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Solutions for certain rectangular slabs continuous over flexible ...

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SOLUTIONS FOR CERTAIN RECTANGULAR<br />

SLABS<br />

the modulus of elasticity and moment of inertia of the<br />

are not zero.<br />

edge beams,<br />

The deflection of each of the edge beams becomes<br />

where<br />

SPa<br />

2<br />

1<br />

z = w - f7 sin au sin ax<br />

J y-b rW 3 N 1,2,3, n 3<br />

2Pa 3 1<br />

= o - , - fs sin au sin ax<br />

r 4 E I 2 1,2,3, n 4<br />

2Pa 3 1<br />

z o- = - sin au sin ax<br />

r E2I2 1.3.. n 4<br />

(114)<br />

P (a - u) x<br />

(a= u) (2au - X 2 - u2)<br />

6E212a<br />

<strong>for</strong><br />

x < u<br />

(115)<br />

P (a - x) u<br />

= x- (2ax - u 2 - x 2 )<br />

6E212a<br />

<strong>for</strong> x > u.<br />

Here zo is the simple beam deflection <strong>for</strong> the edge beam supporting<br />

the concentrated load, but without the effect of the slab. The<br />

quantities f7 and fs are given in Appendix B.<br />

The bending moment in either edge beam is<br />

d 2 zo 2Pa 1<br />

Mbeam = - Ed 2<br />

S<br />

2 fs sin au sin ax.<br />

da;" T 1- .-. n<br />

When the loads are at the center of the edge beams, the moment under<br />

each load becomes<br />

Pa/ f<br />

max. Mbeam -- 11- 8 )<br />

4 \ 72 n1,,.. 2 /<br />

At the edge of the slab the bending moment My is zero and<br />

M u = Mbeam.<br />

y- aH2<br />

(116)

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