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Hypersonic flow and heat transfer of a micro-rough plate in the near-continuum regime 期刊论文
PHYSICS OF FLUIDS, 2023, 卷号: 35, 期号: 10, 页码: 21
Authors:  Guo, Jinghui;  Wang XY(王小永);  Li, Sijia;  Lin, Guiping
Favorite  |  View/Download：19/0  |  Submit date：2024/04/15
Development of a stagnation streamline model for thermochemical nonequilibrium flow 期刊论文
PHYSICS OF FLUIDS, 2020, 卷号: 32, 期号: 4, 页码: 046102
Authors:  Hong QZ(洪启臻);  Wang XY(王小永);  Hu Y(胡远);  Sun QH(孙泉华)
View  |  Adobe PDF(2694Kb)  |  Favorite  |  View/Download：445/123  |  Submit date：2020/04/21
Hypersonic  
Numerical study of convective heat transfer of a supersonic combustor with varied inlet flow conditions 期刊论文
ACTA MECHANICA SINICA, 2019, 卷号: 35, 期号: 5, 页码: 943-953
Authors:  Fan WH(范文慧);  Zhong FQ(仲峰泉);  Ma SG(马素刚);  Zhang XY(张新宇)
View  |  Adobe PDF(4075Kb)  |  Favorite  |  View/Download：309/91  |  Submit date：2020/03/11
Wall heat flux  Numerical simulation  Ethylene  Supersonic combustor  
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：232/73  |  Submit date：2019/05/29
Aeroheating  Heatshield configuration  Sphere-cone angle  Mars  Turbulent