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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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张鹏 [8]
范学军 [7]
吴坤 [4]
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张泰昌 [3]
袁越明 [3]
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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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View/Download:443/151
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Submit date:2018/12/27
Supersonic combustion
Flame stabilization mode
DLR Strut injection scheme
Stagnation Temperature
Overall equivalence ratio
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:128/0
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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
Effect of cowl shock on restart characteristics of simple ramp type hypersonic inlets with thin boundary layers
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2018, 卷号: 74, 页码: 72-80
Authors:
Yue LJ(岳连捷)
;
Jia YN(贾轶南)
;
Xu X
;
Zhang XY(张新宇)
;
Zhang P(张鹏)
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Submit date:2018/10/30
Inlet restart
Cowl shock
Shock wave boundary layer interactions
LES Study of Flame Stabilization in DLR Hydrogen Supersonic Combustor with Strut Injection
会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:
Wu K(吴坤)
;
Zhang P(张鹏)
;
Yao W(姚卫)
;
Fan XJ(范学军)
;
Zhang, Peng(pengzhang.zhang@polyu.edu.hk)
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Submit date:2018/01/16
Combustion
Diesel Engines
Hydrogen
Large Eddy Simulation
Spacecraft
Stabilization
Supersonic Aircraft
Temperature Measurement
Wall Flow
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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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
超声速燃烧熄火极限实验研究
会议论文
第八届全国高超声速科技学术会议, 中国黑龙江哈尔滨, 2015-12-28
Authors:
张泰昌
;
袁越明
;
范学军
;
张鹏
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Adobe PDF(625Kb)
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View/Download:346/70
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Submit date:2016/08/16
熄火极限
超声速燃烧
凹腔
火焰稳定
层流火焰
化学发光
剪切层
隔离段
速度计算
总温
超声速燃烧稳焰模式分布研究
会议论文
第八届全国高超声速科技学术会议, 中国黑龙江哈尔滨, 2015-12-28
Authors:
袁越明
;
张泰昌
;
范学军
;
张鹏
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Submit date:2016/08/16
火焰结构
超声速燃烧
凹腔
当量比
燃烧室内
火焰稳定
总温
一维性
隔离段
参数空间