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.
机构:Technion-Israel Inst of Technology,, Dep of Aeronautical Engineering,, Haifa, Isr, Technion-Israel Inst of Technology, Dep of Aeronautical Engineering, Haifa, Isr
机构:
Inst Tecnol Aeronaut, Div Aeronaut Engn, BR-12228900 Sao Jose Dos Campos, BrazilInst Tecnol Aeronaut, Div Aeronaut Engn, BR-12228900 Sao Jose Dos Campos, Brazil
Bismarck-Nasr, MN
Bones, CA
论文数: 0引用数: 0
h-index: 0
机构:
Inst Tecnol Aeronaut, Div Aeronaut Engn, BR-12228900 Sao Jose Dos Campos, BrazilInst Tecnol Aeronaut, Div Aeronaut Engn, BR-12228900 Sao Jose Dos Campos, Brazil