Vestnik Moskovskogo Universiteta. Seriya 1. Matematika. Mekhanika
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Vestnik Moskovskogo Universiteta. Seriya 1. Matematika. Mekhanika, 2011, Number 5, Pages 61–65 (Mi vmumm724)  
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Flutter of a cylindrical shell subjected to an internal supersonic gas flow

A. V. Vasil'ev

Lomonosov Moscow State University, Faculty of Mechanics and Mathematics
Full-text PDF (231 kB)
Abstract: The well-known piston theory formula for the excess aerodynamic pressure is used in the majority of works devoted to the panel flutter of shells. In this paper, we consider the solution of the problem on the flutter of a cylindrical shell with internal flow by supersonic gas flow in a new formulation.
Key words: flutter, cylindrical shell, internal flow.
Received: 29.10.2010
Bibliographic databases:
Document Type: Article
UDC: 539.3
Language: Russian
Citation: A. V. Vasil'ev, “Flutter of a cylindrical shell subjected to an internal supersonic gas flow”, Vestnik Moskov. Univ. Ser. 1. Mat. Mekh., 2011, no. 5, 61–65
Citation in format AMSBIB
\Bibitem{Vas11}
\by A.~V.~Vasil'ev
\paper Flutter of a cylindrical shell subjected to an internal supersonic gas flow
\jour Vestnik Moskov. Univ. Ser.~1. Mat. Mekh.
\yr 2011
\issue 5
\pages 61--65
\mathnet{http://mi.mathnet.ru/vmumm724}
\mathscinet{http://mathscinet.ams.org/mathscinet-getitem?mr=2964362}
\zmath{https://zbmath.org/?q=an:06774427}
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