FGM Composite Cylindrical Shell Panel Analysis for Post Buckling Resting on Elastic Foundations and Thermomechanical Loading

摘要

FGM composite Cylindrical shell Panel Analysis in thermomechanical loading for post buckling resting on elastic foundations is carried out. The technique applied is first order perturbation with SFEM in MATLAB code. Present study is focused on study of variations in plate thickness ratios simultaneously increase in amplitude ratios and elastic foundations in thermal environments. Present findings are compared with Published work and with more robust simulation. Applicability of this study is in Aerospace Engineering.