已选(0)清除
条数/页: 排序方式: |
| 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:363/69  |  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:291/83  |  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:305/81  |  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 |
| TSTO马赫7安全级间分离问题的数值研究 期刊论文 力学学报, 2022, 卷号: 54, 期号: 2, 页码: 526-542 作者: 王粤; 汪运鹏; 薛晓鹏; 姜宗林 Adobe PDF(3565Kb)  |  收藏  |  浏览/下载:342/70  |  提交时间:2021/12/23 两级入轨 高超声速 分离流动 气动干扰 级间分离 |
| 高超声速高焓条件下的内嵌式温敏漆测量方法 期刊论文 力学学报, 2022, 卷号: 54, 期号: 01, 页码: 48-58 作者: 苑朝凯; 姜宗林 Adobe PDF(1381Kb)  |  收藏  |  浏览/下载:125/28  |  提交时间:2022/03/16 温敏漆 热流密度场 辐射效应 高超声速流动 辨识方法 |
| 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:104/2  |  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:140/27  |  提交时间:2022/06/10 Boundary layer correction High-enthalpy flow Hypersonic wind tunnel Nozzle design Real-gas effects |
| Numerical investigation of free oblique detonation wave induced by non-intrusive energy deposition 期刊论文 AIP ADVANCES, 2021, 卷号: 11, 期号: 12, 页码: 17 作者: Zhang WS(张文硕); Zhang, Zijian; Jiang ZL(姜宗林); Han X(韩信); Liu, Yunfeng; Wang, Chun Adobe PDF(15045Kb)  |  收藏  |  浏览/下载:234/22  |  提交时间:2022/01/24 |
| Simulation on Three-Dimensional Shock Interactions and Aerodynamic Heating Between Body and Wing 期刊论文 AIAA JOURNAL, 2021, 页码: 12 作者: Lin MY(林明月); Wang C(王春); Peng J(彭俊); Jiang ZL(姜宗林) Adobe PDF(4805Kb)  |  收藏  |  浏览/下载:299/52  |  提交时间:2022/01/12 |
| Criteria for hypersonic airbreathing propulsion and its experimental verification 期刊论文 CHINESE JOURNAL OF AERONAUTICS, 2021, 卷号: 34, 期号: 3, 页码: 94-104 作者: Jiang ZL(姜宗林); Zhang ZJ(张子健); Liu YF(刘云峰); Wang C(王春); Luo ZT(罗长童) Adobe PDF(1806Kb)  |  收藏  |  浏览/下载:278/54  |  提交时间:2021/05/17 Concept demonstration Hypersonic propulsion Oblique detonation engine Scramjet Shock wave Supersonic combustion Wind tunnel test |