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| Nonequilibrium Heating/Cooling Effects in a Mach Number 10 Hydrogen-Fueled Scramjet 期刊论文
JOURNAL OF PROPULSION AND POWER, 2024, 页码: 17
作者: Liu H(刘杭); Yao W(姚卫) ; Zhang X(张旭); Zhang XY(张晓源); Liu, Jianwen; Yue LJ(岳连捷); Sun QH(孙泉华)
  收藏 | 浏览/下载：26/0 | 提交时间：2024/03/11
Scramjet Dynamic Zone Flamelet Model High Enthalpy Shock Tunnel Combustors Improved Delayed Detached Eddy Simulation Vibrational Energy nonequilibrium heating cooling effects thermal nonequilibrium chemical nonequilibrium hydrogen |
| Investigation of Burst Pressure of Flat-Scored Metal Diaphragms in Hypersonic Impulse Facilities 期刊论文
AIAA JOURNAL, 2024, 页码: 8
作者: Wang WT(王文韬); Wang Q(汪球); Li JP(李进平); Zhao W(赵伟); Gao, Liangjie; Liu, Zhongchen; Qian, Zhansen
收藏 | 浏览/下载：39/0 | 提交时间：2024/02/26
Finite Element Method Hypersonic Shock Tube/Tunnel Diaphragm Burst Pressure |
| Experimental and numerical investigation on the unsteady interaction in longitudinal stage separation for parallel-staged two-body configuration 期刊论文
Physics of Fluids, 2024, 卷号: 36, 页码: 016116
作者: Wang Y(王粤); Wang YP(汪运鹏); Jiang ZL(姜宗林)
Adobe PDF(7258Kb) | 收藏 | 浏览/下载：70/15 | 提交时间：2024/01/15
Two-stage-to-orbit Wind tunnel test Numerical simulation Stage separation Hypersonic Shock waves |
| Numerical and Experimental Study on the Duration of Nozzle Starting of the Reflected High-Enthalpy Shock Tunnel 期刊论文
APPLIED SCIENCES-BASEL, 2022, 卷号: 12, 期号: 6, 页码: 16
作者: Yu JP(于江鹏); Li JP(李进平); Wang Q(汪球); Zhang XY(张晓源); Zhang SZ(张仕忠)
Adobe PDF(6583Kb) | 收藏 | 浏览/下载：309/145 | 提交时间：2022/05/17
nozzle starting high-enthalpy shock tunnel center startup complete startup |
| 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：275/52 | 提交时间：2021/05/17
Concept demonstration Hypersonic propulsion Oblique detonation engine Scramjet Shock wave Supersonic combustion Wind tunnel test |
| 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：232/63 | 提交时间：2020/11/30
Shock tunnel High enthalpy Aerodynamic force measurement Strain gauge balance |
| Numerical modeling of a high-enthalpy shock tunnel driven by gaseous detonation 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 104, 页码: 8
作者: Luo K(罗凯); Wang Q(汪球); Li JW(栗继伟); Li JP(李进平); Zhao W(赵伟)
Adobe PDF(2023Kb) | 收藏 | 浏览/下载：298/94 | 提交时间：2020/11/30
Quasi-one-dimensional Detonation Shock tunnel Shock speed |
| A Fast-Response Calorimeter with Dynamic Corrections for Transient Heat Transfer Measurements 期刊论文
APPLIED SCIENCES-BASEL, 2020, 卷号: 10, 期号: 17, 页码: 22
作者: Zhang SZ(张仕忠); Wang Q(汪球); Li JP(李进平); Zhang XY(张晓源); Chen H(陈宏)
Adobe PDF(8566Kb) | 收藏 | 浏览/下载：172/41 | 提交时间：2020/11/30
calorimeter shock tunnel heat transfer measurement hypersonic |
| 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：244/100 | 提交时间：2020/11/30
hypervelocity shock tunnel detonation driver flight condition tailored condition test facilities |
| Investigation of dual ignition for a detonation-driven shock tunnel in forward driving mode 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2020, 卷号: 33, 期号: 5, 页码: 1468-1475
作者: Wang Q(汪球); Luo K(罗凯); Li JW(栗继伟); Li JP(李进平); Zhao W(赵伟)
Adobe PDF(2057Kb) | 收藏 | 浏览/下载：247/77 | 提交时间：2020/08/26
Shock tunnel Detonation driver Diaphragm Dual ignition High-enthalpy flow |
