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Knowledge Management System of Institue of Mechanics, CAS
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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)
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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)
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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)
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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)
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Submit date:2014/04/02
Vehicle
Leading
0algorithm
Genetic
Hypersonic
Optimization
Aerothermal
Based
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Around
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Evaluated
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About
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Differ