Question: An antisymmetric [0/90] laminate is loaded under a biaxial load Nx = Ny = No. The following strains and curvatures are obtained &=&=&o, Kx

An antisymmetric [0/90] laminate is loaded under a biaxial load Nx = 

An antisymmetric [0/90] laminate is loaded under a biaxial load Nx = Ny = No. The following strains and curvatures are obtained &=&=&o, Kx = -Ky = Ko. Assuming that Vy < < 1, obtain an expression for Ex as a function of the relevant stiffness parameters Aij, Bij, and Dij.

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