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机译:Loss reduction in a high-speed compressor cascade using an L-shaped endwall groove to generate a streamwise vortex
Northwestern Polytech Univ, Sch Power & Energy, Xian 710129, Shaanxi, Peoples R China;
Northwestern Polytech Univ, Sch Power & Energy, Xian 710129, Shaanxi, Peoples R China|Shaanxi Key Lab Internal Aerodynam Aeroengine, Xian 710129, Peoples R China;
Trinity Coll Dublin, Dept Mech Mfg & Biomed Engn, Dublin, Ireland;
Endwall loss; Linear compressor cascade; L-shaped groove; Streamwise vortex; Geometry generation method;