Vestnik Moskovskogo Universiteta. Seriya 1. Matematika. Mekhanika
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Vestnik Moskovskogo Universiteta. Seriya 1. Matematika. Mekhanika, 2015, Number 2, Pages 32–36 (Mi vmumm220)  
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
Full-text PDF (311 kB) Citations (5)
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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
English version:
Moscow University Mechanics Bulletin, 2015, Volume 70, Issue 2, Pages 23–27
DOI: https://doi.org/10.3103/S0027133015020016
Bibliographic databases:
Document Type: Article
UDC: 539.3
Language: Russian
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
Citation in format AMSBIB
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\by A.~V.~Vasil'ev
\paper Flutter of conical shells under external flow of a supersonic gas
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\issue 2
\pages 32--36
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\jour Moscow University Mechanics Bulletin
\yr 2015
\vol 70
\issue 2
\pages 23--27
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    • This publication is cited in the following 5 articles:
    Citing articles in Google Scholar: Russian citations, English citations
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