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| 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:312/92  |  提交时间:2022/11/14 Two-stage to orbit Numerical simulation Stage separation Hypersonic flow Aerodynamic interference |
| 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:111/2  |  提交时间:2023/03/23 |
| 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:253/27  |  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:316/56  |  提交时间:2022/01/12 |
| Numerical Simulation Research on Thermal Response Characteristics of E-type Coaxial Thermocouples 会议论文 2021 2rd International Conference on Applied Mechanics and Mechanical Engineering, 长沙, 2021/09/12 作者: Qi L(齐力); Han GL(韩桂来); Jiang ZL(姜宗林) 收藏  |  浏览/下载:81/0  |  提交时间:2022/07/06 气动热 同轴热电偶 数值模拟 |
| 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:285/57  |  提交时间:2021/05/17 Concept demonstration Hypersonic propulsion Oblique detonation engine Scramjet Shock wave Supersonic combustion Wind tunnel test |
| 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:343/90  |  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:335/172  |  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:155/42  |  提交时间:2021/02/01 |
| Parameter-correlation study on shock-shock interaction using a machine learning method 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 107, 页码: 106247 作者: Peng J(彭俊); Luo ZT(罗长童); Han ZJ(韩子健); Hu ZM(胡宗民); Han GL(韩桂来); Jiang ZL(姜宗林) Adobe PDF(2818Kb)  |  收藏  |  浏览/下载:280/114  |  提交时间:2021/01/29 Shock-shock interaction Machine learning Hypersonic flow Impinging jet Genetic programming Triple point |