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Computer Aided Design Environment for Composites (CADEC) 14.1.7255.18050

Software Support for Introduction to Composite Materials Design-- 3rd Edition, CRC (2018) by Ever J. Barbero

CADEC--Ply Mechanics-Plane Stress-Reduced Compliance Matrices-Lamina CS

For plane stress, the compliance is a 3x3 matrix that is easily calculated in terms of engineering properties such as longitudinal modulus, etc. In 3D, it is a 6x6 matrix, also easily calculated from engineering properties such as longitudinal modulus, transverse modulus, shear modulus, inplane Poisson ratio, as described in the textbook.

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