Annotation
The problem of determining the critical values ν_(cr) and ω_(cr) of torsional flutter is solved as a boundary-value problem for a distributed elastic system. The vibration modes of an inhomogeneous wing in flutter and a comparison of the values obtained with those given by the Bubnov-Galerkin method are presented.
© 2016 Publisher M.V.Lomonosov Moscow State University
Authors
S.P. Strelkov, N.D. Tarankova, and A.A. Kharlamov
Department of General Physics for the Division of Mechanics and Mathematics
Department of General Physics for the Division of Mechanics and Mathematics