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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：297/85 | 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：105/2 | 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：241/23 | 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：305/53 | 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：79/0 | 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：280/55 | 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：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 |
| 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：265/109 | 提交时间：2021/01/29
Shock-shock interaction Machine learning Hypersonic flow Impinging jet Genetic programming Triple point |
