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提醒：Tag:气动弹性力学
【标题】Calculated using NASTRAN wing of the divergence speed pressure. Pdf(177.85 KB)
【摘要】Wing divergent issues, not the traditional dynamic aeroelastic mechanical analysis methods, but with aerodynamic elasticity of static analysis methods, calculated with the multi-group under the conditions of the (q, θ) value, obtained through a curve divergence speed pressure . By comparison, such as axis can use hyperbolic characterization of divergence, to obtain divergence speed pressure for a simple formula.... (04-13 17:12)
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