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Vestnik Moskovskogo Universiteta. Seriya 1. Matematika. Mekhanika, 2015, Number 2, Pages 32–36
(Mi vmumm220)
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This article is cited in 5 scientific papers (total in 5 papers)
Mechanics
Flutter of conical shells under external flow of a supersonic gas
A. V. Vasil'ev Lomonosov Moscow State University, Faculty of Mechanics and Mathematics
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 flutter problem for conical shells under external flow of a supersonic gas in a new formulation and discuss the effect of new terms on the critical Mach number.
Key words:
flutter, conical shell, external flow.
Received: 16.11.2011 Revised: 05.12.2013
Citation:
A. V. Vasil'ev, “Flutter of conical shells under external flow of a supersonic gas”, Vestnik Moskov. Univ. Ser. 1. Mat. Mekh., 2015, no. 2, 32–36; Moscow University Mechanics Bulletin, 70:2 (2015), 23–27
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https://www.mathnet.ru/eng/vmumm220 https://www.mathnet.ru/eng/vmumm/y2015/i2/p32
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Abstract page: | 93 | Full-text PDF : | 42 | References: | 27 |
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