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机译:冲击隧道中节流引起的超音速进气道的非稳态行为
University of Science and Technology of China, 230027 Hefei, People's Republic of China,Modern Mechanics Department;
University of Science and Technology of China, 230027 Hefei, People's Republic of China,Modern Mechanics Department;
University of Science and Technology of China, 230027 Hefei, People's Republic of China,Modern Mechanics Department;
University of Science and Technology of China, 230027 Hefei, People's Republic of China,Modern Mechanics Department;
机译:平移整流罩在高超声速进气道中冲击波行为的数值研究
机译:冲击波隧道中超音速喷嘴入口启动特性的数值研究
机译:使用冲击隧道实验测量侧壁压缩超燃冲压发动机进气口周围的高超声速流场
机译:节流下高超声道入口不稳定行为的数值研究
机译:熵的考虑适用于高超声速入口的冲击不稳定。
机译:生产sOUND非稳定节流流入谐振腔的随着应用程序来浊音
机译:节流下高超声速进气道非稳态行为的数值研究