机译:湍流模型和缝隙宽度对超声速流动中横向缝隙注入流场的影响
Science and Technology on Scramjet Laboratory, National University of Defense Technology, Changsha, Hunan 410073, People's Republic of China;
Science and Technology on Scramjet Laboratory, National University of Defense Technology, Changsha, Hunan 410073, People's Republic of China;
Science and Technology on Scramjet Laboratory, National University of Defense Technology, Changsha, Hunan 410073, People's Republic of China;
Science and Technology on Scramjet Laboratory, National University of Defense Technology, Changsha, Hunan 410073, People's Republic of China;
Science and Technology on Scramjet Laboratory, National University of Defense Technology, Changsha, Hunan 410073, People's Republic of China;
Science and Technology on Scramjet Laboratory, National University of Defense Technology, Changsha, Hunan 410073, People's Republic of China;
aerospace propulsion system; transverse jet; turbulence model; slot width; supersonic flow; length of the upstream separation region; height of the mach surface;
机译:超声速流中入射激波与横向缝隙注入相互作用的数值预测
机译:流向缝隙对横向气体注入流场流动和混合特性的参数影响:数值研究
机译:超声速流动中横向槽注入的计算研究
机译:超音速流动中横向注入和拟激波引起的湍流
机译:鱼道垂直槽内的流场:John Day大坝的湍流,速度和槽长的影响以及Lamprey过道系统的设计。
机译:新型熔喷气流场的数值分析双槽喷气机模具
机译:横向燃料喷射的不稳定三维分析使用独立涡流模拟第二部分:反应流域