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| 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:324/86  |  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:113/2  |  提交时间:2023/03/23 |
| 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:320/58  |  提交时间:2022/01/12 |
| Noise reduction for temperature-sensitive paint measurement contaminated by strong background radiation in a high enthalpy hypersonic tunnel 期刊论文 ACTA MECHANICA SINICA, 2021, 页码: 7 作者: Peng, Di; Liu, Xu; Jiao, Lingrui; Li, Ziyan; Wen, Xin; Yuan CK(苑朝凯); Han GL(韩桂来); Liu YF(刘云峰); Liu, Yingzheng; Jiang ZL(姜宗林) Adobe PDF(3477Kb)  |  收藏  |  浏览/下载:266/53  |  提交时间:2021/03/30 Temperature-sensitive paint Time-resolved measurement Hypersonic flow Background radiation |
| Experimental investigation of hypersonic flight-duplicated shock tunnel characteristics 期刊论文 ACTA MECHANICA SINICA, 2021, 页码: 12 作者: Yuan CK(苑朝凯); Jiang ZL(姜宗林) Adobe PDF(3790Kb)  |  收藏  |  浏览/下载:398/63  |  提交时间:2021/03/03 Hypersonics Shock tunnels Flow characteristics |
| 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:346/90  |  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:337/173  |  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:156/42  |  提交时间:2021/02/01 |
| Intelligent Force-Measurement System Use in Shock Tunnel 期刊论文 SENSORS, 2020, 卷号: 20, 期号: 21, 页码: 6179 作者: Wang YP(汪运鹏); Jiang ZL(姜宗林) Adobe PDF(2149Kb)  |  收藏  |  浏览/下载:190/55  |  提交时间:2020/12/28 artificial intelligence BALANCE SYSTEM deep learning DESIGN dynamic calibration FLOWS force-measurement system strain-gauge balance |
| 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:256/75  |  提交时间:2020/11/30 Shock tunnel High enthalpy Aerodynamic force measurement Strain gauge balance |