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中国科学院力学研究所机构知识库
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Large eddy simulation of rest hypersonic combustor based on dynamic zone flamelet model
会议论文
AIAA Propulsion and Energy 2020 Forum, 24 August 2020 through 28 August 2020
Authors:
Yao W(姚卫)
;
Chen L(陈留)
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Submit date:2021/06/11
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:129/42
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Submit date:2020/11/20
Dynamic zone flamelet model
GH2/GO2
Large Eddy Simulation (LES)
Rocket combustor
Turbulence-chemistry interaction
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
Authors:
Chen L
;
Yao W(姚卫)
;
Fan XJ(范学军)
Adobe PDF(1280Kb)
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Submit date:2020/11/20
BLUFF-BODY FLAMES IN HOT AND DILUTED ENVIRONMENTS
会议论文
ASME Power Conference 2018 (POWER2018), Lake Buena Vista, FL, JUN 24-28, 2018
Authors:
Liu CY.
;
Zhang J(张健)
;
Yang T.
;
Ma YH.
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View/Download:186/57
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Submit date:2019/04/19
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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View/Download:425/210
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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:241/79
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Submit date: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
Authors:
Yao W(姚卫)
;
Fan XJ(范学军)
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Adobe PDF(832Kb)
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View/Download:262/78
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Submit date: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
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)
Adobe PDF(1195Kb)
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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
Intrinsic lengths govern failure mode transition in metallic glasses
会议论文
ICTAM, 北京, 2012-8
Authors:
Dai LH(戴兰宏)
;
Chen Y(陈艳)
Adobe PDF(691Kb)
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View/Download:1768/1219
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Submit date:2013/03/01
Experimental investigation of cavity-based scramjet model
会议论文
14th AIAA/AHI International Space Planes and Hypersonics Systems Technologies Conference, Canberra, Australia, November 6, 2006 - November 9, 2006
Authors:
Gu HB(顾洪斌)
;
Chen LH(陈立红)
;
张新宇(Chang XY)
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Adobe PDF(162Kb)
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View/Download:146/67
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Submit date:2017/06/01
Kerosene Fuel
Mass Flow Rate
Scramjet Engine