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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)
View  |  Adobe PDF(199Kb)  |  Favorite  |  View/Download:638/143  |  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