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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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Document Type:会议论文
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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)
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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
A numerical model for evolution of internal structure of cloud cavitation
会议论文
16th International Symposium on Transport Phenomena and Dynamics of Rotating Machinery, ISROMAC 2016, Honolulu, HI, United states, April 10, 2016 - April 15, 2016
Authors:
Du TZ(杜特专)
;
Huang CG(黄晨光)
;
Wang YW(王一伟)
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Submit date:2019/11/20
Bubble break
up
Bubble clusters
Bubble number densities
Cloud cavitations
Condensation rates
Dimension analysis
Evolution modeling
Reynolds Averaged Navier
Stokes Equations
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
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
Authors:
Liu CY
;
Zhang J(张健)
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Submit date:2018/11/08
Oxygen
Diluted environments
Monotonic trend
Partial premixing
Stabilization mechanisms
Transition process
Transitional flames
Transitional process
Turbulent combustion
The effects of air vitiation on the supersonic turbulent channel flow using direct numerical simulation
会议论文
52nd AIAA/SAE/ASEE Joint Propulsion Conference, 2016, Salt Lake City, UT, United states, July 25, 2016 - July 27, 2016
Authors:
Chen XP
;
Li XP(李晓鹏)
;
Dou HS
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Submit date:2017/05/05
Mass Fraction
Mean Velocities
Nondimensional
Reynolds Analogy
Static Temperature
Statistical Characteristics
Temperature Correlation
Turbulent Channel Flows
Full-scale Detached Eddy Simulation of kerosene fueled scramjet combustor based on skeletal mechanism
会议论文
20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Glasgow, United kingdom, July 6, 2015 - July 9, 2015
Authors:
Yao W(姚卫)
;
Wang J(王晶)
;
Lu Y(陆阳)
;
Li XP(李晓鹏)
;
Fan XJ(范学军)
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Submit date:2016/07/01
Adiabatic Flame Temperature
Combustion
Directed Graphs
Flow Separation
Heat Flux
Kerosene
Large Eddy Simulation
Musculoskeletal System
Real Time Systems
Sensitivity Analysis
Spacecraft
Transients
Analysis for Combustion Properties of Crude Oil Pool Fire
会议论文
2014 International Symposium on Safety Science and Technology, Beijing, China, November 4-6, 2014
Authors:
Chen Z(陈阵)
;
Wei XL(魏小林)
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Submit date:2015/09/16
Combustion Properties
Calculation Models
Burning Rate
Flame Shape
Thermal Radiation Intensity
Accident Consequence Simulation Analysis of Pool Fire in Fire Dike
会议论文
2014 International Symposium on Safety Science and Technology, Beijing, China, November 4-6, 2015
Authors:
Zhang M
;
Song WH
;
Wang J
;
Chen Z(陈阵)
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Submit date:2015/09/16
Mathematical Model
Cfd Simulation
Combustion
Heat Radiation Flux
Experiment study on improved closed loop pulsating heat pipe with silver/water nanofluid
会议论文
2nd International Conference on Energy and Environmental Protection (ICEEP 2013), Guilin, China, APR 19-21, 2013
Authors:
Shi WX
;
Li WY
;
Pan LS(潘利生)
;
Shi, WX (reprint author), Beijing Univ Civil Engn & Architecture, Sch Environm & Energy Engn, Beijing 100044, Peoples R China.
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Submit date:2014/02/24
Nanofluid
Improved Closed Loop
Pulsating Heat Pipe
Start Up
Operation Stability
Heat Transfer