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On the limitations of hybrid particle-in-cell for ion thruster plume simulations 期刊论文
PHYSICS OF PLASMAS, 2019, 卷号: 26, 期号: 10, 页码: 8
Authors:  Wang J;  Hu Y(胡远)
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Wall Heat Flux Measurements for a Kerosene-Fueled Supersonic Combustor 期刊论文
JOURNAL OF AEROSPACE ENGINEERING, 2019, 卷号: 32, 期号: 5, 页码: 11
Authors:  Cheng D(程迪);  Wang J(王晶);  Lu Y(陆阳);  Li L(李龙);  Yao W(姚卫);  Fan XJ(范学军)
View  |  Adobe PDF(2651Kb)  |  Favorite  |  View/Download:445/146  |  Submit date:2019/09/09
Heat flux measurement  Kerosene  Supersonic combustion  Scramjet  Heat flux sensor  
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
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Aeroheating  Heatshield configuration  Sphere-cone angle  Mars  Turbulent  
Spectral Radiant Intensity Calculation of Air in Shock Tube 会议论文
31st International Symposium on Shock Waves, Nagoya, Japan, 2017-07-9~14
Authors:  Lyu, Jun Ming;  Cheng, X. L.;  Yu, J. J.;  Li F(李飞);  Yu XL(余西龙)
Adobe PDF(791Kb)  |  Favorite  |  View/Download:98/31  |  Submit date:2023/03/17
Influences of Domain Symmetry on Supersonic Combustion Modeling 期刊论文
JOURNAL OF PROPULSION AND POWER, 2019, 卷号: 35, 期号: 2, 页码: 451-465
Authors:  Yao W(姚卫);  Wu K(吴坤);  Fan XJ(范学军)
Adobe PDF(862Kb)  |  Favorite  |  View/Download:363/108  |  Submit date:2019/04/11