Numerical investigation of blade vibration responseinduced by inlet distortion in axial compressor
National Key Lab. on Aero-engine Aerodynamics and Thermodynamics, Coll. of Energy and Power Engineering,Beijing Univ. of Aeronautics and Astronautics, Beijing 100191, China;National Key Lab. on Aero-engine Aerodynamics and Thermodynamics, Coll. of Energy and Power Engineering,Beijing Univ. of Aeronautics and Astronautics, Beijing 100191, China;National Key Lab. on Aero-engine Aerodynamics and Thermodynamics, Coll. of Energy and Power Engineering,Beijing Univ. of Aeronautics and Astronautics, Beijing 100191, China
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