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机译:非绝热小波/进度可变方法在加压条件下H_2 / O_2燃烧大涡模拟中的应用
Department of Mechanical Engineering and Science, Advanced Research Institute of Fluid Science and Engineering, Kyoto University, Kyoto daigaku-Katsura, Nishikyo-ku, Kyoto, Japan;
Nagoya Guidance and Propulsion Systems Works, Mitsubishi Heavy Industries Ltd., 1200 Higashi Tanaka, Komaki, Aichi, Japan;
Department of Mechanical Engineering and Science, Advanced Research Institute of Fluid Science and Engineering, Kyoto University, Kyoto daigaku-Katsura, Nishikyo-ku, Kyoto, Japan;
Numerical Flow Designing Co., Ltd., 1-10-10 Higashi-Gotanda, Shinagawa-ku, Tokyo, Japan;
Nagoya Guidance and Propulsion Systems Works, Mitsubishi Heavy Industries Ltd., 1200 Higashi Tanaka, Komaki, Aichi, Japan;
Nagoya Guidance and Propulsion Systems Works, Mitsubishi Heavy Industries Ltd., 1200 Higashi Tanaka, Komaki, Aichi, Japan;
Department of Mechanical Engineering and Science, Advanced Research Institute of Fluid Science and Engineering, Kyoto University, Kyoto daigaku-Katsura, Nishikyo-ku, Kyoto, Japan;
机译:基于小波进度可变方法的湍流非预混燃烧的SMLD联合PDF模型
机译:挥动/进展可变方法的评估和撞击生成的层流逆流扩散火焰中的歧管方法
机译:一维H_2 / O_2逆流扩散火焰模拟超临界压力下小火焰台构造
机译:大涡仿真及多标量挥动方法对甲烷 - 氢气混合燃烧型工业燃气轮机燃烧器的应用
机译:大涡模拟湍流燃烧的进度可变方法。
机译:湍流燃烧模拟的加厚随机场方法
机译:喷射燃烧数值模拟的爆发/进展变量方法的有效性