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Computational Results for the KTH-NASA Wind-Tunnel Model Used for Acquisition of Transonic Nonlinear Aeroelastic Data.

机译：用于获取跨音速非线性气动弹性数据的KTH-Nasa风洞模型的计算结果。

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Silva, W. A.; Chwalowski, P.; Wieseman, C. D.; Eller, D.; Ringertz, U.;
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年度 2017
页码 1-19
总页数 19
原文格式 PDF
正文语种 eng
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7. Using transonic small disturbance theory for predicting the aeroelastic stability of a flexible wind-tunnel model [O] . Bennett Robert M., Silva Walter A. 1990

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Computational Results for the KTH-NASA Wind-Tunnel Model Used for Acquisition of Transonic Nonlinear Aeroelastic Data.

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