Wing aeroelasticity analysis based on an integral boundary-layer method coupled with Euler solver

被引：0
|
作者：
Ma, Yanfeng [1 ,2 ]
He, Erming [1 ]
Zeng, Xianang [2 ]
Li, Junjie [2 ]
机构：
[1] School of Aeronautics, Northwestern Polytechnical University, Xi'an,Shaanxi,710072, China
[2] AVIC Xi'an Aircraft Design and Research Institute, Xi'an,Shaanxi,710089, China
来源：
Chinese Journal of Aeronautics | 2016年 / 29卷 / 05期
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页码：1262 / 1272
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