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机译:基于支柱的超燃冲压燃烧器燃烧模式过渡效应的实验研究
School of Energy Science and Engineering, Harbin Institute of Technology, Heilongjiang, People's Republic of China;
School of Energy Science and Engineering, Harbin Institute of Technology, Heilongjiang, People's Republic of China;
School of Energy Science and Engineering, Harbin Institute of Technology, Heilongjiang, People's Republic of China;
School of Energy Science and Engineering, Harbin Institute of Technology, Heilongjiang, People's Republic of China;
School of Energy Science and Engineering, Harbin Institute of Technology, Heilongjiang 150001, People's Republic of China;
Scramjet combustor; combustion mode transition; thrust; sudden change; flow field;
机译:基于Strut的Scramjet燃烧器模型中燃烧模式转变的动态特性
机译:典型基于支杆的超燃冲压燃烧器对燃烧流场的参数影响
机译:典型的基于杆和基于腔杆的超燃冲压燃烧器模式转换中的非线性过程
机译:基于Strut的Scramjet燃烧器模型中燃烧模式转变的动态特性的实验研究
机译:实验室双模式超燃冲压燃烧器的燃烧稳定性,结构和扩散。
机译:具有观察水平随机效应推动者-滞留效应和动态协变量的聚类多状态模型:在银屑病关节炎研究中模拟转变强度和停留时间
机译:典型基于支杆的超燃冲压燃烧器对燃烧流场的参数影响
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