Prediction and evaluation of aerodynamic stability of high bypass ratio turbofan engine deployed with thrust reverser

被引：0
|
作者：
Wang, Zhiqiang [1 ]
Shen, Xigang [2 ]
Hu, Jun [1 ]
机构：
[1] College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing,210016, China
[2] Aero Engine (Group) Corporation of China Shenyang Engine Research Institute, Shenyang,110015, China
来源：
Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica | 2017年 / 38卷 / 02期
关键词：
18;
D O I：
10.7527/S1000-6893.2016.0143
中图分类号：
学科分类号：
摘要：
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