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Solutions for certain rectangular slabs continuous over flexible ...

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SOLUTIONS FOR CERTAIN RECTANGULAR SLABS<br />

Fic. 24<br />

in Fig. 24, the deflection w may be taken as the sum of the deflection<br />

of a uni<strong>for</strong>mly loaded beam,<br />

w 4pa 4 _1 p<br />

= N-<br />

E<br />

sin ax = (x 4 -<br />

N .... n<br />

24N<br />

2 a x 3<br />

+ a 3 x), (131)<br />

and a correction<br />

4pa 4 1<br />

w" - • -E (b3 cosh ay-C3 ay sinh ay) sin ax. (132)<br />

75N 17.,. nI<br />

Thus, <strong>for</strong> any value of y within the slab,<br />

4pa 4 1<br />

w = - (1-b 3 cosh ay+c 3 ay sinh ay) sin ax. (133)<br />

75N i,3,•,..n 5<br />

The boundary conditions at y = b, similar to (97) and (98),<br />

when applied to w, give the results:<br />

Ab3 = 2n7rH 2 (2 cosh ab + ab sinh ab)<br />

+ 2A [(1 - A) ab cosh ab - (1 + u) sinh ab], (134)<br />

Ac 3 = 2nrH 2 cosh ab + 2 ju (1 - p) sinh ab, J<br />

where A is given in Appendix B. In the special case when H 2 = 0<br />

this solution reduces to that given by Holl.* In the other limiting<br />

case, when H 2 = oo, the solution reduces to that given by NAdait <strong>for</strong><br />

the uni<strong>for</strong>mly loaded <strong>rectangular</strong> slab simply supported on four sides.<br />

*D. L. Holl, "Analysis of Thin Rectangular Plates Supported on Opposite Edges," Bulletin 129,<br />

Iowa Engineering Experiment Station, Iowa State College, 1936, pp. 15, 87, and 88.<br />

tA. Nadai, Die elastischen Platten, 1925, p. 123.

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