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中国科学院力学研究所机构知识库
Knowledge Management System of Institue of Mechanics, CAS
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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
Method
Design
Attack
Novel
Around
Angle
Evaluated
Greatly
About
Fluid
Result
Differ