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2 International Journal of Applied Mechanics and Engineering

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First ply failure analysis of laminated composite beam for different boundary conditions under thermo mechanical loading

Choudhury Arnab, Mondal Samar Chandra, Sarkar Susenjit

International Journal of Applied Mechanics and Engineering

2020

Vol. 25, no. 1

12--26

Failure analysis of a laminated composite beam subjected to uniformly distributed load and thermal load is studied for different boundary conditions and fiber orientation angles, based on first ply failure load. Three different boundary conditions are studied: simply supported, fixed-fixed and fixed-free. The strength ratio is computed and compared for different failure theories. The effect of fiber orientation angle and aspect ratio on the strength ratio based on first ply failure load is presented in the paper. The strength ratio and transverse deflection are determined for Graphite/Epoxy and Glass/Epoxy composite and their hybrid combinations to find out the optimum hybrid composite beam with minimum weight, deflection and cost. The problem is solved in MATLAB platform. The mode of failure of the composite beam is determined by using maximum stress theory.

Failure analysis of laminated composite plate under hygro-thermo mechanical load and optimisation

Choudhury A., Mondal S. C., Sarkar S.

International Journal of Applied Mechanics and Engineering

2019

Vol. 24, no. 3

509--526

Failure analysis of laminated composite plates for different mechanical, thermo mechanical and hygro-thermo mechanical loads for different ply thicknesses, stacking sequences, fiber orientation angles and composite material systems is presented in the paper. A comparative study of different failure theories is also presented in the paper. The effect of fiber orientation angles on the first ply failure load is also studied. A hybrid composite laminate is developed based on the first ply failure load which minimizes weight and cost. The last ply failure load based on fully discounted method is calculated for different stacking sequences. An optimum composite material system and laminate layup is studied for a targeted strength ratio which minimizes weight.