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| 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:298/85  |  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 |
| 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 |
| Formation of stabilized oblique detonation waves in a combustor 期刊论文 COMBUSTION AND FLAME, 2021, 卷号: 223, 页码: 423-436 作者: Zhang ZJ(张子健); Wen, Chihyung; Zhang WS(张文硕); Liu YF(刘云峰); Jiang ZL(姜宗林) Adobe PDF(3599Kb)  |  收藏  |  浏览/下载:328/89  |  提交时间:2021/03/03 Oblique detonation wave Combustor Oblique detonation engine Normal detonation wave Boundary layer separation |
| Advances in critical technologies for hypersonic and high-enthalpy wind tunnel 期刊论文 CHINESE JOURNAL OF AERONAUTICS, 2020, 卷号: 33, 期号: 12, 页码: 3027-3038 作者: Jiang ZL(姜宗林); Hu ZM(胡宗民); Wang YP(汪运鹏); Han GL(韩桂来) Adobe PDF(1129Kb)  |  收藏  |  浏览/下载:322/169  |  提交时间:2021/03/30 High-enthalpy flow Hypersonic wind tunnel Aerospace vehicle Aerodynamic balance Heat flux sensor Optical measurement technique |
| A Data-Correlation Model of Aerodynamic Heating Based on Globally Optimal Learning Method 会议论文 16th International Conference on Natural Computation, Fuzzy Systems and Knowledge Discovery (ICNC-FSKD 2020), 西安,中国, 19-21 December 2020 作者: Chen Z(陈阵); Li S(李森); Luo ZT(罗长童); Jiang ZL(姜宗林) Adobe PDF(1545Kb)  |  收藏  |  浏览/下载:147/39  |  提交时间:2021/02/01 |
| Impulse force-measurement system 期刊论文 SHOCK WAVES, 2020, 页码: 11 作者: Wang YP(汪运鹏); Jiang ZL(姜宗林) Adobe PDF(1551Kb)  |  收藏  |  浏览/下载:239/67  |  提交时间:2020/11/30 Shock tunnel High enthalpy Aerodynamic force measurement Strain gauge balance |
| 基于第二粘性的Navier-Stokes方程组求解正激波结构 期刊论文 计算物理, 2020, 卷号: 37, 期号: 5, 页码: 505-513 作者: 李馨东; 赵英奎; 胡宗民; 姜宗林 浏览  |  Adobe PDF(812Kb)  |  收藏  |  浏览/下载:345/76  |  提交时间:2019/12/16 Navier-Stokes方程 Stokes假设 第二粘性 体积粘性,正激波结构 |
| On theory and methods for advanced detonation-driven hypervelocity shock tunnels 期刊论文 NATIONAL SCIENCE REVIEW, 2020, 卷号: 7, 期号: 7, 页码: 1198-1207 作者: Jiang ZL(姜宗林); Li JP(李进平); Hu ZM(胡宗民); Liu YF(刘云峰); Yu HR(俞鸿儒) Adobe PDF(1090Kb)  |  收藏  |  浏览/下载:252/101  |  提交时间:2020/11/30 hypervelocity shock tunnel detonation driver flight condition tailored condition test facilities |