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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./通讯作者:Yao, Wei
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)
Favorite
  |  
View/Download:91/0
  |  
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)
Favorite
  |  
View/Download:182/0
  |  
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)
View
  |  
Adobe PDF(1388Kb)
  |  
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  |  
View/Download:379/124
  |  
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
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)
View
  |  
Adobe PDF(832Kb)
  |  
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  |  
View/Download:342/104
  |  
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 (
[email protected]
)
View
  |  
Adobe PDF(2131Kb)
  |  
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  |  
View/Download:402/140
  |  
Submit date:2017/05/05
Equivalence Ratios
Heat Flux Distributions
Heat Transfer Characteristics
Scramjet
Supercritical Kerosenes
Supersonic Combustion
Supersonic Combustors
Total Temperatures
Performance of the fuel injector in supersonic combustor
会议论文
16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference, Bremen, Germany, October 19, 2009 - October 22, 2009
Authors:
Wei Z(卫喆)
;
Chen LH(陈立红)
;
Gu HB(顾洪斌)
;
Li F(李飞)
;
Gu SL(顾声龙)
;
Chang XY(张新宇)
;
Wei, Z. (
[email protected]
)
View
  |  
Adobe PDF(167Kb)
  |  
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  |  
View/Download:247/64
  |  
Submit date:2017/07/14
Concentration Profiles
Engine Design
Fuel Injectors
Fuel-air Mixing
Gas Sampling
Ramp Injector
Scramjet Combustors
Scramjet Test
Supersonic Combustors