Chinese | English

Search in the results

IMECH-IR

Browse/Search Results:  1-4 of 4 Help

Selected(0)Clear Items/Page:    Sort:
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：238/83  |  Submit date：2020/11/20
Aerothermal condition  Cooling effectiveness  Cooling performance  Thermal sensitivity  Turbine vane  
Aerodynamic and Aerothermal Performance of Power-law Shaped Leading Edge of Hypersonic Waveriders 期刊论文
Procedia Engineering, 2013, 卷号: 67, 页码: 207-217
Authors:  Wang FM(王发民);  Han HQ(韩汉桥);  Lei MF(雷麦芳);  Zhang J(张杰)
View  |  Adobe PDF(3673Kb)  |  Favorite  |  View/Download：357/80  |  Submit date：2015/09/24
Aerothermal Protection  Power-law Leading Edge  Aerodynamic Performance  
Aerodynamic and Aerothermal Performance of Power-law Shaped Leading Edge of Hypersonic Waveriders 会议论文
7th Asian-Pacific Conference on Aerospace Technology and Science, 7th APCATS 2013, Taiwan, China, MAY 23-26, 2013
Authors:  Wang FM(王发民);  Han HQ(韩汉桥);  Lei MF(雷麦芳);  Zhang J(张杰);  Wang FM(王发民)
View  |  Adobe PDF(3663Kb)  |  Favorite  |  View/Download：592/149  |  Submit date：2014/03/11
Hypersonic  Aerothermal Protection  Power-law Leading Edge  Aerodynamic Performance  
Aerothermal optimization of hypersonic vehicle leading edge based on genetic algorithm 会议论文
23rd International Congress of Theoretical and Applied Mechanics, 中国北京/Beijing, China, 2012-08-19
Authors:  Cui K(崔凯);  Hu SC(胡守超);  Gao TY(高太元);  Wang XP(王秀平);  Yang GW(杨国伟)
View  |  Adobe PDF(199Kb)  |  Favorite  |  View/Download：612/129  |  Submit date：2014/04/02
Vehicle  Leading  0algorithm  Genetic  Hypersonic  Optimization  Aerothermal  Based  Method  Design  Attack  Novel  Around  Angle  Evaluated  Greatly  About  Fluid  Result  Differ