机译:背压和分流器引起的TBCC入口过低的启动/重启滞后特性分析
Science and Technology on Scramjet Laboratory, Hypervelocity Aerodynamics Institute of CARDC,Harbin Institute of Technology;
Harbin Institute of Technology;
Harbin Institute of Technology;
Harbin Institute of Technology;
Harbin Institute of Technology;
Harbin Institute of Technology;
Harbin Institute of Technology;
Turbine-based combined cycle (TBCC); Inlet mode transition; Unstart/restart hysteresis; Backpressure; Splitter;
机译:控制路线对TBCC进气不足的起动/重启特性的影响
机译:边界层渗出对高超音速进气口启动/重启特性的影响
机译:基于信息融合的超燃冲压发动机进气口反压启动检测
机译:基于涡轮机的组合循环(TBCC)入口模式过渡的空气动力学设计与数值模拟
机译:多模块高超声速进气的起步耦合机理分析
机译:透平式联合循环进气模式过渡的气动设计和数值模拟
机译:TBCC进口实验和分析