机译:三维TBCC排气喷嘴的流场及性能分析
Jiangsu Province Key Laboratory of Aerospace Power System, College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics (NUAA), Nanjing, Jiangsu, China;
Jiangsu Province Key Laboratory of Aerospace Power System, College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics (NUAA), Nanjing, Jiangsu, China;
Shenyang Aircraft Design and Research Institute, Aviation Industry Corporation of China (AVIC), Shenyang, Liaoning, China;
Shenyang Aircraft Design and Research Institute, Aviation Industry Corporation of China (AVIC), Shenyang, Liaoning, China;
Jiangsu Province Key Laboratory of Aerospace Power System, College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics (NUAA), Nanjing, Jiangsu, China;
hypersonic vehicle; method of characteristics; mode transition; TBCC exhaust system; thrust performance;
机译:马赫数不均匀入口对超燃冲压喷嘴流场和性能的影响
机译:基于受限横向注入的冲击矢量控制喷嘴流场特性及性能研究
机译:环形塞式喷嘴流场分析
机译:空气动力学/几何参数对TBCC喷射器喷嘴性能的影响
机译:2DCD喷嘴的二次喷射推力矢量控制(SITVC)的性能分析和流场表征。
机译:太阳能驱动废气热电热泵回收系统的实验研究与性能分析
机译:排气喷嘴流场的三种Navier-Stokes解算器的比较