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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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Nonequilibrium Heating/Cooling Effects in a Mach Number 10 Hydrogen-Fueled Scramjet
期刊论文
JOURNAL OF PROPULSION AND POWER, 2024, 页码: 17
Authors:
Liu H(刘杭)
;
Yao W(姚卫)
;
Zhang X(张旭)
;
Zhang XY(张晓源)
;
Liu, Jianwen
;
Yue LJ(岳连捷)
;
Sun QH(孙泉华)
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View/Download:54/0
  |  
Submit date:2024/03/11
Scramjet
Dynamic Zone Flamelet Model
High Enthalpy Shock Tunnel
Combustors
Improved Delayed Detached Eddy Simulation
Vibrational Energy
nonequilibrium heating
cooling effects
thermal nonequilibrium
chemical nonequilibrium
hydrogen
Modeling Analysis on Cavity-based Flame Stabilization in Scramjet Combustor
会议论文
12th Asia-Pacific Conference on Combustion, ASPACC 2019, Fukuoka, Japan, July 1, 2019 - July 5, 2019
Authors:
Wu K(吴坤)
;
Zhang P(张鹏)
;
Fan XJ(范学军)
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View/Download:146/0
  |  
Submit date:2019/11/20
Combustion chemistry
Combustion dynamics
Dual
mode scramjet
Flame stabilization
Improved delayed detached eddy simulations
Overall reactions
Scramjet combustors
Shock
wave structures
Development of Skeletal Kerosene Mechanisms and Application to Supersonic Combustion
期刊论文
ENERGY & FUELS, 2018, 页码: 10.1021/acs.energyfuels.8b03350
Authors:
Yao W(姚卫)
;
Wu K(吴坤)
;
Fan XJ(范学军)
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  |  
Adobe PDF(1388Kb)
  |  
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  |  
Submit date:2018/12/27
Combustion Condition
Combustor Efficiency
Improved Delayed Detached Eddy Simulations
Initial Temperatures
Laminar Flame Speed
Scramjet Combustors
Supersonic Combustion
Turbulence-chemistry Interactions
Experimental Study of Ignition and Flame Characteristics of Surrogate of Cracked Hydrocarbon Fuels in Supersonic Crossflow
会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:
Cheng LW(程柳维)
;
Zhong FQ(仲峰泉)
;
Wang ZP(王知溥)
;
Gu HB(顾洪斌)
;
Ma SG(马素刚)
;
Zhang XY(张新宇)
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  |  
Adobe PDF(517Kb)
  |  
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  |  
View/Download:334/109
  |  
Submit date:2018/01/16
Combustors
Cracks
Diesel Engines
Efficiency
Ethylene
Fighter Aircraft
Fuels
High Speed Cameras
Ignition
Kerosene
Luminance
Spacecraft
Stabilization
Experimental Studies of Film Cooling in Supersonic Combustors
会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:
Fan C(樊川)
;
Wang J(王晶)
;
Fan XJ(范学军)
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  |  
Adobe PDF(735Kb)
  |  
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  |  
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  |  
Submit date:2018/01/16
Combustion
Combustors
Coolants
Kerosene
Spacecraft
Supersonic Aerodynamics
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:299/90
  |  
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
Measurement of heat flux distribution of supercritical kerosene fueled supersonic combustor
会议论文
32nd AIAA Aerodynamic Measurement Technology and Ground Testing Conference, 2016, Washington, DC, United states, June 13, 2016 - June 17, 2016
Authors:
Cheng D(程迪)
;
Wang J(王晶)
;
Gong J
;
Lu Y(陆阳)
;
Yao W(姚卫)
;
Li L(李龙)
;
Fan XJ(范学军)
;
Fan, Xuejun (xfan@imech.ac.cn)
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  |  
Adobe PDF(2131Kb)
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  |  
Submit date:2017/05/05
Equivalence Ratios
Heat Flux Distributions
Heat Transfer Characteristics
Scramjet
Supercritical Kerosenes
Supersonic Combustion
Supersonic Combustors
Total Temperatures
Development and Preliminary Validation of A Thermal Analysis Method for Hydrocarbon Regenerative-cooled Supersonic Combustor
会议论文
20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Glasgow, Scotland, 6-9 July, 2015
Authors:
Lu Y(陆阳)
;
Wang XZ(王新竹)
;
Li L(李龙)
;
Cheng D(程迪)
;
Yuan T(袁涛)
;
Yao W(姚卫)
;
Fan XJ(范学军)
Adobe PDF(445Kb)
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  |  
Submit date:2016/01/08
Hydrocarbons
Combustors
Cooling
Heat Transfer
Equilibrium modeling for optimum design of operation parameters of MSW plasma gasification
会议论文
International Conference on Thermal Treatment Technologies and Hazardous Waste Combustors 2011, Jacksonville, FL, United states, MAY 10-13, 2011
Authors:
Wang GQ(王贵全)
;
Li YJ(李要建)
;
Xu YX(徐永香)
;
Sheng HZ(盛宏至)
;
Wang GQ(王贵全)
Adobe PDF(1183Kb)
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  |  
Submit date:2013/02/26
Combustion
Combustors
Hazardous Materials
Heat Treatment
Heating
Moisture
Moisture Determination
Municipal Solid Waste
Plasma Jets
Plasma Torches
Plasmas
Synthesis Gas
Technology
Waste Treatment
Chinese Academy Of Sciences
Concentration Distributions
Constraint Conditions
Duration Time
Environmentally-friendly Technology
Equilibrium Modeling
Equilibrium Models
Excess Air Ratios
Feeding Rate
Gasification Process
Gasification Temperatures
Gasifiers
Heating Value
High Temperature
Low Emission
Msw
Operating Parameters
Operation Parameters
Optimum Designs
Plasma Gasification
Process Parameters
Product Distributions
Simulation
State Of The Art
Syn-gas
Volume Reductions
Working Parameters
Theoretical and engineering research on the municipal solid waste plasma gasification
会议论文
International Conference on Thermal Treatment Technologies and Hazardous Waste Combustors 2011, Jacksonville, FL, United states, MAY 10-13, 2011
Authors:
Sheng HZ(盛宏至)
;
Deng J(邓晶)
;
Li YJ(李要建)
;
Xu YX(徐永香)
;
Sheng HZ(盛宏至)
Adobe PDF(1653Kb)
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  |  
Submit date:2013/02/26
Atmospheric Pressure
Calorific Value
Combustion
Combustors
Conceptual Design
Energy Conversion
Gas Engines
Gasification
Hazardous Materials
Heat Treatment
Hydrochloric Acid
Organic Pollutants
Plasma Applications
Plasmas
Radioactive Waste Disposal
Synthesis Gas
Waste Disposal
Waste Treatment
Cooling Process
Dew Points
Energy Recovery
Engine Generator
Environmentally-friendly Technology
Hcl Gas
High Temperature
Hot Syngas
Kitchen Garbage
Lower Heating Value
Msw
Plasma Gasification
Plasma Reactors
Pre-processing
Pretreatment Systems
Reaction Temperature
Reactor
Reactor Chamber
Syn-gas