Abstract:
Nonlinear vibrations of viscoelastic elements of aviation structures are studied. A method and an algorithm for the numerical solution of integrodifferential equations are proposed. The critical velocity of the flow past viscoelastic plates is determined.
Citation:
B. A. Khudayarov, N. G. Bandurin, “Numerical investigation of nonlinear vibrations of viscoelastic plates and cylindrical panels in a gas flow”, Prikl. Mekh. Tekh. Fiz., 48:2 (2007), 156–162; J. Appl. Mech. Tech. Phys., 48:2 (2007), 279–284