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

关键词：

D O I：

暂无

中图分类号：

学科分类号：

摘要：

Journal article (JA)

引用

页码：1262 / 1272

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