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On the determination of the standing oblique detonation wave in an engine combustor using laser absorption spectroscopy of hydroxyl radical 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2024, 卷号: 152, 页码: 11./通讯作者：Liu, Yunfeng
Authors:  Zhang WS(张文硕);  Zhang, Zijian;  Han X(韩信);  Yuan CK(苑朝凯);  Liu YF(刘云峰);  Ma, Liuhao;  Ren, Wei
Favorite  |  View/Download：65/0  |  Submit date：2024/08/19
Standing oblique detonation ramjet  OH radical  Laser absorption spectroscopy  Shock tunnel  Freejet experiment  
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./通讯作者：Yao, Wei
Authors:  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)
Favorite  |  View/Download：88/0  |  Submit date：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./通讯作者：Wang, Qiu
Authors:  Wang WT(王文韬);  Wang Q(汪球);  Li JP(李进平);  Zhao W(赵伟);  Gao, Liangjie;  Liu, Zhongchen;  Qian, Zhansen
Adobe PDF(2024Kb)  |  Favorite  |  View/Download：140/3  |  Submit date：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./通讯作者：汪运鹏
Authors:  Wang Y(王粤);  Wang YP(汪运鹏);  Jiang ZL(姜宗林)
Adobe PDF(7258Kb)  |  Favorite  |  View/Download：187/44  |  Submit date：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./通讯作者：Li, Jinping
Authors:  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)  |  Favorite  |  View/Download：432/165  |  Submit date：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./通讯作者：Jiang, Zonglin
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)
Adobe PDF(1806Kb)  |  Favorite  |  View/Download：336/77  |  Submit date：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./通讯作者：Wang, Y.
Authors:  Wang YP(汪运鹏);  Jiang ZL(姜宗林)
Adobe PDF(1551Kb)  |  Favorite  |  View/Download：326/92  |  Submit date：2020/11/30
Shock tunnel  High enthalpy  Aerodynamic force measurement  Strain gauge balance  
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./通讯作者：Wang, Qiu, Zhang, Xiaoyuan
Authors:  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)  |  Favorite  |  View/Download：293/81  |  Submit date：2020/11/30
calorimeter  shock tunnel  heat transfer measurement  hypersonic  
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./通讯作者：Wang, Qiu, Li, Jinping
Authors:  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)  |  Favorite  |  View/Download：434/121  |  Submit date：2020/11/30
Quasi-one-dimensional  Detonation  Shock tunnel  Shock speed  
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./通讯作者：Jiang, Zonglin
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：341/105  |  Submit date：2020/11/30
hypervelocity  shock tunnel  detonation driver  flight condition  tailored condition  test facilities