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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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Simulation on Three-Dimensional Shock Interactions and Aerodynamic Heating Between Body and Wing
期刊论文
AIAA JOURNAL, 2021, 页码: 12
Authors:
Lin MY(林明月)
;
Wang C(王春)
;
Peng J(彭俊)
;
Jiang ZL(姜宗林)
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Submit date:2022/01/12
An sequential optimization and aeroelastic constraint transformation method for strength-aeroelastic comprehensive design
期刊论文
JOURNAL OF FLUIDS AND STRUCTURES, 2020, 卷号: 93, 页码: 14
Authors:
Zhang ZS
;
Wang XJ
;
Chen XJ(陈贤佳)
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Submit date:2020/04/07
Comprehensive design
Sequential optimization strategy
Airplane wing
Structural strength
Aeroelasticity
Characterizing three-dimensional features of vortex surfaces in the flow past a finite plate
期刊论文
PHYSICS OF FLUIDS, 2020, 卷号: 32, 期号: 1, 页码: 15
Authors:
Tong WW
;
Yang Y(杨越)
;
Wang SZ(王士召)
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Submit date:2020/05/18
Six sigma robust design optimization for thermal protection system of hypersonic vehicles based on successive response surface method
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2019, 卷号: 32, 期号: 9, 页码: 2095-2108
Authors:
Zhu JJ
;
Wang XJ
;
Zhang HG
;
Li YW
;
Wang RX(王睿星)
;
Qiu ZP
Adobe PDF(2082Kb)
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Submit date:2020/03/21
Hypersonic vehicle
Six sigma robust optimization
Successive response surface
Thermal protection system
Uncertainty
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
Theories and technologies for duplicating hypersonic flight conditions for ground testing
期刊论文
NATIONAL SCIENCE REVIEW, 2017, 卷号: 4, 期号: 3, 页码: 290-U461
Authors:
Jiang ZL(姜宗林)
;
Yu HR(俞鸿儒)
;
Jiang, ZL (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing, Peoples R China.
;
Jiang, ZL (reprint author), Univ Chinese Acad Sci, Sch Engn Sci, Beijing, Peoples R China.
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Submit date:2017/11/29
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)
Adobe PDF(639Kb)
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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
Study on Compression Surface Deformation of Waveriders
会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:
Xu YZ(徐应洲)
;
Cui K(崔凯)
;
Li GL(李广利)
;
Xiao Y(肖尧)
Adobe PDF(461Kb)
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Submit date:2018/01/16
Aerodynamic Configurations
Aerodynamics
Computational Fluid Dynamics
Deformation
Evolutionary Algorithms
Fluid Dynamics
Hypersonic Aerodynamics
Optimization
Spacecraft
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
Adobe PDF(872Kb)
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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
Flow characteristics of hypersonic inlets with different cowl-lip blunting methods
期刊论文
SCIENCE CHINA-Physics, Mechanics & Astronomy, 2014, 卷号: 57, 期号: 4, 页码: 741-752
Authors:
Lu HB(卢洪波)
;
Yue LJ(岳连捷)
;
Zhang XY(张新宇)
;
Yue LJ(岳连捷)
Adobe PDF(1133Kb)
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Submit date:2014/04/15
Hypersonic Inlet
Cowl-lip Bluntness
Flow Characteristics
Shock Pattern
Shock Interference