无粘流
颤振
热的
计算机科学
机械
物理
空气动力学
气象学
作者
Elizabeth J. Kenyon,Vilas Shinde
摘要
Aerothermoelastic panel flutter at high-speeds (supersonic/hypersonic) can be detrimental to the aircraft structures. In this paper, we delineate different regions of inviscid panel flutter on a stability map that is derived in terms of the more accessible mass ratio (
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