Effects of Material Constructions on Supersonic Flutter Characteristics for Composite Rectangular Plates Reinforced with Carbon Nano-structures

Abstract In this paper effects of material constructions on natural frequencies and critical aerodynamic pressures are investigated. It is assumed that the rectangular plate made a polymeric matrix reinforced with graphene nanoplatelets or carbon nanotubes. A general closed analytical method solution presented. demonstrated three parameters define entirely location flutter pressure. The influence properties transverse shear characterized by set multipliers. They can be easily adopted in design procedures.