Investigation of the occurrence of flutter in isotropic and orthotropic plates with different boundary conditions and skew angles

The purpose of the research: to determine the possibility of a panel flutter in the range of average supersonic speeds in a multilayer composite plate with the shape of a rectangle or parallelogram and taking into account the direction of action of the velocity flow relative to its longitudinal edges. The possibility of panel flutter occurrence in the range of average supersonic speeds (1.4