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机译:煤油燃料的火箭联合循环发动机燃烧室的燃烧振荡研究
Northwestern Polytech Univ, Sci & Technol Combust Internal Flow & Thermal Str, Xian 710072, Shaanxi, Peoples R China;
Northwestern Polytech Univ, Sci & Technol Combust Internal Flow & Thermal Str, Xian 710072, Shaanxi, Peoples R China;
Northwestern Polytech Univ, Sci & Technol Combust Internal Flow & Thermal Str, Xian 710072, Shaanxi, Peoples R China|Northwestern Polytech Univ, Sch Astronaut, Xian 710072, Shaanxi, Peoples R China;
Northwestern Polytech Univ, Sci & Technol Combust Internal Flow & Thermal Str, Xian 710072, Shaanxi, Peoples R China;
Northwestern Polytech Univ, Sci & Technol Combust Internal Flow & Thermal Str, Xian 710072, Shaanxi, Peoples R China;
Northwestern Polytech Univ, Sci & Technol Combust Internal Flow & Thermal Str, Xian 710072, Shaanxi, Peoples R China;
Rocket-based combined-cycle; Large eddy simulation; Combustion oscillation; Flame dynamics; Ground test;
机译:基于煤油燃料的火箭联合循环发动机燃烧器的燃烧振荡研究(第129卷,第260页,2016年)
机译:基于煤油燃料的火箭联合循环发动机燃烧室燃烧特性的大涡模拟
机译:煤油超燃冲压燃烧器燃烧特性的实验研究
机译:在升高的压力和温度下的燃烧振荡下,稀薄级航空发动机燃烧器的预混合风道和燃烧室内部同时显示煤油/ OH LIF
机译:雷诺数平均Navier-Stokes对带有独立燃料冲压发动机流的基于模型的基于火箭的联合循环发动机的流量的分析。
机译:使用附加的预混合燃料喷嘴减少阶段式飞机发动机燃烧室的排放
机译:煤油替代燃料在特殊车辆柴油发动机燃烧特性研究
机译:FBC(流化床燃烧器)工程相关性估算一系列燃料的燃烧效率