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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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State Key... [20]
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范学军 [20]
姚卫 [18]
李晓鹏 [14]
吴坤 [10]
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Author:范学军
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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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Submit date:2018/12/27
Supersonic combustion
Flame stabilization mode
DLR Strut injection scheme
Stagnation Temperature
Overall equivalence ratio
Comparative Study of Elliptic and Round Scramjet Combustors Fueled by RP-3
期刊论文
JOURNAL OF PROPULSION AND POWER, 2018, 卷号: 34, 期号: 3, 页码: 772-786
Authors:
Yao W(姚卫)
;
Yuan YM(袁越明)
;
Li XP(李晓鹏)
;
Wang J(王晶)
;
Wu K(吴坤)
;
Fan XJ(范学军)
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Submit date:2018/07/17
Comparative Study of Elliptic and Round Scramjet Combustors Fueled by RP-3
会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, PEOPLES R CHINA, MAR 06-09, 2017
Authors:
Yao W(姚卫)
;
Yuan YM(袁越明)
;
Li XP(李晓鹏)
;
Wang J(王晶)
;
Wu K(吴坤)
;
Fan XJ(范学军)
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Submit date:2018/06/06
Flow characteristic of highly underexpanded jets from various nozzle geometries
期刊论文
APPLIED THERMAL ENGINEERING, 2017, 卷号: 125, 页码: 240-253
Authors:
Li XP(李晓鹏)
;
Zhou, Rui
;
Yao W(姚卫)
;
Fan XJ(范学军)
;
Fan, XJ (reprint author), Chinese Acad Sci, State Key Lab High Temp Gas Dynam, Inst Mech, Beijing 100190, Peoples R China.
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Submit date:2017/11/16
Underexpanded Jets
Noncircular Jets
Nozzle Geometry
Large Eddy Simulation
Numerical investigation of characteristic frequency excited highly underexpanded jets
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2017, 卷号: 63, 页码: 304-316
Authors:
Li XP
;
Fan E
;
Yao W(姚卫)
;
Fan XJ(范学军)
;
Fan, XJ (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
;
Fan, XJ (reprint author), Univ Chinese Acad Sci, Sch Engn Sci, Beijing 100049, Peoples R China.
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Submit date:2017/07/24
Fuel Jets
Underexpanded Jets
Jet Mixing Control
Excited Jets
Large Eddy Simulation
高度欠膨胀声速射流的自相似特性
期刊论文
航空动力学报, 2017, 卷号: 32, 期号: 01, 页码: 177-187
Authors:
李晓鹏
;
姚卫
;
范学军
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Submit date:2017/12/22
高度欠膨胀射流
大涡模拟
自相似特性
高斯拟合
剪切层发展
A comparative study of elliptical and round scramjet combustors by Improved Delayed Detached Eddy Simulation
会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:
Yao W(姚卫)
;
Yuan YM(袁越明)
;
Li XP(李晓鹏)
;
Wang J(王晶)
;
Fan XJ(范学军)
;
Fan, Xuejun(xfan@imech.ac.cn)
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Submit date:2018/01/16
Adiabatic Flame Temperature
Aerodynamics
Boundary Layer Flow
Boundary Layers
Chemical Analysis
Combustion
Computational Chemistry
Directed Graphs
Flow Separation
Mach Number
Principal Component Analysis
Regression Analysis
Sensitivity Analysis
Spacecraft
Supersonic Aerodynamics
Supersonic Aircraft
Transients
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
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
高度欠膨胀射流的瞬态近场结构
期刊论文
推进技术, 2016, 卷号: 37, 期号: 12, 页码: 2233-2242
Authors:
李晓鹏
;
吴坤
;
姚卫
;
范学军
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Submit date:2017/12/26
高度欠膨胀射流
大涡模拟
近场结构
瞬态非定常特征