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Influence of compressibility effect on supersonic combustion modeling
会议论文
AIAA Propulsion and Energy Forum and Exposition, 2019, Indianapolis, IN, United states, August 19, 2019 - August 22, 2019
作者:
Chen L
;
Yao W(姚卫)
;
Fan XJ(范学军)
Adobe PDF(1280Kb)
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浏览/下载:155/72
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提交时间:2020/11/20
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
作者:
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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浏览/下载:412/0
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提交时间:2018/12/26
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
作者:
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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Adobe PDF(1173Kb)
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浏览/下载:434/214
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提交时间: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
作者:
Yao W(姚卫)
;
Fan XJ(范学军)
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Adobe PDF(623Kb)
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浏览/下载:254/85
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提交时间:2018/01/16
Combustion
Cost Benefit Analysis
Costs
Mixtures
Spacecraft
Supersonic Aircraft
Development of zone flamelet modelfor scramjet combustor modeling
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:
Yao W(姚卫)
;
Fan XJ(范学军)
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Adobe PDF(832Kb)
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浏览/下载:269/80
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提交时间:2018/11/08
Combustion
Cost benefit analysis
Costs
Mixtures
Ramjet engines
Supersonic aircraft
Computational costs
Equivalence ratios
Local flow conditions
Scramjet combustors
Statistics approaches
Supersonic combustion
Supersonic combustors
Turbulent combustion
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
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
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提交时间:2017/05/12
Aviation Kerosene
Supercritical Conditions
Pressure
Rp-3
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
作者:
Yao W(姚卫)
;
Wang J(王晶)
;
Lu Y(陆阳)
;
Li XP(李晓鹏)
;
Fan XJ(范学军)
Adobe PDF(1195Kb)
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浏览/下载:465/170
  |  
提交时间: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
Characteristic scales in supersonic combustion
会议论文
49th AIAA/ASME/SAE/ASEE Joint PropulsionConference, San Jose, CA, United states, JUL 14-17, 2013
作者:
Li XP(李晓鹏)
;
Fan XJ(范学军)
;
Li XP(李晓鹏)
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Adobe PDF(669Kb)
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浏览/下载:673/240
  |  
提交时间:2014/02/24
A coupled heat transfer analysis with effects of thermal/catalytic cracking of kerosene for regenerative cooled supersonic combustor
会议论文
23rd International Congress of Theoretical and Applied Mechanics, 中国北京/Beijing, China, 2012-08-19
作者:
Wang X(王曦)
;
Zhong FQ(仲峰泉)
;
Chen LH(陈立红)
;
Zhang XY(张新宇)
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Adobe PDF(113Kb)
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浏览/下载:407/109
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提交时间:2014/04/02
Kerosene
Combustor
Thermal
Regenerative
Coupled
Catalytic
Cracking
Analysis
Supersonic
Transfer
Cooled
Effects
Board
Solving
Extra
Through
Differ
Energy
Cooling
Model