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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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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
Authors:
Prapamonthon P
;
Yooyen S
;
Sleesongsom S
Adobe PDF(1747Kb)
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View/Download:199/40
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Submit date:2020/03/14
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
Authors:
Yao W(姚卫)
;
Li B(李波)
Adobe PDF(1665Kb)
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View/Download:173/51
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Submit date:2020/11/20
Dynamic zone flamelet model
GH2/GO2
Large Eddy Simulation (LES)
Rocket combustor
Turbulence-chemistry interaction
A novel method of cooling channel optimization for active-cooled structure using the calculus of variations
会议论文
AIAA Propulsion and Energy Forum and Exposition, 2019, Indianapolis, IN, United states, August 19, 2019 - August 22, 2019
Authors:
Li X(李轩)
;
Lu Y(陆阳)
;
Wu K(吴坤)
;
Fan XJ(范学军)
Adobe PDF(705Kb)
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Submit date:2020/11/20
Numerical investigation of orthogonal cutting processes with tool vibration of Ti6Al4V alloy
会议论文
17th CIRP Conference on Modelling of Machining Operations, CIRP CMMO, Sheffield, United kingdom, June 13, 2019 - June 14, 2019
Authors:
Shuang F(双飞)
;
Ma W(马维)
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Adobe PDF(872Kb)
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Submit date:2019/11/20
Forced vibration
Self
excited vibrations
Shear banding
Stability limit
Vibration cutting
Numerical prediction of cooling performance sensitivity of 1st stage nozzle guide vane under aerothermal conditions
会议论文
ASME 2019 Gas Turbine India Conference, GTINDIA 2019, Chennai, Tamil Nadu, India, December 5, 2019 - December 6, 2019
Authors:
Prapamonthon P
;
Yin B(银波)
;
Yang GW(杨国伟)
;
Zhang MH(张莫晗)
Adobe PDF(2782Kb)
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Submit date:2020/11/20
Aerothermal condition
Cooling effectiveness
Cooling performance
Thermal sensitivity
Turbine vane
Influence of Chemical Mechanisms on Supersonic Combustion Characteristics Fueled by Kerosene
会议论文
2018 Joint Propulsion Conference, Cincinnati, Ohio, July 9-11, 2018
Authors:
Yao W(姚卫)
;
Wu K(吴坤)
;
Lee YC(李亚超)
;
Fan XJ(范学军)
Adobe PDF(1156Kb)
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View/Download:464/0
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Submit date:2018/12/26
Real-gas Effect Accounted for by the Principle of Extended Corresponding States in Modeling Supersonic Kerosene Jet
会议论文
2018 Joint Propulsion Conference, Cincinnati, Ohio. , July 9-11, 2018
Authors:
Wang Y
;
Yao W(姚卫)
;
Fan XJ(范学军)
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Submit date:2018/12/26
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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  |  
Adobe PDF(1377Kb)
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View/Download:315/121
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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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View/Download:457/116
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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