机译:低扫跨音速层流翼的冲击控制
Nanjing Univ Aeronaut & Astronaut, Coll Aerosp Engn, Nanjing, Jiangsu, Peoples R China|Univ Sheffield, Dept Mech Engn, Sheffield S1 3JD, S Yorkshire, England;
China Aerodynam Res & Dev Ctr, High Speed Aerodynam Inst, Mianyang 621000, Sichuan, Peoples R China|Univ Sheffield, Dept Mech Engn, Sheffield S1 3JD, S Yorkshire, England;
Univ Sheffield, Dept Mech Engn, Aerodynam, Sheffield S1 3JD, S Yorkshire, England|AIAA, Reston, VA 20191 USA;
China Aerodynam Res & Dev Ctr, High Speed Aerodynam Inst, Mianyang 621000, Sichuan, Peoples R China;
Nanjing Univ Aeronaut & Astronaut, Coll Aerosp Engn, Nanjing, Jiangsu, Peoples R China;
Nanjing Univ Aeronaut & Astronaut, Coll Aerosp Engn, Nanjing, Jiangsu, Peoples R China;
Nanjing Univ Aeronaut & Astronaut, Coll Aerosp Engn, Nanjing, Jiangsu, Peoples R China;
机译:低扫跨音速机翼的气动结构设计研究
机译:低扫跨音速机翼的气动结构设计研究
机译:跨音速层流翼式手套的计算评估和线性稳定性
机译:低扫跨跨跨翼翼型低扫跨桥翼的空气动力学 - 结构设计研究
机译:用于分析以下内容的高分辨率TVD方案:I.超音速和跨音速无粘性流。二。粘性流具有激振引起的分离和热传递。
机译:冲击反射/衍射中的自由边界问题以及相关的跨音速流动问题
机译:低扫型跨型跨音层流动翼的冲击控制