Flutter of a Rectangular Panel as a Part of a Thin Wedge Surface

被引:0
|
作者
Kiiko, I. A. [1 ]
Kudryavtsev, B. Yu. [1 ]
机构
[1] Moscow MV Lomonosov State Univ, Fac Mech & Math, Leninskie Gory, Moscow 119899, Russia
关键词
D O I
10.3103/S002713301102004X
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
The stability of an elastic plate and an elastic panel placed in a supersonic gas flow is studied in a nonlinear formulation. The gas velocity vector is directed at a small angle to them. The critical velocity of the flow is determined for various parameter values. The numerical results obtained are compared.
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页码:44 / 47
页数:4
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