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机译:调查典型三维炒盘燃烧器模式过渡配有支柱的燃烧器
College of Aerospace Science and Engineering National University of Defense Technology Changsha Hunan 410073 China;
College of Aerospace Science and Engineering National University of Defense Technology Changsha Hunan 410073 China;
College of Aerospace Science and Engineering National University of Defense Technology Changsha Hunan 410073 China;
College of Aerospace Science and Engineering National University of Defense Technology Changsha Hunan 410073 China;
College of Aerospace Science and Engineering National University of Defense Technology Changsha Hunan 410073 China;
Dual-mode; Mode transition; Strut; Hysteresis phenomenon; Scramjet combustor;
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:基于支撑的双模超燃冲压燃烧器的冲压-冲压过渡机理的数值研究
机译:研究支撑结构和位置对典型超燃冲压燃烧器燃烧性能的影响
机译:典型基于弹壳燃烧器的流场湍流模型研究
机译:双模超燃冲压发动机:对燃烧室设计和运行的计算研究。
机译:流内塔架和支柱对超燃冲压燃烧器性能的影响研究
机译:Scramjet燃烧器中支柱坡道注射器的研究:支柱几何,燃料和喷射直径对混合特性的影响
机译:超燃冲压发动机燃气混合,点火和火焰稳定的数值研究