...
机译:超高速超燃冲压发动机燃烧场的数值研究
Northwestern Polytech Univ, Sci & Technol Combust Internal Flow & Thermostruc, Xian 710072, Shaanxi, Peoples R China;
Northwestern Polytech Univ, Sci & Technol Combust Internal Flow & Thermostruc, Xian 710072, Shaanxi, Peoples R China;
Northwestern Polytech Univ, Sci & Technol Combust Internal Flow & Thermostruc, Xian 710072, Shaanxi, Peoples R China;
Northwestern Polytech Univ, Sci & Technol Combust Internal Flow & Thermostruc, Xian 710072, Shaanxi, Peoples R China;
Northwestern Polytech Univ, Sci & Technol Combust Internal Flow & Thermostruc, Xian 710072, Shaanxi, Peoples R China;
Hypervelocity; Hypersonic combustion; Scramjet; Numerical investigation;
机译:带有双腔火焰架的煤油超燃冲压发动机燃烧机理的实验研究
机译:汽轮燃烧室上游新月腔燃烧特性的数值研究
机译:基于腔的超燃喷射燃烧室中支柱轮廓对燃烧特性的影响的数值研究
机译:双模式超燃冲压发动机中燃烧/冲击波相互作用的数值研究
机译:使用Wind-US进行氢空气燃烧的UVA冲压/超冲压超音速发动机的数值模拟。
机译:GDI发动机燃烧状态的数值评估
机译:超高速条件下三维超燃冲压发动机的实验研究
机译:通过超燃冲压发动机燃烧室模型进行超高速混合和燃烧的数值研究