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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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力学所知识产出(19... [3]
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崔凯 [14]
杨国伟 [14]
胡守超 [7]
王秀平 [6]
高太元 [6]
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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
双旁侧进气高超声速飞机气动布局与评估
会议论文
LHD2012夏季学术研讨会, 吉林延吉, 2012
Authors:
胡守超
;
崔凯
;
李广利
;
屈志朋
;
杨国伟
Adobe PDF(1737Kb)
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Submit date:2014/01/23
高超声速
双旁侧进气
气动布局
计算流体动力学(Cfd)
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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Adobe PDF(199Kb)
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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.
Adobe PDF(53Kb)
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Submit date:2013/02/26
Hypersonic
Blunt Leading Edge
Aerothermodynamic
Inverse Design
Homotopy
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
全参数化高超声速乘波飞行器构型设计
会议论文
第二届高超声速科技学术会议, 中国安徽黄山, 2009-11-02
Authors:
崔凯
;
杨国伟
Adobe PDF(1115Kb)
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View/Download:717/186
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Submit date:2010/11/25
高超声速
一体化
参数化
乘波体
基于CFD分析的弧形翼导弹气动外形优化
期刊论文
中国科学. G辑, 物理学,力学,天文学, 2009, 卷号: 39, 期号: 6, 页码: 865-873
Authors:
崔凯
;
杨国伟
Adobe PDF(3468Kb)
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Submit date:2010/05/03
优化设计
导弹
弧形翼
计算流体力学
可变多面体搜索方法
Response Surface Technique for Static Aeroelastic Optimization on a High-Aspect-Ratio Wing
期刊论文
Journal of Aircraft, 2009, 卷号: 46, 期号: 4, 页码: 1444-1450
Authors:
Yang GW(杨国伟)
;
Chen DW(陈大伟)
;
Cui K(崔凯)
;
Yang GW
Adobe PDF(1016Kb)
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Submit date:2009/08/03
Navier-stokes Solver
Aircraft