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Solutions for certain rectangular slabs continuous over flexible ...

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ILLINOIR F.T'J(4TNEE14TN(5 TYP TMEYSTm RT A<br />

At the center of the beam this moment becomes<br />

2Pa 1<br />

max Mbeam -- -- (1 + av) e-I<br />

2 1,3,, .. n 2 S(42)<br />

Pv lrv 2Pa 1<br />

- loge coth - + - -- e- .<br />

r 2a r 2 1,,.. n 2<br />

8. Numerical Computations of Moments in the Infinitely Long Slab<br />

Having a Rigid Cross Beam and Supporting a Concentrated Load.-<br />

Numerical values* of the corrective bending moments M ' 1 and M 1)<br />

under the load, computed from (30) and (35) <strong>for</strong> I. = 0.15, are<br />

TABLE 1<br />

CORRECTIVE MOMENTS UNDER THE LOAD DUE TO A RIGID CROSS BEAM<br />

Concentrated load on the infinitely long slab of span a having a rigid cross beam. The load is<br />

at a distance u from one of the edges of the slab and at a distance v from the cross beam. Numerical<br />

values of MW() and M,0) in the table are corrective moments under the load, due to the presence of the<br />

beam, and were computed from Equations (30) and (35). The corrective moments are to be added to<br />

the corresponding moments found under the load on the infinitely long slab without the cross beam.<br />

Poisson's ratio, p = 0.15. Curves of moments are shown in Fig. 5 and Fig. 6.<br />

u<br />

a<br />

v<br />

M,.()<br />

P<br />

M,(1)<br />

P<br />

u<br />

a<br />

v<br />

a<br />

M,(1)<br />

P<br />

M4(1)<br />

P<br />

0.1<br />

or<br />

0.9<br />

0.2<br />

or<br />

0.8<br />

0.3<br />

or<br />

0.7<br />

0.05<br />

0.10<br />

0.15<br />

0.20<br />

0.30<br />

0.40<br />

0.50<br />

0.60<br />

0.80<br />

1.00<br />

0.05<br />

0.10<br />

0.15<br />

0.20<br />

0.30<br />

0.40<br />

0.50<br />

0.60<br />

0.80<br />

1.00<br />

0.05<br />

0.10<br />

0.15<br />

0.20<br />

0.30<br />

0.40<br />

0.50<br />

0.60<br />

0.80<br />

1.00<br />

-0.1547<br />

-0.0869<br />

-0.0522<br />

-0.0334<br />

-0.0159<br />

-0.0087<br />

-0.0051<br />

-0.0031<br />

-0.0012<br />

-0.0005<br />

-0.2162<br />

-0.1501<br />

-0.1101<br />

-0.0821<br />

-0.0473<br />

-0.0283<br />

-0.0174<br />

-0.0109<br />

-0.0043<br />

-0.0016<br />

-0.2460<br />

-0.1812<br />

-0.1420<br />

-0.1135<br />

-0.0736<br />

-0.0478<br />

-0.0309<br />

-0.0199<br />

-0.0080<br />

-0.0031<br />

-0.0627<br />

-0.0193<br />

-0.0066<br />

-0.0024<br />

+0.0001<br />

+0.0006<br />

+0.0007<br />

+0.0006<br />

+0.0004<br />

+0.0002<br />

-0.1170<br />

-0.05821<br />

-0.0298<br />

-0.0149<br />

-0.0026<br />

+0.0011<br />

+0.0020<br />

+0.0020<br />

+0.0013<br />

+0.0007<br />

-0.1456<br />

-0.0840<br />

-0.0506<br />

-0.0299<br />

-0.0084<br />

+0.0001<br />

+0.0030<br />

+0.0035<br />

+0.0024<br />

+0.0012<br />

0.4<br />

or<br />

0.6<br />

0.5<br />

0.05<br />

0.10<br />

0.15<br />

0.20<br />

0.30<br />

0.40<br />

0.50<br />

0.60<br />

0.80<br />

1.00<br />

0.05<br />

0.10<br />

0.15<br />

0.20<br />

0.30<br />

0.40<br />

0.50<br />

0.60<br />

0.80<br />

1.00<br />

-0.2610<br />

-0.1966<br />

-0.1580<br />

-0.1299<br />

-0.0892<br />

-0.0607<br />

-0.0406<br />

-0.0267<br />

-0.0109<br />

-0.0043<br />

-0.2656<br />

-0.2014<br />

-0.1630<br />

-0.1350<br />

-0.0942<br />

-0.0651<br />

-0.0441<br />

-0.0292<br />

-0.0121<br />

-0.0047<br />

-0.1602<br />

-0.0978<br />

-0.0629<br />

-0.0400<br />

-0.0135<br />

-0.0014<br />

+0.0033<br />

+0.0045<br />

+0.0033<br />

+0.0017<br />

-0.1647<br />

-0.1022<br />

-0.0669<br />

-0.0434<br />

-0.0154<br />

-0.0021<br />

+0.0033<br />

+0.0048<br />

+0.0036<br />

+0.0019<br />

*Numerical values of the hyperbolic functions were obtained from the British Association <strong>for</strong> the<br />

Advancement of Science, Mathematical Tables, V. 1, London, 1931.

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