Numerical Study of Compressor Rotor Blade Resonance Induced by Wake of Inlet Probe Support
1.College of Energy and Power,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,China;2.AECC Sichuan Gas Turbine Establishment,Mianyang 621000,China;3.School of Aeronautics and Astronautics,Sichuan University,Chengdu 610065,China
YANG Rong-fei1, LIU Hai-xu1, XIANG Hong-hui2, GAO Jie2, WANG Jing-yu3. Numerical Study of Compressor Rotor Blade Resonance Induced by Wake of Inlet Probe Support[J]. Journal of Propulsion Technology, 2021, 42(5): 1002-1012.
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