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| Study on aerodynamic loads at the inlet's cowl lip induced by multiple shock-shock interferences 期刊论文 ACTA MECHANICA SINICA, 2024, 卷号: 40, 期号: 4, 页码: 12 Authors: Lin MY(林明月); Yang F(杨帆); Hu ZM(胡宗民); Han GL(韩桂来) Favorite  |  View/Download:10/0  |  Submit date:2024/05/27 Shock waves Shock-shock interaction Theoretical analysis Hysteresis |
| Experimental investigation of mode transition process in a cavity-based scramjet 期刊论文 PHYSICS OF FLUIDS, 2024, 卷号: 36, 期号: 4, 页码: 11 Authors: Meng Y(孟宇); Sun WM(孙文明); Gu HB(顾洪斌); Chen, Fang Favorite  |  View/Download:7/0  |  Submit date:2024/05/14 |
| Nonequilibrium Heating/Cooling Effects in a Mach Number 10 Hydrogen-Fueled Scramjet 期刊论文 JOURNAL OF PROPULSION AND POWER, 2024, 页码: 17 Authors: Liu H(刘杭); Yao W(姚卫); Zhang X(张旭); Zhang XY(张晓源); Liu, Jianwen; Yue LJ(岳连捷); Sun QH(孙泉华) Favorite  |  View/Download:54/0  |  Submit date:2024/03/11 Scramjet Dynamic Zone Flamelet Model High Enthalpy Shock Tunnel Combustors Improved Delayed Detached Eddy Simulation Vibrational Energy nonequilibrium heating cooling effects thermal nonequilibrium chemical nonequilibrium hydrogen |
| Detonation wave structure and thrust variation of a ram accelerator with different projectile velocities 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2023, 卷号: 143, 页码: 8 Authors: Shang JH(尚甲豪); Wang, Kuanliang; Wang, Aifeng; Wang Q(汪球); Zhao W(赵伟) Adobe PDF(4127Kb)  |  Favorite  |  View/Download:96/13  |  Submit date:2024/01/02 Ram accelerator Detonation Oblique detonation wave Recirculation zone |
| 激波风洞两级入轨飞行器纵向级间分离试验技术 期刊论文 航空学报, 2023, 卷号: 44, 期号: 17, 页码: 128126 Authors: 王粤; 汪运鹏; 姜宗林 Adobe PDF(6797Kb)  |  Favorite  |  View/Download:395/39  |  Submit date:2022/12/01 两级入轨 轨迹捕获 激波风洞 多体分离 动态试验 试验技术 |
| Decomposition of mean skin friction in incident shock wave/turbulent boundary layer interaction flows at Mach 2.25 期刊论文 CHINESE JOURNAL OF AERONAUTICS, 2023, 卷号: 36, 期号: 9, 页码: 178-194 Authors: Duan JY(段俊亦); Tong FL(童福林); Li XL(李新亮); Liu HW(刘洪伟) Adobe PDF(6039Kb)  |  Favorite  |  View/Download:121/8  |  Submit date:2023/11/13 Compressible flow Boundary layers Direct numerical simulation Shock waves Skin friction Turbulent flow |
| Coupling Effect of Multicavity on Flame Stabilization Mode Transitions in Scramjet Combustor 期刊论文 JOURNAL OF PROPULSION AND POWER, 2023 Authors: Wu ZJ(吴振杰); Zhang QF(张启帆); Yu FY(于方游); Luo WH(罗苇航); Gao ZB(高占彪); Yue LJ(岳连捷) Adobe PDF(582Kb)  |  Favorite  |  View/Download:56/7  |  Submit date:2023/06/15 Scramjet Engines Combustor Design flame stabilization mode transition path dependence |
| Characterization and predictive modeling of a trajectory oriented dual mode scramjet combustor 期刊论文 PHYSICS OF FLUIDS, 2023, 卷号: 35, 期号: 2, 页码: 26108 Authors: Zhou RX(周芮旭); Li, Tuo; Li, Xinyang; Lian H(连欢) Adobe PDF(6713Kb)  |  Favorite  |  View/Download:61/6  |  Submit date:2023/04/20 |
| 一种并联两级入轨飞行器纵向分离方案的数值研究 期刊论文 航空学报, 2023, 卷号: 44, 期号: 11, 页码: 127634 Authors: 王粤; 汪运鹏; 王春; 姜宗林 Adobe PDF(4901Kb)  |  Favorite  |  View/Download:603/90  |  Submit date:2022/07/11 两级入轨 高超声速 纵向分离 气动干扰 非定常流动 |
| Numerical Investigation on Longitudinal Stage Separation of Spiked Two-Stage-to-Orbit Vehicle 期刊论文 Journal of Spacecraft and Rockets, 2023, 卷号: 60, 期号: 1, 页码: 215-229 Authors: Wang Y(王粤); Wang YP(汪运鹏); Wang C(王春); Jiang ZL(姜宗林) Adobe PDF(5479Kb)  |  Favorite  |  View/Download:410/78  |  Submit date:2022/08/24 Multistage Launch Vehicle Aerodynamic Characteristics Shock Wave Interaction Angle of Attack Waverider Boundary Layer Flow Total Variation Diminishing Adverse Pressure Gradient Hypersonic Flows Hypersonic Wind Tunnels |