Teaching scripts for Classical Lamination Theory
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Main example script for the symmetric carbon/epoxy laminate \([0/45/-45/90]_s\).
Builds the laminate matrices \(\mathbf{A}\), \(\mathbf{B}\), \(\mathbf{D}\), and the full \(\mathbf{ABD}\) matrix.
Transforms laminate-frame stress into ply material stress.
Computes the Tsai–Hill failure index.
Plots ply stresses and failure index.
Short usage guide and recommended execution order.