005 2 0 . 00003 1.6 0 . 00039 0. 34202 0. 00171 0 . 0 0 0 3 2 0 .00204 0. 00010 3 . 3 o. 00149 1 .29190 0. 00646 0 . 0 0 1 2 7 0 .00777 0 . 00039

ka - 200.(

O . I 0. 00000 0 .00163 0. 00001 0.ooooo 0 .00001 0. ooooo 0. 3 0. 00000 0 .006 54 0. 00003 0 .ooooo 0 .00004 0. ooooo 0. 4 o. O O O O l 0 .026 13 0. 00013 0 .ooooo 0 .00016 0 . ooooo 0 .8 0. 00003 0 .10417 0 . 00052 0 . 0 0 0 0 2 0 .0006 3 0 . ooooo 1.6 0 . 0001 3 0 .41121 0. 00206 0 . 0 0 0 0 7 0 . 0 0 2 4 9 0 . 00001 3 . 3 0. 00047 1 .56843 o. 00784 0 . 0 0 0 2 7 0 .00957 0 . 00005

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207

Appendix B A MATHEMATICAL DESCRIPTION OF THE PROBLEM

A diagrammatic representation of the system was given in Figure 1. The system consists of a semi-infinite elastic solid bounded at the surface by two finite elastic layers of constant thickness. The surface is loaded uniformly over a circular area and so, i f cylindrical polar coordinates (r , 6, z) are used, the stresses and strains in the system w i l l be independent of the angle 6.

Assumptions

1. The Applicability of the Theory of Elasticity.—The materials involved are assumed to be homogeneous and isotropic, the stress/strain relationship to be linear and the modulus to be the same in compression as in tension.

2. Description of System. — The three layers are horizontal and have different elastic properties. The two upper layers are weightless and of infinite extent in the horizontal plane. The bottom layer is infinite i n the horizontal plane and semi-infinite in the v e r t i ­cal plane.

3. Boundary Conditions. - The surfe.ce of the top layer is free of shear stress. Out­side the circular loaded area the surface is free of normal stress and inside the load is uniformly distributed. A l l stresses and displacements are zero at infinite depth.

4. Continuity Conditions. — The three layers are continuously in contact and act together as a composite medium. At the interfaces the normal and shear stresses and the vert ical and horizontal displacements must be the same in both layers.

TABLE 2

NOTATION FOR STRESSES Stress Symbol Vert ical normal Radial normal z Circumferential normal r Shear w

T Shear

rz

Figure 2 . Components of stress in cylindrical co-ordinates.

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208

5. Poisson's Ratio. - T h i s i s assumed to be equal to 0. 5 i n a l l three layers, the main reasons being that the algebra involved in developing the stress expression is consid­erably simplif ied. This value of Poisson's ratio corresponds to an incompressible medium.

Derivations of the Expressions for the Stresses in a Three-Layered System

The notation for the stresses is presented in Table 2. To take advantage of the sym­metry of the problem cylindrical polar coordinates have been used. The components of stress are shown i n Figure 2.

The equations of equilibrium are obtained by considering the total force f o r a small element in both the radial and vert ical directions.

^ , " ^ -JL^ = 0 (la) ar dz r

^•^rz ^^z ^rz „ , , .N

(Because of the axial symmetry in the problem, T^O and T„„ are zero, and there is no equilibrium condition f o r the e-direction).

In the general three-dimensional case in rectangular coordinates, each of the six components of strain (three normal and three shear) may be expressed in terms of the three components of displacement. Thus these equations are not independent and three relationships exist between the six components of strain. These are called the compati­b i l i t y conditions, and they may be expressed i n terms of components of stress by using Hooke's law. In cylindrical polar coordinates with axial symmetry the compatibility conditions become

^^r - •'e) ^ T T 7 (^r + + ^z) = ° ^^a) 2 2 _ , . 1 a

V " r r2 ' " r "9 ' " 1 + n

where ti is Poisson's ratio and

^ r 3 r 9z2

is the Laplacian operator. The components of stress and displacement may be expressed in terms of a stress

function «3 in such a way that Eqs. l a and l b are identically satisfied. These expressions are

Stress

^z

Displacement

= ^ [ ( 2 - . ) v ^ P - 1 ^ ] (3a)

TT [ ' ' V ^ ^ - ] (3b)

^ r z = ^ [ ( l - ' ' ) v V - 0 ] (3d)

(vertical) w = ^ [ ( 1 - 2,x)v'<P + | ^ + 7 | f ] ( 3 ^

^ r az

^9

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209

(horizontal) u = - - ^ ^ ^ (3f)

in which E is the modulus of elasticity. I t may be shown quite easily that Eqs. 2a and 2b are satisfied provided (fl is a. solution

of the biharmonic equation:

V V = 0 (4)

in which is again the Laplacian operator. The problem is thus reduced to the solution of this part ial differential equation sub­

ject to the boundary conditions at the surface, the interfaces and at infinite depth. The boundary conditions are expressed next; the numerical subscripts refer to the different layers.

Interface 1 Interface 2

(z = - hi) (z = -hi-h2)

Zl Z2 Z2 Zs (normal stresses)

^ r z i ~ ^rz2 T = T rz2 rzs

(shear stresses)

Wl = W2 W2 = Ws (vertical displacements)

Ml = U2 U2 = Us (horizontal displacements)

T^„ = 0 (z = 0, surface free of shear stress) r z i

Ws = Us = a„ = T^, = 0 at infinite depth Zs rzs *

(T = 1 O ^ r s a z

CT_ = 0 r > a (surfece loading)

The radial stresses ay are not continuous across the interface because the horizontal displacements are equal; they are determined by the relevant modulus of elasticity.

The'partial differential Eq. 4 may be solved by using the Hankel transform*. However, for purpose here the solution may be expressed i n the following f o r m .

The stress functions

(Pi (top layer) = J (mr) \ (A, + Biz) e""' + (Ci + Diz) e '™^ ' O L

<P2 (middle layer) = J^imr) [ (As + B2Z) e""^ + (C2 + Dzz) e"""^ '

<P3 (bottom layer) = J^(mr) [ (Cs + Dsz) e '™^ '

satisfy Eq. 4 and the conditions at infinite depth**. The ten constants are evaluated by using the boundary conditions at the interfaces, the condition that the surface shear stress is zero and by assuming a stress distribution of the f o r m :

*rhe Hankel transform F(m) of order zero of the function f(x) i s given by 00

P(m) = xf(x)j^(mx)dx 0

for details of the application of this transform to problems in three dimensional e l a s t i c i t y , see (6). * * J (x) i s the Bessel function of order zero.

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210

CT^ (r, m) -mJ^(mr)

The final expressions for the stresses and displacements are then given by

Z J z o 0

• f J O O

o j r , m) + a.(r , m) r dr dm

The total surface load is given by a "»

a (r, m) r dr dm J J Z o o

a mr J^(mr) dr dm = - aJt(am)dm = - 1

o o

(5a)

(5b)

(6)

The f ina l expressions for the stresses and displacements are obtained by substituting the stress functions <p into Eqs. 3a through 3f for the components of stress and then using the Eqs. 5a and 5b. The algebra involved is quite considerable but is simplified by assuming that Poisson's ratio is equal to 0. 5 in a l l three layers. The expressions for the components of stress that appear in the tables are given next.

(1) F i r s t interface

= - ( l - K ) J a i J i ( a i x ) § ^ d x

(2) Second interface

2<r. = J a , J i ( a i x ) § ^ djc

o

20- ^ = (1-K) J a i J i ( a i x ) § ^ dx

Za

2o-_ =

(VK)(1-M) J a , J i ( a t x ) f ^ d x

o 00

- d - K ) J a , J , ( a i x ) g f ^ i d x

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211

C9

2<r. = -(1-K)(1-N) J a t J t ( a i x ) dx o

The Byrabola and funct ions i n those expressions are 'def ined as f o l l o u s :

at = a A a , H =» h i A a * k i = E t . / E * , and k , «= E 2 / E 3 ,

7- =. ^ ^ - I M ka~1

f , ( x ) = (1+Hx) { e - ^ - KN«e-(^*«)=^ - ( l -Hx) {ife-^te _ ^a^-CSH+Oxj

-Npt (x )e - (^*2)x_j^p^(^j^ . (K+2)x

ga(x) = K ( 2 - 5 H x ) e " ^ - (2-Hx)e""^ - N* (2+Hx)o~(^+^)^

+KN«(2+5Hx)o-(^^*^)^ - Np3(x)o-(^*2)x _ ^p. (x)e- («*2)x

P i ( x ) = - (l+x+ftc)o''^"*'')^ - KN(l-x+^Ix-2Hx*)e"("+^)^

+K(l+x-IIx-2Jix*)e"(^+^)^ + ir(l-x-Hx)e"(^^"^^)^

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212

GaCx) = K(-2+x+5IIx-2Hx^)o"^5"*^)^ + (2-x-Hx)e"("+^

- N(2-5x-5Hx)o'(^^^*^^^ + KN(2-5x-Hx-10fIx^)e"("''^^^

D(x) = 1+2KIl( l+2x*)e'^ + K ^ N ' e ' ^ + K * o " ^ + 2KN(l+2x» )e"(^+2)x

^ N^,-(WI+4)x _ 2K(l+2II«x*)c-2H^ . K*Np,(x)o-<2K^2)x _ jjpe (x)c-(2H+^

- 2KN*(l+2H«x»)e"^2"*^^^

and

P i ( x ) = PaC-x) = -K(l+2x-Hx+2x*-2Hx^-4Kx^) + (l-2x-Hx+2x*+2Hx*)

P3(x) = p4( -x) = K(4+2Hx+8x'+2^') - (2-2tx-5Hx-2x'-2Hx*)

- K'(2+Ztx-5Hx+10x^+2Hx'-20}Ix')

Ps(x) = PeC-x) = K(2+4x+Hx-2x'-10Hx"+AHx') - (2-^-5Hx-2x*-2Hx*)

P T ( X ) = 2+4x^-8Hx*+2ai'x*+l6H»x^

PeCx) = 2+lpc*+8Hx'+4Jr'x'

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213

q , (x ) = N(2+5x+Hx-10Hx^) - (2-x-5Hx+2Hx^)

qa(x) = N(2+5x+5PIx) - (2-x-IIx)

qjix) = N(2+x+Hx) - (2-5x-5Hx)

q4 (x ) = N(2+x+5Hx+2Hx*) - (2-5x-Hx-10Hx*)

-The expression for gi(x) differs f rom that given by Acum and Fox in the fourth te rm in the th i rd bracket. This was discovered when an unaccountable discrepancy was noted for values of a Zl r i

An e r ro r was suspected when a certain lack of symmetry in

the expression for gi(x) was noted. Inspection showed that the coefficient of exp -(3H+4)x

should be N^ on both occasions, whereas the pap§r of Acum and Fox shows N instead of N^ in the third bracket. When this change was made the disagreement disappeared. The corrected expression was verif ied later when i t was derived f r o m f i r s t principles.

As a further check some results were obtained for comparison with those of Acum and Fox. These are presented in Appendix C (figures in brackets bemg taken f r o m Acum and Fox's paper).

Appendix C 0 . 2 5 5 .0

5 .0

o.S

0.5

0.5

0.5

0.74131 (0 .7410)

0.944.M (o .9470)

1.39453 (1 .3900)

(1 .2700)

o. 73401 1.69907 (0 .72^0) (1 .7000)

o.3q.r.3Q 0.49183 (o .3q7o) (o .5o3o)

0.30774 7.47254 (0 .3080 ) (7 .4700)

0.64196 12.73750 (0 .6420 ) (12 .7300)

0.23520 8.73121 (o .2850) (3 .7200)

o.56937 17. ;7833 (o .5700) (17 . ;5oo)

a« ra o.37892

(o .3790) o.35063

(o .2540)

o .3303i (o .3400)

o.09836 ( 0 . 1020)

o. I 4 9 ; s (o .1500)

0.25475 (0 .2550}

o. 17462 (o .1740)

(o .3490)

o.08733 (0 .0379 )

o.26496 (o .2650)

o.oz 171 ( o . o i 1 7 )

0 .0412s ( 0 . 0 4 1 3 )

0.05798 (o .0580)

o.19381 (o .1940)

8a ra o.38 000

(o .3800) 1.04512

(1 .0400)

0.70741 (o .7070)

2.23183 (2 .2300;

o.233 30 (o .2380)

0.7523^ (0 .7520)

0.00791 o.467.,3 (0 .00791) (0 .4660)

0.02934 I .61943 (0 .0292 ) (1 .6100)

0.07600 (o.076 1)

o< 20902 (o .2090) k , » 5 . 0 ka « 100 .0

o.00707 (o .00707)

o.02232 (o .0223)

k, a 50 .0 ka « 5 .0 o.o 4768

(o .0477) 0.1504c

(o .1500)

k i a 50 .0 ka a 100 .0 o.00467

(o .00466) O.016 IQ

( 0 . 0 1 6 1 ) ContlnuBd

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214

H 0 2 . 0 k, a 5 .0 ka a 5 ,0

<r ^ St Fa Ba ra 0. 5

1. 0

0.02848 (0 .0285 )

0 .0950? (o .0951)

0.21464 (0 .2150)

0.73664 (0 .7270 )

0 .0439? (0 .0430)

0 .1453? (0 .1450)

0.00955 (0 .00950)

0.03640 (0 .0364 )

0.04100 (0 .0409)

0.15324 (0 .1530 )

0.00820 (0 .00817)

0.0306 5 (0 .0306 )

0.5

0 .5

I . o

o.00524 (o .00522)

o.01867 (o .0187)

0.3826c 0.00765 0.00269 0.00856 ( 0 . 3 8 2 0 ) (0 .00765) (0 .00263) (0 .00853)

1.36457 0.02720 0.01054 0.03287 (1 .3600 ) ( 0 .0273 ) ( 0 . 0 1 0 5 ) (0 .0330)

0.00280 0.51248 (0.00281)^ (0 .5230 )

o.009x4 (0 .00921 )

0.01752 (0 .0176}

o. 06004 (o .0600)

0 . 0 I 0 2 C 0.00039 0.01430 ( 0 . 0 1 0 5 ) ( 0 .00041 ) ( 0 .0147 )

1.88310 0.03766 0.00156 0.05566 (1 .9300) (0 .0385) (0 .00163) (0 .0575)

0.27077 0.03706 0.00671 0.02701 (0 .2730 ) (0 .0372) (0 .00670) ( 0 .0270 )

0.93871 0.09388 0.03588 0.10202 (0 .9390 ) (0 .0938) ( 0 . 0 2 5 9 ) ( 0 . 1 0 2 0 )

k i a 50 .0 k , " 5 .0

o.00171 (0 .00170)

o.00657 (o .0066)

k i ka

50 .0 100.0

o.00014 (0 .00015)

o.00056 (0 .00058)

kt ka

1 0 . 0 5 . 0

0.00540 (0 .00540)

0.02040 (0 .0304 )

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175

(test 10), the sample expanded in the absence of water as could possibly occur with a sampling technique. It is significant that the slopes of the recompression curves vary considerably. Tests 6, 7, and 8 tend to follow the rebound lines 4, 5, and 9, and 11, 12, and 13 fall far higher. In particular, the slope of 13 is iVa times greater than that of test 8 which measures the true compressibility of the clay.

ACKNOWLEDGMENT The author owes a substantial debt to the Department of Mathematical Analysis at the

National Physical Research Laboratory, in particular to C. Cryer, who helped with the analysis and made important suggestions, and to J, Neetling for his aid in programing the consolidation problem for the computer. Also, P. Hall rendered valuable assistance in the computational work.

REFERENCES 1. Biot, M. A . , "General Theory of Three-Dimensional Consolidation." J. Appl.

Phys., 12:155 (1941). 2. Terzaghi, K . , "Theoretical Soil Mechanics." Wiley (1943). 3. Schiffman, R. L . , "Consolidation of Soil Under Time-Dependent Loading and

Varying PermeabUity." HRBProc, ,37: 584-617 (1958). 4. Croney, D. , Coleman, J. D. , and Black, W. P. M . , "Movement and Distri­

bution of Water in Soil in Relation to Highway Design and Performance." HRB Special Report 40, 226-252 (1958).

5. McNabb, A . , "A Mathematical Treatment of One-Dimensional Soil Consolidation." Quart. Appl. Math., Vol. 17, (Jan. 4, 1960).

6. Taylor, D. W., "F\indamentals of Soil Mechanics." Wiley (1948). 7. Crank, J . , "Mathematics of Diffusion." Oxford (1956). 8. Timoshenko, S., "Theory of Elasticity." McGraw-Hill (1934). 9. Skempton, A. W., and Bjerrum, L . , "A Contribution to the Settlement Analysis

of Foundations on Clay." Geotechnique. 7: 4 (1957). 10. Cooling, L . F., "The Measurement of Pore-Water Pressure and Its Application

to Some Engineering Soil Problems." R . L L . E . M . Paper 18, Theme la. Symposium sur les Observations des Ourvrages Realises au Laboratorio Nacional de Engenheria Civil , Lisbon (Oct. 1955).

11. Sneddon, I . N . , "Fourier Transforms." McGraw-Hill (1951). 12. de Josselin de Jong, G., "Application of Stress Rinctions to Consolidation Prob­

lems." Proc , 4th Internat. Conf. on boil Mechanics and Found. Eng., 1: 320-323 (1957).

13. Hart, E. G., Kondner, R. L . , and Boyer, W. C , "Analysis for partially Penetrating Sand Drains." Proc. Amer. Soc. Civ. Engrs., 84: S.M. 4 (Oct. 1958).

14. Seely, F. B . , and Smith. J. O., "Advanced Mechanics of Materials." Wiley (1952). 15. Love, A. E. H . , "The Stress Produced in a; Semi-Infinite Solid by Pressure on

Part of the Boundary." PhU. Trans., Series A, Vol. 226(1929). 16. de Wet, J. A . , "The Use of the Energy Concept in Soil Mechanics." Proc., 5th

Internat. Conf. on Soil Mechanics and Found. Eng., 1: 403-407 (1961).