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Knowledge Management System of Institue of Mechanics, CAS
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State Key ... [7]
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崔凯 [7]
杨国伟 [7]
王秀平 [7]
胡守超 [7]
高太元 [7]
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Creator:王秀平
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Creator:高太元
Community:高温气体动力学国家重点实验室
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三维后体/尾喷管一体化构型优化设计及性能分析
期刊论文
科学通报, 2012, 卷号: 57, 期号: 4, 页码: 239-247
Authors:
高太元
;
崔凯
;
王秀平
;
胡守超
;
杨国伟
;
任亮
Adobe PDF(2922Kb)
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Submit date:2013/01/16
高超声速
后体/尾喷管一体化
单壁扩张喷管
优化设计
计算流体动力学
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
  |  
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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
Leading edge aerothermal inverse design of hyersonic vehicle based on homotopy optimization method
会议论文
6th International Conference on Fluid Mechanics, Guangzhou, PEOPLES R CHINA, JUN 30-JUL 03, 2011
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)
;
Cui, K (reprint author), Chinese Acad Sci, Inst Mech, LHD, Beijing 100190, Peoples R China.
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Submit date:2013/02/26
Hypersonic
Blunt Leading Edge
Aerothermodynamic
Inverse Design
Homotopy
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
Authors:
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)
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Submit date: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
Authors:
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)
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Submit date:2013/02/26
Hypersonic
Shape Optimization
Sequential Quadratic Programming (Sqp)
基于CFD分析的高超声速飞行器上表面优化
会议论文
LHD2011夏季学术研讨会, 内蒙赤峰, 2011
Authors:
高太元
;
崔凯
;
胡守超
;
王秀平
;
杨国伟
Adobe PDF(609Kb)
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Submit date:2014/01/23
高超声速
B-样条参数化
Sqp
Cfd
双发动机高超声速乘波飞行器性能分析
会议论文
LHD2011夏季学术研讨会, 内蒙赤峰, 2011
Authors:
崔凯
;
高太元
;
胡守超
;
王秀平
;
杨国伟
Adobe PDF(873Kb)
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Submit date:2014/01/23
高超声速
乘波体
升阻比
计算流体力学