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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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A one-dimensional transient calculation method for flow instability of supercritical hydrocarbon in cooling channels
会议论文
AIAA Propulsion and Energy Forum, VIRTUAL EVENT, 2021年8月9-11日
Authors:
Jin YC(靳一超)
;
Wu K(吴坤)
;
Lu Y(陆阳)
;
Fan XJ(范学军)
Adobe PDF(1121Kb)
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Submit date:2022/07/04
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
Authors:
Jin Y
;
Liao F(廖飞)
;
Cai JS
;
Morris PJ
Adobe PDF(2986Kb)
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View/Download:247/85
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Submit date:2020/11/20
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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Submit date:2020/11/20
Dynamic zone flamelet model
GH2/GO2
Large Eddy Simulation (LES)
Rocket combustor
Turbulence-chemistry interaction
Supercritical GN2/GH2 jet modeled by the ECS method
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)
;
Jin YC(靳一超)
;
Lee YC(李亚超)
Adobe PDF(1048Kb)
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Submit date:2020/11/20
Numerical simulation of proppant transportation in hydraulic fracture based on DDPM-KTGF model
会议论文
ASME-JSME-KSME 2019 8th Joint Fluids Engineering Conference, AJKFluids 2019, San Francisco, CA, United states, July 28, 2019 - August 1, 2019
Authors:
Zhang Y(张岩)
;
Lu XB(鲁晓兵)
;
Zhang XH(张旭辉)
;
Li P(李鹏)
Adobe PDF(1313Kb)
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Submit date:2020/11/20
DDPM-KTGF model
Hydraulic fracturing
Proppant transportation
Two-phase flow
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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Submit date:2018/12/26
Comparative Study of Elliptic and Round Scramjet Combustors Fueled by RP-3
会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, PEOPLES R CHINA, MAR 06-09, 2017
Authors:
Yao W(姚卫)
;
Yuan YM(袁越明)
;
Li XP(李晓鹏)
;
Wang J(王晶)
;
Wu K(吴坤)
;
Fan XJ(范学军)
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  |  
Adobe PDF(805Kb)
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Submit date:2018/06/06
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
Authors:
Su JH
;
Chen XD(陈晓东)
;
Hu GQ(胡国庆)
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Adobe PDF(6321Kb)
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Submit date:2018/06/06
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
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
Authors:
Yao W(姚卫)
;
Fan XJ(范学军)
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Adobe PDF(623Kb)
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View/Download:296/105
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Submit date:2018/01/16
Combustion
Cost Benefit Analysis
Costs
Mixtures
Spacecraft
Supersonic Aircraft