Derive the differential equation and the boundary conditions governing the small transverse deflections of a simply supported, rectangular, symmetric angle-ply laminate that is subjected to distributed loading. If the loading is described by Equation 7.144, does a solution of the form given in Equation 7.145 satisfy this differential equation and boundary conditions? Why?

Transcribed Image Text:

00 (x, y) = mm sin m=1 n=1 mx sin (7.144) a b