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崔凯 [9]
胡守超 [9]
杨国伟 [6]
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Creator:hushouchao分胡守超
Document Type:会议论文
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A conceptual design of next generation hypersonic air-breathing airplanes with dual waveriders forebody
会议论文
20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 2015, Glasgow, United kingdom, July 6, 2015 - July 9, 2015
Authors:
Cui K(崔凯)
;
Hu SC(胡守超)
;
Li GL
;
Xiao Y(肖尧)
;
Situ M
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Submit date:2017/05/05
Aero
Dynamic Performance
Aerodynamic Performance Predictions
Design Methodology
Flight Altitudes
Numerical Results
Propulsion System
Turbulent Models
Wing Body Aircraft
Shape design to minimize the peak heat-flux of blunt leading-edge
会议论文
51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition 2013, Grapevine, TX, United states, JAN 07-10, 2013
Authors:
Cui K(崔凯)
;
Hu SC(胡守超)
;
Cui K(崔凯)
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Submit date:2014/02/24
高压捕获翼气动布局研究
会议论文
中国力学大会——2013, 中国北京, 2013-08-19
Authors:
崔凯
;
李广利
;
胡守超
;
屈志朋
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Submit date:2014/04/02
气动布局
高压
支撑机构
飞行器
乘波体
升阻比
三角翼
高升力
湍流
设计需求
阻性
计算结果
大容积
外形
进一步:0
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)
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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.
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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.
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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