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| Experimental and numerical investigation on the unsteady interaction in longitudinal stage separation for parallel-staged two-body configuration 期刊论文 Physics of Fluids, 2024, 卷号: 36, 页码: 016116 作者: Wang Y(王粤); Wang YP(汪运鹏); Jiang ZL(姜宗林) Adobe PDF(7258Kb)  |  收藏  |  浏览/下载:80/15  |  提交时间:2024/01/15 Two-stage-to-orbit Wind tunnel test Numerical simulation Stage separation Hypersonic Shock waves |
| Characteristics of cellular structure of detonation waves propagating in annular channels 期刊论文 PHYSICS OF FLUIDS, 2023, 卷号: 35, 期号: 10, 页码: 13 作者: Yao KP(姚克鹏); Yang PF(杨鹏飞); Wang C(王春); Jiang ZL(姜宗林) Adobe PDF(8005Kb)  |  收藏  |  浏览/下载:28/2  |  提交时间:2024/02/19 |
| Numerical investigation of unsteady aerodynamic characteristics induced by the interaction of oblique/bow shock waves during rotation 期刊论文 PHYSICS OF FLUIDS, 2023, 卷号: 35, 期号: 8, 页码: 86124 作者: Wang DG(王大高); Han GL(韩桂来); Liu MK(刘美宽); Jiang ZL(姜宗林) Adobe PDF(10056Kb)  |  收藏  |  浏览/下载:50/0  |  提交时间:2023/09/26 |
| 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 作者: Wang Y(王粤); Wang YP(汪运鹏); Wang C(王春); Jiang ZL(姜宗林) Adobe PDF(5479Kb)  |  收藏  |  浏览/下载:366/69  |  提交时间: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 |
| Numerical Investigation of Aerodynamic Separation Schemes for Two-Stage-to-Orbit-like Two-body System 期刊论文 Aerospace Science and Technology, 2022, 卷号: 131, 期号: Part A, 页码: 107995 作者: Wang Y(王粤); Wang YP(汪运鹏); Jiang ZL(姜宗林) Adobe PDF(9707Kb)  |  收藏  |  浏览/下载:297/85  |  提交时间:2022/11/14 Two-stage to orbit Numerical simulation Stage separation Hypersonic flow Aerodynamic interference |
| Experimental Study of Longitudinal Stage Separation of Two-Body Configuration in Shock Tunnel 期刊论文 AIAA Journal, 2022, 卷号: 60, 期号: 12, 页码: 6940-6946 作者: Wang Y(王粤); Wang YP(汪运鹏); Jiang ZL(姜宗林) Adobe PDF(2434Kb)  |  收藏  |  浏览/下载:309/82  |  提交时间:2022/08/23 Aerodynamic Coefficients Two Stage to Orbit Aerodynamic Performance Hypersonic Flight Hypersonic Wind Tunnels Solenoid Valves Oblique Shock Pneumatic Actuator Hypersonic Flows Computer Aided Engineering |
| Oblique detonation wave triggered by a double wedge in hypersonic flow 期刊论文 CHINESE JOURNAL OF AERONAUTICS, 2022, 卷号: 35, 期号: 4, 页码: 176-184 作者: Teng, Honghui; Zhang, Yuhang; Yang PF(杨鹏飞); Jiang ZL(姜宗林) Adobe PDF(1747Kb)  |  收藏  |  浏览/下载:163/33  |  提交时间:2022/07/18 Double wedge Hypersonic flow Initiation structures Oblique detonation Shock interactions |
| A numerical study of oblique detonation re-stabilization by expansion waves 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2022, 卷号: 122, 页码: 8 作者: Yao KP(姚克鹏); Wang C(王春); Jiang ZL(姜宗林) Adobe PDF(1789Kb)  |  收藏  |  浏览/下载:211/37  |  提交时间:2022/06/10 Oblique detonation Stationary Thermal choking Expansion waves |
| Gaseous Detonation Physics and Its Universal Framework Theory 专著 Beijing:Springer Nature, 2022 作者: Jiang ZL(姜宗林); Teng, Honghui Adobe PDF(13641Kb)  |  收藏  |  浏览/下载:105/2  |  提交时间:2023/03/23 |
| Theories and methods for designing hypersonic high-enthalpy flow nozzles 期刊论文 CHINESE JOURNAL OF AERONAUTICS, 2022, 卷号: 35, 期号: 1, 页码: 318-339 作者: Wang YP(汪运鹏); Jiang ZL(姜宗林) Adobe PDF(2554Kb)  |  收藏  |  浏览/下载:143/28  |  提交时间:2022/06/10 Boundary layer correction High-enthalpy flow Hypersonic wind tunnel Nozzle design Real-gas effects |