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Knowledge Management System of Institue of Mechanics, CAS
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Numerically thermal analysis of a turbine vane at high temperature
会议论文
5th International Workshop on Heat/Mass Transfer Advances for Energy Conservation and Pollution Control, IWHT 2019, Novosibirsk, Russia, August 13, 2019 - August 16, 2019
作者:
Prapamonthon P
;
Yooyen S
;
Sleesongsom S
Adobe PDF(1747Kb)
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浏览/下载:166/29
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提交时间:2020/03/14
Comparative Heat Flux Measurement of a Sharp Cone Between Three Hypersonic Test Facilities at LHD
会议论文
31st International Symposium on Shock Waves, Nagoya, Japan, 2017-07-9~14
作者:
Wang Q(汪球)
;
Lu P(卢盼)
;
Li JW(栗继伟)
;
Wu S(吴松)
;
Li JP(李进平)
;
Zhao W(赵伟)
;
Jiang ZL(姜宗林)
Adobe PDF(299Kb)
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浏览/下载:75/29
  |  
提交时间:2023/03/17
Aerodynamic Testing at Duplicating Hypersonic Flight Conditions with Hyper-Dragon
会议论文
31st International Symposium on Shock Waves, Nagoya, Japan, 2017-07-9~14
作者:
Jiang ZL(姜宗林)
;
Yu HR(俞鸿儒)
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Adobe PDF(523Kb)
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浏览/下载:453/52
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提交时间:2020/01/06
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:275/112
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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)
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Adobe PDF(1358Kb)
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浏览/下载:416/104
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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
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)
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Adobe PDF(1377Kb)
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浏览/下载:475/90
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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
Detailed transitional process of the flames in hot and diluted environments from lifted flames to MILD combustion
会议论文
10th U.S. National Combustion Meeting, College Park, MD, United states, April 23, 2017 - April 26, 2017
作者:
Liu CY
;
Zhang J(张健)
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Adobe PDF(414Kb)
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浏览/下载:212/74
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提交时间:2018/11/08
Oxygen
Diluted environments
Monotonic trend
Partial premixing
Stabilization mechanisms
Transition process
Transitional flames
Transitional process
Turbulent combustion
Pressure and Heat Flux Calibration of the Long-test-duration Hypervelocity Detonation-driven Shock Tunnel
会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
作者:
Wang Q(汪球)
;
Li JW
;
Lu P
;
Li JP(李进平)
;
Zhao W(赵伟)
;
Jiang ZL(姜宗林)
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Adobe PDF(679Kb)
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浏览/下载:380/66
  |  
提交时间:2018/01/16
Calibration
Detonation
Heat Transfer
Nozzles
Spacecraft
Supersonic Aerodynamics
Thermodynamics
Uncertainty Analysis
Development of a radiative heating system for studies of heat transfer in fuel-cooled structures
会议论文
14th International Energy Conversion Engineering Conference, Salt Lake City, UT, JUL 25-27, 2016
作者:
Dong D(董达)
;
Lu Y(陆阳)
;
Yuan YM(袁越明)
;
Fan XJ(范学军)
;
Dong, D (reprint author), Chinese Acad Sci, Inst Mech, LHD, Beijing 100190, Peoples R China.
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Adobe PDF(637Kb)
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浏览/下载:288/72
  |  
提交时间:2017/05/12
Aviation Kerosene
Supercritical Conditions
Pressure
Rp-3
Measurement of heat flux distribution of supercritical kerosene fueled supersonic combustor
会议论文
32nd AIAA Aerodynamic Measurement Technology and Ground Testing Conference, 2016, Washington, DC, United states, June 13, 2016 - June 17, 2016
作者:
Cheng D(程迪)
;
Wang J(王晶)
;
Gong J
;
Lu Y(陆阳)
;
Yao W(姚卫)
;
Li L(李龙)
;
Fan XJ(范学军)
;
Fan, Xuejun (xfan@imech.ac.cn)
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Adobe PDF(2131Kb)
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浏览/下载:317/121
  |  
提交时间:2017/05/05
Equivalence Ratios
Heat Flux Distributions
Heat Transfer Characteristics
Scramjet
Supercritical Kerosenes
Supersonic Combustion
Supersonic Combustors
Total Temperatures