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One method of analyzing wing stability in flight

S.P. Strelkov, N.D. Tarankova, and A.A. Kharlamov

Moscow University Physics Bulletin 1975. 30. N 3. P. 8

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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.

Authors
S.P. Strelkov, N.D. Tarankova, and A.A. Kharlamov
Department of General Physics for the Division of Mechanics and Mathematics
Issue 3, 1975

Moscow University Physics Bulletin

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