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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
Authors: Wang Y(王粤) ; Wang YP(汪运鹏); Jiang ZL(姜宗林)
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Two-stage to orbit Numerical simulation Stage separation Hypersonic flow Aerodynamic interference |
| 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
Authors: 王粤; 汪运鹏; 薛晓鹏; 姜宗林
Adobe PDF(3565Kb) | Favorite | View/Download：396/82 | Submit date：2021/12/23
两级入轨 高超声速 分离流动 气动干扰 级间分离 |
| Gaseous Detonation Physics and Its Universal Framework Theory 专著
Beijing:Springer Nature, 2022
Authors: Jiang ZL(姜宗林); Teng, Honghui
 Adobe PDF(13641Kb) | Favorite | View/Download：128/2 | Submit date：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
Authors: Zhang WS(张文硕); Zhang, Zijian; Jiang ZL(姜宗林); Han X(韩信); Liu YF(刘云峰); Wang C(王春)
Adobe PDF(15045Kb) | Favorite | View/Download：269/31 | Submit date：2022/01/24 |
| 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
Authors: Jiang ZL(姜宗林); Zhang ZJ(张子健); Liu YF(刘云峰); Wang C(王春); Luo ZT(罗长童)
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Concept demonstration Hypersonic propulsion Oblique detonation engine Scramjet Shock wave Supersonic combustion Wind tunnel test |
| 斜爆轰发动机燃烧机理试验研究 期刊论文
推进技术, 2021, 卷号: 42, 期号: 04, 页码: 786-794
Authors: 张子健; 韩信; 马凯夫; 张文硕; 刘云峰; 苑朝凯; 姜宗林
Adobe PDF(6817Kb) | Favorite | View/Download：285/83 | Submit date：2021/04/19
斜爆轰发动机 超声速燃烧 激波诱导燃烧 斜爆轰波 斜激波 |
| Formation of stabilized oblique detonation waves in a combustor 期刊论文
COMBUSTION AND FLAME, 2021, 卷号: 223, 页码: 423-436
Authors: 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) | Favorite | View/Download：380/94 | Submit date：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
Authors: Jiang ZL(姜宗林); Hu ZM(胡宗民); Wang YP(汪运鹏); Han GL(韩桂来)
Adobe PDF(1129Kb) | Favorite | View/Download：356/178 | Submit date：2021/03/30
High-enthalpy flow Hypersonic wind tunnel Aerospace vehicle Aerodynamic balance Heat flux sensor Optical measurement technique |
| Aerodynamic principles of shock-induced combustion ramjet engines 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 103, 页码: 8
Authors: Ma KF(马凯夫); Zhang ZJ(张子健); Liu YF(刘云峰); Jiang ZL(姜宗林)
Adobe PDF(1657Kb) | Favorite | View/Download：284/101 | Submit date：2020/08/26
Scramjet engines Shock-induced combustion ramjet engines Supersonic combustion Chapman-Jouguet detonation |
| 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
Authors: 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) | Favorite | View/Download：278/101 | Submit date：2020/11/30
hypervelocity shock tunnel detonation driver flight condition tailored condition test facilities |
