Numerical Study of Benchmark Super-Critical Wing at Flutter Condition

机译：颤振条件下基准超临界机翼的数值研究

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This paper presents a numerical study of the Benchmark Super-Critical Wing, BSCW at flutter condition which were done as a part of the AIAA Aeroelastic Predictions Workshop, AePW Ⅱ. The primary purpose is the evaluation of the time synchronization effect on the convergence of the coupled CFD-CSM process.

机译：本文介绍了作为基准条件的超临界机翼，在颤动条件下的BSCW，这是AIAA气动弹性预测研讨会AePWⅡ的一部分。主要目的是评估时间同步对耦合CFD-CSM过程收敛的影响。

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《AIAA aerospace sciences meeting;AIAA SciTech Forum》|2016年|12947-12957|共11页
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Adam Jirasek; Mats Dalenbring; Jan Navratil;
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4. Numerical Study of Benchmark Super-Critical Wing at Flutter Condition [C] . Adam Jirasek, Mats Dalenbring, Jan Navratil AIAA aerospace sciences meeting . 2016

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Numerical Study of Benchmark Super-Critical Wing at Flutter Condition

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