机译:Scramjet中冲击波影响剪切层生长的研究
Northwestern Polytech Univ, Sci & Technol Combust, Internal Flow & Thermal Struct Lab, Xian 710072, Peoples R China;
Northwestern Polytech Univ, Sci & Technol Combust, Internal Flow & Thermal Struct Lab, Xian 710072, Peoples R China;
Northwestern Polytech Univ, Sci & Technol Combust, Internal Flow & Thermal Struct Lab, Xian 710072, Peoples R China;
Northwestern Polytech Univ, Sci & Technol Combust, Internal Flow & Thermal Struct Lab, Xian 710072, Peoples R China;
Northwestern Polytech Univ, Sci & Technol Combust, Internal Flow & Thermal Struct Lab, Xian 710072, Peoples R China;
Northwestern Polytech Univ, Sci & Technol Combust, Internal Flow & Thermal Struct Lab, Xian 710072, Peoples R China;
机译:高速冲击波相互作用中剪切层失稳对船首激波的影响
机译:扰波效应对扰燃燃烧室湍流混合层的冲击波效应的数值评价
机译:剪切敏感液晶涂层在超声速冲击波中测量壁面剪应力的研究
机译:模型冲压发动机中冲击波影响剪切层生长的数值研究
机译:通过环形管道(SCRAMJET)进行超音速流场中冲击波和湍流边界层相互作用的实验研究。
机译:影响3C夹杂物发生的因素的调查用于轴上的轴C面4H-SIC外延层
机译:超燃冲压发动机进气流的冲击波边界层相互作用研究
机译:三维激波波边界层相互作用的研究。掠过冲击/湍流边界层相互作用的流场模型