First and Last Ply Failure Load of Laminate using Partial and Complete Degradation
Stores geometric, elastic, strength, hygrothermal properties of the lamina.
Have functionality to return transformation, compliance, stiffness and reduced stiffness matrix of lamina.
Stores array of Lamina class object, position of these lamina from mid surface and their failure status.
Have functionality to return ABD Matrix of the laminate and failure status of laminate.
First and Last Ply failure loads.
local stresses and local strains in each lamina.
global stresses and global strains in each lamina.
Mid surface strains and curvature.