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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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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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Submit date:2017/05/05
Equivalence Ratios
Heat Flux Distributions
Heat Transfer Characteristics
Scramjet
Supercritical Kerosenes
Supersonic Combustion
Supersonic Combustors
Total Temperatures
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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View/Download:496/179
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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
Numerical study of conjugate heat transfer of supercritical kerosene flow in rectangular cooling channel
会议论文
15th International Heat Transfer Conference, IHTC 2014, Kyoto, Japan, August 10, 2014 - August 15, 2014
Authors:
Zhong FQ(仲峰泉)
;
Dang GX(党国鑫)
;
Xing YF(邢云绯)
;
Chen LH(陈立红)
;
Zhang XY(张新宇)
;
Zhong, Fengquan (fzhong@imech.ac.cn)
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Submit date:2017/05/27
Conjugate Heat Transfer
Heat Conduction Equations
Numerical Study
Pseudo-critical Temperature
Rectangular Cooling Channels
Supercritical Kerosenes
Thermodynamic And Transport Properties
Turbulent Transports
Flow rate analyses and calibrations of kerosene cracking for supersonic combustion
会议论文
41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Tucson, AZ, United states, July 10, 2005 - July 13, 2005
Authors:
Fan XJ(范学军)
;
Yu G(俞刚)
;
Li JG(李建国)
Adobe PDF(315Kb)
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Submit date:2017/06/01
Average Molecular Weight
Chemical Formulae
Cracking Model
Gaseous Products
High Temperature
Ideal Gas Law
Ideal Gas Mixtures
Mass Flow Rate
Mole Fraction
Residence Time
Room Temperature
Sonic Nozzle
Supercritical Condition
Supersonic Combustion
Temperature Dependencies
Thermal Cracking
Three-component