Mathematical modelling of nonlinear flutter of viscoelastic elements and units of the flying device

In work the generalized mathematical model for a class of nonlinear problems about flutter of viscoelastic isotropic plates, panels and the shells which are flowed round by a supersonic flow of gas is constructed. Computing algorithms are developed and the complex of applied programs for the decision of a wide class of problems about nonlinear flutter of viscoelastic elements and units of the flying device is created.