Stall flutter computation of turbomachinery blade based on a CFD/CSD coupling method

被引：2
|
作者：
Zhou, Di [1 ]
Lu, Zhiliang [1 ]
Guo, Tongqing [1 ]
Shen, Ennan [1 ]
机构：
[1] College of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing,210016, China
来源：
Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica | 2015年 / 36卷 / 04期
关键词：
Compendex;
D O I：
10.7527/S1000-6893.2014.0212
中图分类号：
学科分类号：
摘要：
Computational fluid dynamics
引用
收藏
页码：1076 / 1085
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