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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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范学军 [10]
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吴坤 [5]
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Indexed By:EI
Creator:范学军
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Language:英语
Document Type:期刊论文
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An experimental investigation of supersonic combustion of cracked JP-10
期刊论文
ACTA ASTRONAUTICA, 2023, 卷号: 203, 页码: 329-340
Authors:
Cui NF(崔乃夫)
;
Rao W(饶威)
;
Li YJ(李昱君)
;
Zhu, Yinhai
;
Zhang TC(张泰昌)
;
Fan XJ(范学军)
Adobe PDF(14542Kb)
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Submit date:2023/02/07
Cracking
JP-10
Supersonic combustion
Regenerative cooling
An Experimental Investigation of Supersonic Combustion of Mildly Cracked N-Dodecane
期刊论文
COMBUSTION SCIENCE AND TECHNOLOGY, 2022, 页码: 20
Authors:
Cui NF(崔乃夫)
;
Rao W(饶威)
;
Li YJ(李昱君)
;
Zhang TC(张泰昌)
;
Fan XJ(范学军)
Adobe PDF(10728Kb)
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Submit date:2022/11/14
Mildly cracked
n-dodecane
supersonic combustion
regenerative cooling
On jet-wake flame stabilization in scramjet: A LES/RANS study from chemical kinetic and fluid-dynamical perspectives
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2022, 卷号: 120, 页码: 12
Authors:
Wu K(吴坤)
;
Zhang, Peng
;
Fan XJ(范学军)
Adobe PDF(3834Kb)
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Submit date:2022/01/24
Supersonic combustion
Jet-wake flame stabilization
Hybrid LES
RANS
Detailed hydrogen chemistry
Counter-rotating vortex pair
Wall Heat Flux Measurements for a Kerosene-Fueled Supersonic Combustor
期刊论文
JOURNAL OF AEROSPACE ENGINEERING, 2019, 卷号: 32, 期号: 5, 页码: 11
Authors:
Cheng D(程迪)
;
Wang J(王晶)
;
Lu Y(陆阳)
;
Li L(李龙)
;
Yao W(姚卫)
;
Fan XJ(范学军)
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Submit date:2019/09/09
Heat flux measurement
Kerosene
Supersonic combustion
Scramjet
Heat flux sensor
Computational realization of multiple flame stabilization modes in DLR strut-injection hydrogen supersonic combustor
期刊论文
PROCEEDINGS OF THE COMBUSTION INSTITUTE, 2019, 卷号: 37, 期号: 3, 页码: 3685-3692
Authors:
Wu K(吴坤)
;
Zhang P(张鹏)
;
Yao W(姚卫)
;
Fan XJ(范学军)
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Adobe PDF(1820Kb)
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Submit date:2018/12/27
Supersonic combustion
Flame stabilization mode
DLR Strut injection scheme
Stagnation Temperature
Overall equivalence ratio
On the application of tabulated dynamic adaptive chemistry in ethylene-fueled supersonic combustion
期刊论文
COMBUSTION AND FLAME, 2018, 卷号: 197, 页码: 265-275
Authors:
Wu K(吴坤)
;
Contino F
;
Yao W(姚卫)
;
Fan XJ(范学军)
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View/Download:580/198
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Submit date:2018/12/12
Tabulated dynamic adaptive chemistry
Skeletal mechanism
Supersonic combustion
Ethylene
Large Eddy Simulation
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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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
Characterization of flame stabilization modes in an ethylene-fueled supersonic combustor using time-resolved CH* chemiluminescence
期刊论文
PROCEEDINGS OF THE COMBUSTION INSTITUTE, 2017, 卷号: 36, 期号: 2, 页码: 2919-2925
Authors:
Yuan YM(袁越明)
;
Zhang TC(张泰昌)
;
Yao W(姚卫)
;
Fan XJ(范学军)
;
Zhang P(张鹏)
;
Fan, XJ (reprint author), Chinese Acad Sci, State Key Lab High Temp Gas Dynam, Beijing 100190, PR, Peoples R China.
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View/Download:333/106
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Submit date:2017/12/27
Supersonic Combustion
Flame Stabilization
Stagtnation Temperature
Gloabal Equivalence Ratio
Ch** Ch*emiluminesenCh*e
Numerical Investigation on Flame Stabilization in DLR Hydrogen Supersonic Combustor with Strut Injection
期刊论文
COMBUSTION SCIENCE AND TECHNOLOGY, 2017, 卷号: 189, 期号: 12, 页码: 2154-2179
Authors:
Wu K(吴坤)
;
Zhang P(张鹏)
;
Yao W(姚卫)
;
Fan XJ(范学军)
;
Zhang, P (reprint author), Hong Kong Polytech Univ, Dept Mech Engn, Hong Kong 999077, Hong Kong, Peoples R China.
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Submit date:2017/12/18
Detailed Hydrogen Oxidation Mechanism
Dlr
Flame Stabilization
Sensitivity Analysis
Supersonic Combustion
Effects of entry conditions on cracked kerosene-fueled supersonic combustor performance
期刊论文
Combustion Science and Technology, 2007, 卷号: 179, 期号: 10, 页码: 2199-2217
Authors:
Fan XJ(范学军)
;
Yu G(俞刚)
;
Li JG(李建国)
;
Yue LJ(岳连捷)
;
Zhang XY(张新宇)
;
Sung CJ
;
Fan, XJ (reprint author), Chinese Acad Sci, Inst Mech, Beijing 100080, Peoples R China.
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Submit date:2009/08/03
Entry Conditions
Kerosene
Supersonic Combustion
Thermal Cracking
Model Combustor
Propulsion
Injection