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机译:局部高助力转子风扇空气动力性能和流量机理的数值研究
Chinese Acad Sci Inst Engn Thermophys Key Lab Light Duty Gas Turbine Beijing Peoples R China|Univ Chinese Acad Sci Beijing Peoples R China|Chinese Acad Sci Innovat Acad Light Duty Gas Turbine Beijing Peoples R China;
Chinese Acad Sci Inst Engn Thermophys Key Lab Light Duty Gas Turbine Beijing Peoples R China|Univ Chinese Acad Sci Beijing Peoples R China|Chinese Acad Sci Innovat Acad Light Duty Gas Turbine Beijing Peoples R China;
Chinese Acad Sci Inst Engn Thermophys Key Lab Light Duty Gas Turbine Beijing Peoples R China|Univ Chinese Acad Sci Beijing Peoples R China|Chinese Acad Sci Innovat Acad Light Duty Gas Turbine Beijing Peoples R China;
Chinese Acad Sci Inst Engn Thermophys Key Lab Light Duty Gas Turbine Beijing Peoples R China|Univ Chinese Acad Sci Beijing Peoples R China|Chinese Acad Sci Innovat Acad Light Duty Gas Turbine Beijing Peoples R China;
Chinese Acad Sci Inst Engn Thermophys Key Lab Light Duty Gas Turbine Beijing Peoples R China|Univ Chinese Acad Sci Beijing Peoples R China|Chinese Acad Sci Innovat Acad Light Duty Gas Turbine Beijing Peoples R China;
Chinese Acad Sci Inst Engn Thermophys Key Lab Light Duty Gas Turbine Beijing Peoples R China|Univ Chinese Acad Sci Beijing Peoples R China|Chinese Acad Sci Innovat Acad Light Duty Gas Turbine Beijing Peoples R China;
Chinese Acad Sci Inst Engn Thermophys Key Lab Light Duty Gas Turbine Beijing Peoples R China|Univ Chinese Acad Sci Beijing Peoples R China|Chinese Acad Sci Innovat Acad Light Duty Gas Turbine Beijing Peoples R China;
Axial compressor; Fan; Tandem rotor; Numerical simulation; Flow mechanism;
机译:改进的仅转子轴流风扇-部分:任意涡流的数值有效空气动力学模型
机译:面向仅转子的改进型轴流风机-第一部分:任意涡流的数值有效空气动力学模型
机译:主动流动控制的扇翼气动性能的数值研究。
机译:跨音速风扇转子叶尖泄漏不定源机理的数值研究
机译:自激叶尖流动不稳定性和叶片行相互作用对低速和跨音速压缩机转子性能预测影响的数值研究。
机译:雪弗龙混合器内部空气动力和燃烧性能的数值研究
机译:讨论:“转子设计尖端速度对静态和横向条件下的型号VTOL升力风扇的空气动力学性能”(Stockman,No,Loeffler,As和Liebein,S.,1973,Asme J. Eng。Power,95, PP。293-300)