Flutter Analysis of A Laminated Composite Plate with Temperature Dependent Material Properties

Abstract

The research progress and some of the references can be found in the literature as can be seen in Fung [1] and Dowell [2, 3]. Bismarck-Nasr [4] reviewed the finite element analysis of aeroelasticity of plates and shells. The most used aerodynamic theory is piston theory that was first suggested by Ashley and Zartarian [5]. Mei [6] developed a finite element approach to panel flut-