中文版 | English

在结果中检索

IMECH-IR
（本次检索基于用户作品认领结果）

浏览/检索结果: 共4条，第1-4条 帮助

限定条件            
已选(0)清除 条数/页：   排序方式：
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
作者:  Cui K(崔凯);  Hu SC(胡守超);  Gao TY(高太元);  Wang XP(王秀平);  Yang GW(杨国伟)
浏览  |  Adobe PDF(199Kb)  |  收藏  |  浏览/下载：473/73  |  提交时间：2014/04/02
Vehicle  Leading  0algorithm  Genetic  Hypersonic  Optimization  Aerothermal  Based  Method  Design  Attack  Novel  Around  Angle  Evaluated  Greatly  About  Fluid  Result  Differ  
Aerodynamic optimization and evaluation for the three-dimensional afterbody/nozzle integrated configuration of hypersonic vehicles 期刊论文
Chinese Science Bulletin, 2012, 卷号: 57, 期号: 8, 页码: 849-857
作者:  Gao TY(高太元);  Cui K(崔凯);  Wang XP(王秀平);  Hu SC(胡守超);  Yang GW(杨国伟);  Ren L;  kcui@imech.ac.cn
Adobe PDF(985Kb)  |  收藏  |  浏览/下载：1130/308  |  提交时间：2012/09/26
Hypersonic Afterbody/Nozzle Integrated Configuration Single Expanding Ramp Nozzle Optimization Computational Fluid Dynamics  
Primary study of aerodynamic performance evaluation and optimization of the high-speed train 会议论文
6th International Conference on Fluid Mechanics, Guangzhou, PEOPLES R CHINA, JUN 30-JUL 03, 2011
作者:  Wang XP(王秀平);  Cui K(崔凯);  Hu SC(胡守超);  Gao TY(高太元);  Yang GW(杨国伟);  Wang, XP (reprint author), Chinese Acad Sci, Inst Mech, LHD, Beijing 100190, Peoples R China.
Adobe PDF(349Kb)  |  收藏  |  浏览/下载：608/142  |  提交时间：2013/02/26
China Railways High-speed (Crh)  Nose Shape  Computational Fluid Mechanics  Optimization  
Optimization of the upper surface of hypersonic vehicle based on CFD analysis 会议论文
6th International Conference on Fluid Mechanics, Guangzhou, PEOPLES R CHINA, JUN 30-JUL 03, 2011
作者:  Gao TY(高太元);  Cui K(崔凯);  Hu SC(胡守超);  Wang XP(王秀平);  Yang GW(杨国伟);  Gao, TY (reprint author), Chinese Acad Sci, Inst Mech, Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
Adobe PDF(305Kb)  |  收藏  |  浏览/下载：721/196  |  提交时间：2013/02/26
Hypersonic  Shape Optimization  Sequential Quadratic Programming (Sqp)