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| Numerical investigations of the lateral heat transfer in coaxial thermocouples 期刊论文
NUMERICAL HEAT TRANSFER PART A-APPLICATIONS, 2022, 页码: 19
作者: Qi L(齐力) ; Han GL(韩桂来); Hu ZM(胡宗民); Wang C(王春); Jiang ZL(姜宗林)
 Adobe PDF(3726Kb) |  收藏 | 浏览/下载：242/48 | 提交时间：2022/07/18
Coaxial thermocouples lateral heat transfer maximum temperature point numerical simulation surface heat flux |
| Mechanisms of the destabilized Mach reflection of inviscid oblique detonation waves before an expansion corner 期刊论文
JOURNAL OF FLUID MECHANICS, 2022, 卷号: 940, 页码: 39
作者: Zhang, Zijian; Liu YF(刘云峰); Wen, Chihyung
Adobe PDF(1777Kb) | 收藏 | 浏览/下载：145/34 | 提交时间：2022/05/17
detonation waves |
| Evolution of heat transfer at the stagnation point during the detached bow shock establishment 期刊论文
SHOCK WAVES, 2021, 页码: 8
作者: Wang Q(汪球); Li JP(李进平); Luo K(罗凯); Li JW(栗继伟); Zhao W(赵伟)
Adobe PDF(1158Kb) | 收藏 | 浏览/下载：243/52 | 提交时间：2021/05/17
Hypersonic Aerodynamic heating Detached bow shock Shock tube expansion tube |
| 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：278/54 | 提交时间：2021/05/17
Concept demonstration Hypersonic propulsion Oblique detonation engine Scramjet Shock wave Supersonic combustion Wind tunnel test |
| 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：380/57 | 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：327/89 | 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：320/168 | 提交时间：2021/03/30
High-enthalpy flow Hypersonic wind tunnel Aerospace vehicle Aerodynamic balance Heat flux sensor Optical measurement technique |
| Numerical investigation of a Mach 9 oblique detonation engine with fuel pre-injection 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 105, 页码: 9
作者: Zhang ZJ(张子健); Ma KF(马凯夫); Zhang WS(张文硕); Han X(韩鑫); Liu YF(刘云峰); Jiang ZL(姜宗林)
Adobe PDF(2608Kb) | 收藏 | 浏览/下载：265/110 | 提交时间：2020/11/30
Oblique detonation engine Pre-injection Detonative combustion Mixing Hydrogen |
| 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 |
| Experimental Investigation of Hypervelocity Flow in an Expansion Tunnel 期刊论文
AIAA JOURNAL, 2020, 卷号: 58, 期号: 6, 页码: 2776-2783
作者: Yuan CK(苑朝凯); Zhou K(周凯); Hu ZM(胡宗民); Liu YF(刘云峰); Jiang ZL(姜宗林)
Adobe PDF(1471Kb) | 收藏 | 浏览/下载：232/57 | 提交时间：2020/07/06 |
