Static aeroelastic optimization of hypersonic aircraft based on high-fidelity model

被引：0
|
作者：
Su, Hua [1 ]
Gu, Liang-Xian [1 ]
Gong, Chun-Lin [1 ]
机构：
[1] National Key Laboratory of Aerospace Flight Dynamics, School of Astronautics, Northwestern Polytechnical University, Xi'an 710072, China
来源：
Hangkong Dongli Xuebao/Journal of Aerospace Power | 2013年 / 28卷 / 08期
关键词：
Computational fluid dynamics;
D O I：
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中图分类号：
学科分类号：
摘要：
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页码：1836 / 1842
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