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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... [1]
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崔凯 [11]
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Creator:崔凯
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Hypersonic I-shaped aerodynamic configurations
期刊论文
SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY, 2018, 卷号: 61, 期号: 2, 页码: 24722
Authors:
Cui K(崔凯)
;
Xiao Y(肖尧)
;
Xu YZ
;
Li GL
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Submit date:2018/10/30
High-Pressure Capturing Wing Configurations
期刊论文
AIAA JOURNAL, 2017, 卷号: 55, 期号: 6, 页码: 1909-1919
Authors:
Cui K(崔凯)
;
Li GL
;
Xiao Y(肖尧)
;
Xu YZ
;
Cui,K(reprint author), Chinese Acad Sci, Inst Mech
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Submit date:2017/07/24
Preliminary Study of Aerodynamic Performance for Waverider-based Hypersonic Vehicles with Dorsal Mounted Engines
会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:
Xiao Y(肖尧)
;
Cui K(崔凯)
;
Li GL(李广利)
;
Xu YZ(徐应洲)
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View/Download:303/99
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Submit date:2018/01/16
Aerodynamics
Air Engines
Aspect Ratio
Computational Fluid Dynamics
Drag
Engines
Hypersonic Aerodynamics
Lift
Lift Drag Ratio
Propulsion
Spacecraft
Vehicles
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
Conceptual design and aerodynamic evaluation of hypersonic airplane with double flanking air inlets
期刊论文
SCIENCE CHINA-TECHNOLOGICAL SCIENCES, 2013, 卷号: 56, 期号: 8, 页码: 1980-1988
Authors:
Cui K(崔凯)
;
Hu SC(胡守超)
;
Li GL(李广利)
;
Qu ZP(屈志朋)
;
Situ M
;
Cui, K (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
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Submit date:2013/09/27
Hypersonic
Flanking Air Inlet
Waverider
Computational Fluid Dynamics(Cfd)
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
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.
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Submit date:2013/02/26
China Railways High-speed (Crh)
Nose Shape
Computational Fluid Mechanics
Optimization
Shape Optimization for Hypersonic Arc-Wing Missiles
期刊论文
Journal of Spacecraft and Rockets, 2010, 卷号: 47, 期号: 4, 页码: 694-700
Authors:
Cui K(崔凯)
;
Yang GW(杨国伟)
Adobe PDF(4987Kb)
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Submit date:2010/09/07
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