Review of Nonlinear Panel Flutter at Supersonic and Hypersonic Speeds
Review of Nonlinear Panel Flutter at Supersonic and Hypersonic Speeds
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DOI：
10.1115/1.3098919
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发表时间：
1999-10
影响因子：
14.3
通讯作者：
C. Mei;K. Abdel-Motagaly;R. Chen
中科院分区：
文献类型：
--
作者：
C. Mei;K. Abdel-Motagaly;R. Chen
综述了超音速和高超声速壁板颤振的各种分析方法和实验结果。分析方法主要分为两种。第一类是经典方法，包括Galerkin结合数值积分的方法、调和平衡法和摄动法。第二类是频域(本征解)或时间域(数值积分)的有限元方法。对实验文献进行了综述。描述了不同参数对颤振行为的影响。考虑的参数包括面内力、热载荷、流动方向和初始曲率。文中还考虑了复合材料壁板在超音速和高温下的主动控制。本文引用了84篇参考文献。
A review of various analytical methods and experimental results of supersonic and hypersonic panel flutter is presented. The analytical methods are categorized into two main methods. The first category is the classical methods, which include Galerkin in conjunction with numerical integration, harmonic balance and perturbation methods. The second category is the finite element methods in either the frequency domain (eigensolution) or the time domain (numerical integration). A review of the experimental literature is given. The effects of different parameters on the flutter behavior are described. The parameters considered include inplane forces, thermal loading, flow direction, and initial curvature. Active control of composite panels at supersonic speeds and elevated temperatures is also considered. This review article cites 84 references.