By Simon McBeath
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____________ . _ . _________ . ____ . __ . __ _ 0,8 ~[100%] 0,6 . . . . ... - - - - -' ............................. 0,4 - -- - -_. - - _... _. - _. - - - - _. -- -- - -- - - - _. , - _. - - - - - - - - - - - - - - .. - - - - -- - - _.. - - - _.. 2 _. _.. -- - - -. -. - - -- _. -. - - -. - _... 2 TIOO15208, rectangular plate, all supported edges, uniform load- {(Opl90qhols; p + q =5. 25 In both cases, the maximum deflection is given by balanced configurations for non-square plates. The next deflection is given by lightly unbalanced configurations (60% of fibres in the transverse direction and 40% in the longitudinal direction) and so on.
1 Short fibre composites Short fibre composites include sheet moulding composites (SMC) and whisker composites. Using laminated plate theory, we can derive: • The Q-isotropic constants for randomly oriented fibres in the plate can be obtained using the plane stress constants mentioned before. 21 • The Q-isotropic strengths can be obtained using the [1t/3] Q-isotropic laminates subjected to uniaxial tensile and compressive stresses, and pure shear, together with the quadratic failure criterion .
0,9 0,8 0,7 0,6 ..... - .......... ••••• I I 0,5 1 . 9. Representation of in-plane loads for fo = 120°. 48 1,5 ...... 1 0,5 .......... .......... - 0 ..... z - I I 0,5 1 III •• • • • ..... I~--~k----+------1 • 1 , 5 ........ 10. Representation of in-plane loads for fo = 150°. 10 0 -10 -20 -3 0 ..... '. I '1. ". '. 11. Representation of in-plane loads for fo =180°. The relationships between Nf and NjIl shown in Fig. 11 depend only upon f, because r and p appear in the factor ( p . r 2 ) in the expressions of both in-plane loads Nf and NjIl for angles higher and lower than f o.