机译:基于火箭组合循环发动机腔曲线脉冲再生冷却通道超临界烃燃料的流动和热分析
Northwestern Polytech Univ Internal Flow &
Thermostruct Lab Sci &
Technol Combust Xian 710072 Shaanxi Peoples R China;
Northwestern Polytech Univ Internal Flow &
Thermostruct Lab Sci &
Technol Combust Xian 710072 Shaanxi Peoples R China;
Northwestern Polytech Univ Internal Flow &
Thermostruct Lab Sci &
Technol Combust Xian 710072 Shaanxi Peoples R China;
Northwestern Polytech Univ Internal Flow &
Thermostruct Lab Sci &
Technol Combust Xian 710072 Shaanxi Peoples R China;
Northwestern Polytech Univ Internal Flow &
Thermostruct Lab Sci &
Technol Combust Xian 710072 Shaanxi Peoples R China;
Northwestern Polytech Univ Internal Flow &
Thermostruct Lab Sci &
Technol Combust Xian 710072 Shaanxi Peoples R China;
Pyrolysis; Supercritical hydrocarbon; Curved channel; Dean vortices; Regenerative cooling;
机译:基于火箭组合循环发动机腔曲线脉冲再生冷却通道超临界烃燃料的流动和热分析
机译:用于跳闸发动机的再生冷却通道中超临界烃燃料流动的不均匀行为
机译:多模式火箭联合循环发动机中蓄冷塔的热分析
机译:AC-18-44349具有微肋的再生冷却通道中超临界碳氢化合物燃料的传热增强
机译:雷诺数平均Navier-Stokes对带有独立燃料冲压发动机流的基于模型的基于火箭的联合循环发动机的流量的分析。
机译:使用回收的向日葵油导致的生物柴油和棕榈油作为航空涡轮发动机燃料的实验研究
机译:液体火箭发动机冷却通道中碳氢化合物燃料传热强化系统的设计