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Numerical investigation of mode transition and hysteresis in a cavity-based dual-mode scramjet combustor 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 94, 页码: 10
Authors:  Zhang X(张旭);  Yue LJ(岳连捷);  Huang TL(黄庭隆);  Zhang QF(张启帆);  Zhang XY(张新宇)
View  |  Adobe PDF(3862Kb)  |  Favorite  |  View/Download:366/129  |  Submit date:2020/03/21
Hysteresis  Dual-mode scramjet  Supersonic combustion  Mode transition  Flame stabilization  Combustion oscillation  
Construction of bi-layer biluminophore fast-responding pressure sensitive coating for non-contact unsteady aerodynamic testing 期刊论文
POLYMER TESTING, 2019, 卷号: 77, 页码: 8
Authors:  Yang D;  Ren JK;  Li JW(栗继伟);  Wang QL;  Wang Q(汪球);  Xie Z;  Qu XZ
View  |  Adobe PDF(2608Kb)  |  Favorite  |  View/Download:1051/800  |  Submit date:2019/11/25
Pressure sensitive paint (PSP)  Bi-layer structured coating  Fast-response  Self-referenced measurement  
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:445/104  |  Submit date:2019/05/29
Heat transfer measurement  Lateral heat conduction  Shock tunnel  Thermocouple  Hypersonic  
Numerical study on the aerothermodynamics of different heatshield configurations for Mars entry capsules 期刊论文
ACTA ASTRONAUTICA, 2019, 卷号: 157, 页码: 189-198
Authors:  Zhong K;  Yan C;  Chen SS;  Wang XY(王小永);  Ju SJ
View  |  Adobe PDF(8635Kb)  |  Favorite  |  View/Download:252/74  |  Submit date:2019/05/29
Aeroheating  Heatshield configuration  Sphere-cone angle  Mars  Turbulent  
Experimental study of flame characteristics of ethylene and its mixture with methane and hydrogen in supersonic combustor 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 86, 页码: 775-781
Authors:  Zhong FQ(仲峰泉);  Cheng LW(程柳维);  Gu HB(顾洪斌);  Zhang XY(张新宇)
Adobe PDF(2032Kb)  |  Favorite  |  View/Download:328/102  |  Submit date:2019/05/29
Supersonic combustor  Hydrocarbon  Mixture fuel  Flame structure  Ignition