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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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Numerical simulation of 30p30n multi-element airfoil using delayed detached-eddy simulation
会议论文
AIAA AVIATION 2020 FORUM, 15 June 2020 through 19 June 2020
作者:
Jin Y
;
廖飞, Cai JS
Adobe PDF(4611Kb)
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浏览/下载:196/104
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提交时间:2021/06/11
Large eddy simulation of rest hypersonic combustor based on dynamic zone flamelet model
会议论文
AIAA Propulsion and Energy 2020 Forum, 24 August 2020 through 28 August 2020
作者:
Yao W(姚卫)
;
Chen L(陈留)
Adobe PDF(2272Kb)
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浏览/下载:260/144
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提交时间:2021/06/11
Investigation of high-order cell-centered finite difference method for aeroacoustics
会议论文
25th AIAA/CEAS Aeroacoustics Conference, 2019, Delft, Netherlands, May 20, 2019 - May 23, 2019
作者:
Jin Y
;
Liao F(廖飞)
;
Cai JS
;
Morris PJ
Adobe PDF(2986Kb)
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浏览/下载:209/74
  |  
提交时间:2020/11/20
Tunable Dirac cones in two-dimensional acoustic metamaterials with Matryoshka structure
会议论文
26th International Congress on Sound and Vibration, ICSV 2019, Montreal, QC, Canada, July 7, 2019 - July 11, 2019
作者:
Chen M(陈猛)
;
Jiang H(姜恒)
;
Wang YR(王育人)
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Adobe PDF(1630Kb)
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浏览/下载:246/80
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提交时间:2019/11/20
Acoustic metamaterials
Acoustic structures
Dirac cones
Dispersion curves
Edge state
Honeycomb lattices
Topological phase
Topological transitions
Application of dynamic zone flamelet model to a GH2/GO2 rocket combustor
会议论文
AIAA Propulsion and Energy Forum and Exposition, 2019, Indianapolis, IN, United states, August 19, 2019 - August 22, 2019
作者:
Yao W(姚卫)
;
Li B(李波)
Adobe PDF(1665Kb)
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浏览/下载:140/43
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提交时间:2020/11/20
Dynamic zone flamelet model
GH2/GO2
Large Eddy Simulation (LES)
Rocket combustor
Turbulence-chemistry interaction
Inertial migrations of cylindrical particles in rectangular microchannels: Variations of equilibrium positions and equivalent diameters
会议论文
8th Meeting of the Hellenic-Society-of-Rheology, Limassol, CYPRUS, JUL 12-14, 2017
作者:
Su JH
;
Chen XD(陈晓东)
;
Hu GQ(胡国庆)
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Adobe PDF(6321Kb)
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浏览/下载:261/108
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提交时间:2018/06/06
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
作者:
Lee YC(李亚超)
;
Yao W(姚卫)
;
Fan XJ(范学军)
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Adobe PDF(1377Kb)
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浏览/下载:277/112
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提交时间:2020/08/26
Low-dissipation compressible Solver, Skew-symmetric Form, Benchmark Flow Problems
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
作者:
Lee YC
;
Yao W(姚卫)
;
Fan XJ(范学军)
;
Yao, Wei(weiyao@imech.ac.cn)
浏览
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Adobe PDF(1358Kb)
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浏览/下载:422/107
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提交时间: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
Development of zone flamelet model for scramjet combustor modeling
会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
作者:
Yao W(姚卫)
;
Fan XJ(范学军)
浏览
  |  
Adobe PDF(623Kb)
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  |  
浏览/下载:258/87
  |  
提交时间:2018/01/16
Combustion
Cost Benefit Analysis
Costs
Mixtures
Spacecraft
Supersonic Aircraft
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
作者:
Lee YC
;
Yao W(姚卫)
;
Fan XJ(范学军)
浏览
  |  
Adobe PDF(1377Kb)
  |  
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  |  
浏览/下载:480/91
  |  
提交时间: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