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Multi-objective design optimization of the combinational configuration of the upstream energy deposition and opposing jet for drag reduction in supersonic flows 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 105, 页码: 10
Authors:  Ju SJ(鞠胜军);  Sun ZX(孙振旭);  Yang GW(杨国伟);  Prapamonthon P;  Zhang JY
Adobe PDF(3818Kb)  |  Favorite  |  View/Download：457/118  |  Submit date：2020/11/30
Optimization design  Drag reduction  Supersonic flow  Energy deposition  Opposing jet  
Separate and Combined Effects of Surface Roughness and Thermal Barrier Coating on Vane Cooling Performance 期刊论文
JOURNAL OF THERMAL SCIENCE AND ENGINEERING APPLICATIONS, 2020, 卷号: 12, 期号: 5, 页码: 15
Authors:  Prapamonthon P;  Yin B(银波);  Yang GW(杨国伟);  Zhang MH
Adobe PDF(2963Kb)  |  Favorite  |  View/Download：347/124  |  Submit date：2020/11/30
gas-turbine heat transfer  surface roughness  cooling performance  thermal barrier coating  
Fixed-Point Fluid structure interaction analysis BASED ON geometrically exact approach 期刊论文
SCIENTIFIC REPORTS, 2020, 卷号: 10, 期号: 1, 页码: 16
Authors:  Yu ML(余明亮);  Nie XY(聂雪媛);  Yang GW(杨国伟);  Zhong PN(钟培楠)
Adobe PDF(4371Kb)  |  Favorite  |  View/Download：311/102  |  Submit date：2020/08/26
Parametric study on drag reduction with the combination of the upstream energy deposition and the opposing jet configuration in supersonic flows 期刊论文
ACTA ASTRONAUTICA, 2020, 卷号: 171, 页码: 300-310
Authors:  Ju SJ;  Sun ZX(孙振旭);  Yang GW(杨国伟);  Prapamonthon P;  Zhang JY
Adobe PDF(3216Kb)  |  Favorite  |  View/Download：363/97  |  Submit date：2020/05/18
Computational fluid dynamics  Drag reduction  Supersonic flow  Energy deposition  Opposing jet  
Understanding of temperature and cooling effectiveness sensitivity of a film-cooled vane under coolant inlet temperature effect: A case study 期刊论文
CASE STUDIES IN THERMAL ENGINEERING, 2019, 卷号: 14, 页码: UNSP 100505
Authors:  Prapamonthon P;  Yin B(银波);  Yang GW(杨国伟);  Zhang MH
View  |  Adobe PDF(3342Kb)  |  Favorite  |  View/Download：268/82  |  Submit date：2020/03/21
TURBINE BLADE  HEAT-TRANSFER  
Numerical prediction of cooling performance sensitivity of 1st stage nozzle guide vane under aerothermal conditions 会议论文
ASME 2019 Gas Turbine India Conference, GTINDIA 2019, Chennai, Tamil Nadu, India, December 5, 2019 - December 6, 2019
Authors:  Prapamonthon P;  Yin B(银波);  Yang GW(杨国伟);  Zhang MH(张莫晗)
Adobe PDF(2782Kb)  |  Favorite  |  View/Download：206/74  |  Submit date：2020/11/20
Aerothermal condition  Cooling effectiveness  Cooling performance  Thermal sensitivity  Turbine vane