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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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State Key ... [6]
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崔凯 [5]
胡守超 [5]
李广利 [4]
司徒明 [3]
肖尧 [3]
Situ M [2]
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力学学报 [2]
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基于实验设计方法的高超声速飞机前缘型线优化分析
期刊论文
力学学报, 2016, 卷号: 48, 期号: 2, 页码: 290-299
Authors:
胡守超
;
崔凯
;
李广利
;
肖尧
;
司徒明
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Submit date:2016/12/16
Hypersonic Airplane
Air-breathing Vehicle
Shape Optimization
Parameterization
Uniform Design
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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View/Download:338/145
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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
高超声速飞机前缘型线优化分析
会议论文
第八届全国高超声速科技学术会议, 中国黑龙江哈尔滨, 2015-12-28
Authors:
胡守超
;
崔凯
;
李广利
;
肖尧
;
司徒明
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Adobe PDF(631Kb)
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View/Download:322/86
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Submit date:2016/08/16
高超声速飞机
型线
压心
参数化设计方法
升阻比
高压气流
巡航飞行
实验设计方法
耦合效应
吸气式
双旁侧进气高超声速飞机概念设计与评估
期刊论文
中国科学. 技术科学, 2013, 卷号: 43, 期号: 10, 页码: 1085-1093
Authors:
崔凯
;
胡守超
;
李广利
;
屈志朋
;
司徒明
Adobe PDF(1833Kb)
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Submit date:2013/12/04
高超声速
旁侧进气
乘波体
计算流体动力学(Cfd)
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.
Adobe PDF(1426Kb)
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Submit date:2013/09/27
Hypersonic
Flanking Air Inlet
Waverider
Computational Fluid Dynamics(Cfd)
酚醛树脂高温热解的激波管实验研究
期刊论文
力学学报, 2009, 卷号: 41, 期号: 4, 页码: 463-468
Authors:
闫卫锋
;
王苏
;
马伟
;
李帅辉
;
范秉诚
;
何宇中
;
崔季平
Adobe PDF(1114Kb)
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Submit date:2010/01/21
酚醛树脂
热解
再入过程
激波管
质谱分析
色谱分析