Flutter of a Multicomponent Beam in a Supersonic Flow

被引:4
|
作者
Amato, Marco [1 ]
Elishakoff, Isaac [2 ]
Reddy, J. N. [3 ]
机构
[1] Univ Bologna, Dept Civil Chem Environm & Mat Engn, Viale Risorgimento 2, I-40136 Bologna, Italy
[2] Florida Atlantic Univ, Dept Ocean & Mech Engn, Boca Raton, FL 33431 USA
[3] Texas A&M Univ, Dept Mech Engn, College Stn, TX 77843 USA
关键词
Supersonic Flow; Finite Element Solution; Galerkin Method; Piston Theory; Flow Velocity; Dirac Delta Function; Aerodynamic Damping; Elastic Deformation; Nonlinear Systems; Free Vibrations; BUCKLING MODE LOCALIZATION; FINITE-ELEMENT METHOD; PANEL FLUTTER; UNCERTAINTY QUANTIFICATION; MULTIBAY PANELS; PLATES; STABILITY; VIBRATION; AEROELASTICITY;
D O I
10.2514/1.J060631
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
This study is devoted to the investigation of flutter of beams with highly contrasting materials. Two versions of the Galerkin method are applied: original version and modified version. It is shown that the modified Galerkin method tends to the exact solution for the inhomogeneous case in contrast with the original implementation, which does not. Secondly, modified and original Galerkin methods tend to the same solution in the homogeneous case. As far as the flutter is concerned, the modified Galerkin method tends to the finite element solution for the inhomogeneous case in contrast with the original implementation, which does not. Both original and modified Galerkin methods in the inhomogeneous case require many more terms (namely, 300) than the modified Galerkin method in the homogeneous case, where 10 terms sufficient.
引用
收藏
页码:4342 / 4353
页数:12
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