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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:30/0  |  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:45/0  |  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:76/15  |  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:315/146  |  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:278/54  |  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:237/66  |  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:305/98  |  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:173/41  |  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:250/101  |  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:252/78  |  提交时间:2020/08/26 Shock tunnel Detonation driver Diaphragm Dual ignition High-enthalpy flow |