Flutter and Limit Cycle Oscillations of Cantilevered Plate in Supersonic Flow
Flutter and Limit Cycle Oscillations of Cantilevered Plate in Supersonic Flow
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DOI：
10.2514/1.c035992
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发表时间：
2020-10
影响因子：
2.2
通讯作者：
Kevin A. McHugh;M. Freydin;K. K. Bastos-K.;P. Beran;E. Dowell
中科院分区：
文献类型：
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作者：
Kevin A. McHugh;M. Freydin;K. K. Bastos-K.;P. Beran;E. Dowell
在气动弹性环境中，对大挠度结构的理论模型的研究兴趣正在增长。本文介绍了一个悬臂板模型，该模型承受轴向超声速流动以.
Research interest is growing for theoretical models of highly deflected structures in aeroelastic settings. Presented here is a model of a cantilevered plate subjected to axial supersonic flow to d...