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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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Indexed By:EI
Language:英语
Document Type:会议论文
Community:高温气体动力学国家重点实验室
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The influence of detonation interval on the dynamic response of underground fortification
会议论文
2nd International Conference on Applied Mechanics and Advanced Materials (ICAMAM 2023), Changsha, China, 06/01/2023 - 08/01/2023
Authors:
Yuan,Jianfei
;
Feng C(冯春)
;
Lin,Qindong
;
Jiao,Wenjun
;
Gan,Yundan
Adobe PDF(841Kb)
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Submit date:2023/07/17
A low-dissipation solver based on OpenFOAM designed for large eddy simulation in compressible flows
会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:
Lee YC(李亚超)
;
Yao W(姚卫)
;
Fan XJ(范学军)
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Submit date:2020/08/26
Low-dissipation compressible Solver, Skew-symmetric Form, Benchmark Flow Problems
A comparative study of elliptical and round scramjet combustors by Improved Delayed Detached Eddy Simulation
会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:
Yao W(姚卫)
;
Yuan YM(袁越明)
;
Li XP(李晓鹏)
;
Wang J(王晶)
;
Fan XJ(范学军)
;
Fan, Xuejun(xfan@imech.ac.cn)
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Submit date:2018/01/16
Adiabatic Flame Temperature
Aerodynamics
Boundary Layer Flow
Boundary Layers
Chemical Analysis
Combustion
Computational Chemistry
Directed Graphs
Flow Separation
Mach Number
Principal Component Analysis
Regression Analysis
Sensitivity Analysis
Spacecraft
Supersonic Aerodynamics
Supersonic Aircraft
Transients
A low-dissipation scheme based on OpenFoam designed for large eddy simulation in compressible flow
会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:
Lee YC
;
Yao W(姚卫)
;
Fan XJ(范学军)
;
Yao, Wei(weiyao@imech.ac.cn)
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Adobe PDF(1358Kb)
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View/Download:448/115
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Submit date:2018/01/16
Computational Fluid Dynamics
Computer Software
Digital Storage
Kinetic Energy
Kinetics
Open Source Software
Open Systems
Runge Kutta Methods
Shock Tubes
Shock Waves
Spacecraft
Turbulence
Two Phase Flow
A low-dissipation solver based on openFOAM designed for large eddy simulation in compressible flow
会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Hypersonics 2017, Xiamen, China, March 6, 2017 - March 9, 2017
Authors:
Lee YC
;
Yao W(姚卫)
;
Fan XJ(范学军)
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Adobe PDF(1377Kb)
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Submit date:2018/11/08
Computational Fluid Dynamics
Digital Storage
Kinetic Energy
Kinetics
Open Source Software
Open Systems
Ramjet Engines
Runge Kutta Methods
Shock Tubes
Turbulence
Two Phase Flow
Bench
Mark Problems
Central
Upwind Scheme
Computational Fluid Dynamics Software
Skew
Symmetric Forms
Temporal Discretization
Turbulence Structures
Unstructured Meshes
Wall Bounded Turbulence
Direct numerical simulation of supersonic turbulent boundary layer subjected to a curved compression ramp
会议论文
Meeting of the Institute-of-Non-Newtonian-Fluid-Mechanics (INNFM), Llanwddyn, WALES, 2017
Authors:
Tong FL(童福林)
;
Li XL(李新亮)
;
Duan, Yanhui
;
Yu ZP(于长平)
;
Yu, CP (reprint author), Chinese Acad Sci, Inst Mech, LHD, Beijing 100190, Peoples R China.
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View/Download:323/127
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Submit date:2018/01/16
Concave Surface Curvature
Adverse Pressure-gradient
Large-eddy Simulation
Reynolds-number
Near-wall
Flows
Separation
Vortices
Models
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)
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Adobe PDF(461Kb)
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View/Download:334/91
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Submit date:2018/01/16
Aerodynamic Configurations
Aerodynamics
Computational Fluid Dynamics
Deformation
Evolutionary Algorithms
Fluid Dynamics
Hypersonic Aerodynamics
Optimization
Spacecraft
Coupling Analysis for the Thermo-Acoustic-Vibration Response of a Thin-Walled Box
会议论文
10th International Conference on Vibration Engineering and Technology of Machinery, Manchester ENGLAND, SEP 09-11 2014
Authors:
Yang Y(杨焱)
;
Wu CW(吴臣武)
;
yangyan@imech.ac.cn
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Submit date:2015/09/29
Thermal
Vibration
Acoustic
Multi-physics Environment
Numerical analyses of discrete gust response for a flexible aircraft
会议论文
21st AIAA Applied Aerodynamics Conference 2003, Orlando, FL, United states, June 23, 2003 - June 26, 2003
Authors:
Yang GW(杨国伟)
;
Obayashi S
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View/Download:199/86
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Submit date:2017/06/01
Direct-coupling Method
Dynamic Equations Of Motion
Flexible Aircraft
Flexible Airplane
Freedom Of Motion
One-minus-cosine Gust
Quasi-steady Model
Supersonic Transport