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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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崔凯 [17]
李广利 [8]
胡守超 [7]
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Numerical study on aerodynamic performance of waverider with a new bluntness method
期刊论文
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2021, 卷号: 235, 期号: 10, 页码: 1225-1233
Authors:
Qu ZP
;
Xiao HD
;
Lv MY
;
Li GL(李广利)
;
Cui K(崔凯)
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Submit date:2021/06/11
bluntness method
computational fluid dynamics
hypersonic
volume
Waverider
Experimental investigation of a hypersonic I-shaped configuration with a waverider compression surface
期刊论文
SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY, 2020, 卷号: 63, 期号: 5, 页码: 3
Authors:
Li GL(李广利)
;
Cui K(崔凯)
;
Xu YZ(徐应洲)
;
Wang HX(王浩祥)
;
Yang J(杨靖)
;
Xu XG(许先贵)
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Submit date:2020/05/18
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
乘波体压缩面变化对其气动性能影响分析
期刊论文
力学学报, 2017, 卷号: 49, 期号: 01, 页码: 75-83
Authors:
崔凯
;
徐应洲
;
肖尧
;
李广利
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Submit date:2017/12/22
乘波体
优化设计
增量参数化方法
微分演化算法
计算流体力学
Effects of Shock Impingement on Aerothermal and Aerodynamic Performance for High-pressure Capturing Wings
会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:
Li GL(李广利)
;
Cui K(崔凯)
;
Xiao Y(肖尧)
;
Xu YZ(徐应洲)
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View/Download:368/85
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Submit date:2018/01/16
Aerodynamics
Angle Of Attack
Angle Of Attack Indicators
Boundary Layers
Drag
Drag Coefficient
High Pressure Effects
Hypersonic Aerodynamics
Hypersonic Flow
Spacecraft
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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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)
高速飞行器高压捕获翼气动布局概念研究
期刊论文
中国科学. 物理学, 力学, 天文学, 2013, 卷号: 43, 期号: 5, 页码: 652-661
Authors:
崔凯
;
李广利
;
胡守超
;
屈志朋
Adobe PDF(3076Kb)
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Submit date:2013/06/17
高速飞行器
气动布局
高压捕获翼
升力补偿
升阻比
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