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高温气体动力学国家... [12]
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浏览/检索结果:
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专题:高温气体动力学国家重点实验室
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An improved stiff-ODE solving framework for reacting flow simulations with detailed chemistry in OpenFOAM
期刊论文
COMBUSTION THEORY AND MODELLING, 2023, 卷号: 27, 期号: 1, 页码: 57-82
作者:
Wu K(吴坤)
;
Jiang YT(蒋雨廷)
;
Huo ZJ(霍志杰)
;
Cheng D(程迪)
;
Fan XJ(范学军)
Adobe PDF(3242Kb)
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浏览/下载:126/10
  |  
提交时间:2023/02/03
reacting flow simulation
detailed chemistry
stiff ODE
Jacobian
linear system solver
Atomization of misaligned impinging liquid jets
期刊论文
PHYSICS OF FLUIDS, 2021, 卷号: 33, 期号: 9, 页码: 15
作者:
Zhang, Chenwei
;
Zhang ZY(张振宇)
;
Wu K(吴坤)
;
Xia, Xi
;
Fan XJ(范学军)
Adobe PDF(15401Kb)
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浏览/下载:250/57
  |  
提交时间:2022/01/12
AMP Exception
AMP Exception
Computational realization of multiple flame stabilization modes in DLR strut-injection hydrogen supersonic combustor
期刊论文
PROCEEDINGS OF THE COMBUSTION INSTITUTE, 2019, 卷号: 37, 期号: 3, 页码: 3685-3692
作者:
Wu K(吴坤)
;
Zhang P(张鹏)
;
Yao W(姚卫)
;
Fan XJ(范学军)
Adobe PDF(1820Kb)
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浏览/下载:468/159
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提交时间:2018/12/27
Supersonic combustion
Flame stabilization mode
DLR Strut injection scheme
Stagnation Temperature
Overall equivalence ratio
Development of Skeletal Kerosene Mechanisms and Application to Supersonic Combustion
期刊论文
ENERGY & FUELS, 2018, 页码: 10.1021/acs.energyfuels.8b03350
作者:
Yao W(姚卫)
;
Wu K(吴坤)
;
Fan XJ(范学军)
Adobe PDF(1388Kb)
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浏览/下载:313/100
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提交时间:2018/12/27
Combustion Condition
Combustor Efficiency
Improved Delayed Detached Eddy Simulations
Initial Temperatures
Laminar Flame Speed
Scramjet Combustors
Supersonic Combustion
Turbulence-chemistry Interactions
Flow characteristic of highly underexpanded jets from various nozzle geometries
期刊论文
APPLIED THERMAL ENGINEERING, 2017, 卷号: 125, 页码: 240-253
作者:
Li XP(李晓鹏)
;
Zhou, Rui
;
Yao W(姚卫)
;
Fan XJ(范学军)
;
Fan, XJ (reprint author), Chinese Acad Sci, State Key Lab High Temp Gas Dynam, Inst Mech, Beijing 100190, Peoples R China.
Adobe PDF(5723Kb)
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浏览/下载:428/188
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提交时间:2017/11/16
Underexpanded Jets
Noncircular Jets
Nozzle Geometry
Large Eddy Simulation
Numerical investigation of characteristic frequency excited highly underexpanded jets
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2017, 卷号: 63, 页码: 304-316
作者:
Li XP
;
Fan E
;
Yao W(姚卫)
;
Fan XJ(范学军)
;
Fan, XJ (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
;
Fan, XJ (reprint author), Univ Chinese Acad Sci, Sch Engn Sci, Beijing 100049, Peoples R China.
Adobe PDF(3588Kb)
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浏览/下载:460/146
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提交时间:2017/07/24
Fuel Jets
Underexpanded Jets
Jet Mixing Control
Excited Jets
Large Eddy Simulation
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)
Adobe PDF(1377Kb)
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  |  
浏览/下载:288/113
  |  
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)
Adobe PDF(1358Kb)
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浏览/下载:433/110
  |  
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
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)
Adobe PDF(1377Kb)
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收藏
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浏览/下载:492/96
  |  
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
A Thermal Analysis Method for Fuel-Cooled Combustor Structure based on Heat Flux Measurement
会议论文
18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference., Tours,France, 2012.9.24-28
作者:
Lu Y(陆阳)
;
Li L(李龙)
;
Fan XJ(范学军)
Adobe PDF(483Kb)
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  |  
浏览/下载:1001/369
  |  
提交时间:2013/02/28