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Optical diagnostics in a detonation-driven direct-connected circular combustor fueled with hydrogen for mach 10 scramjet 期刊论文
INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2021, 卷号: 46, 期号: 54, 页码: 27801-27815
Authors:  Zhou GX(周功喜);  Zhang X(张旭);  Li JP(李进平);  Zhang XY(张晓源);  Zhang SZ(张仕忠);  Lin X(林鑫);  Li F(李飞);  Chen H(陈宏);  Yue LJ(岳连捷);  Yu XL(余西龙)
Adobe PDF(4108Kb)  |  Favorite  |  View/Download:342/52  |  Submit date:2021/09/07
High mach number scramjet  Circular cross-section  TDLAS  Multi-view simultaneous imaging  POD  
Evolution of heat transfer at the stagnation point during the detached bow shock establishment 期刊论文
SHOCK WAVES, 2021, 页码: 8
Authors:  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)  |  Favorite  |  View/Download:268/59  |  Submit date:2021/05/17
Hypersonic  Aerodynamic heating  Detached bow shock  Shock tube  expansion tube  
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
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:334/105  |  Submit date: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
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:199/49  |  Submit date: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
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:269/101  |  Submit date:2020/11/30
hypervelocity  shock tunnel  detonation driver  flight condition  tailored condition  test facilities  
Influence of test model material on the accuracy of transient heat transfer measurements in impulse facilities 期刊论文
EXPERIMENTAL THERMAL AND FLUID SCIENCE, 2019, 卷号: 104, 页码: 59-66
Authors:  Wang Q(汪球);  Olivier H;  Einhoff J;  Li JP(李进平);  Zhao W(赵伟)
View  |  Adobe PDF(1085Kb)  |  Favorite  |  View/Download:432/102  |  Submit date:2019/05/29
Heat transfer measurement  Lateral heat conduction  Shock tunnel  Thermocouple  Hypersonic