Numerical simulation of rotationally-induced ingress through turbine rim seals

被引：0
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作者：
Zhou, Kun-Yuan [1 ]
Luo, Xiang [1 ]
Xu, Guo-Qiang [1 ]
机构：
[1] National Key Laboratory of Science and Technology on Aero-Engine Aero-Thermodynamics, School of Jet Propulsion, Beijing University of Aeronautics and Astronautics, Beijing 100191, China
来源：
Hangkong Dongli Xuebao/Journal of Aerospace Power | 2011年 / 26卷 / 12期
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页码：2704 / 2709
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