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机译:具有3D侧壁压缩入口的超燃冲压发动机中氢燃烧的数值研究
Science and Technology on Scramjet Laboratory, National University of Defense Technology, Changsha 410073, Hunan, PR China;
Science and Technology on Scramjet Laboratory, National University of Defense Technology, Changsha 410073, Hunan, PR China;
Science and Technology on Scramjet Laboratory, National University of Defense Technology, Changsha 410073, Hunan, PR China;
Science and Technology on Scramjet Laboratory, National University of Defense Technology, Changsha 410073, Hunan, PR China;
Supersonic combustion; Inlet distortion; Sidewall compression inlet; CFD;
机译:进气式热压超燃冲压发动机燃烧行为的数值研究
机译:超燃冲压发动机进气道侧壁压缩和内部收缩的实验研究
机译:超燃冲压发动机进气口中侧壁压缩和再分层的影响
机译:3D超燃冲压发动机进气道中侧壁压缩和再分层作用的数值研究
机译:使用Wind-US进行氢空气燃烧的UVA冲压/超冲压超音速发动机的数值模拟。
机译:Scramjet入口模型中的开始和解置现象的数值研究
机译:进气式热压超燃冲压发动机燃烧行为的数值研究
机译:10马赫的通用侧壁压缩超燃冲压发动机进气道的雷诺数和兜帽位置效应:计算和实验研究