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This document provides instructions for Assignment 1 of the course AE682A: Analysis of Composite Structures. Students are asked to: 1) Write a MATLAB code to calculate the A, B, D matrices given laminate stacking sequence and lamina properties. The code should also determine lamina strains, stresses, and first-ply failure load using Tsai-Hill criterion for given loads. 2) Use the code to: a) Compare engineering constants of two laminates and comment on effect of 90-degree plies. b) Determine margin of s

Author

Vishnu A R

Language

EN