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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... [24]
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张新宇 [24]
陈立红 [24]
李飞 [12]
顾洪斌 [12]
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顾声龙 [6]
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Creator:张新宇
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Creator:陈立红
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Engine performance analysis and optimization of a dual-mode scramjet with varied inlet conditions
期刊论文
ACTA MECHANICA SINICA, 2016, 卷号: 32, 期号: 1, 页码: 75-82
Authors:
Tian L
;
Chen LH(陈立红)
;
Chen Q(陈强)
;
Zhong FQ(仲峰泉)
;
Zhang XY(张新宇)
;
Chen, LH (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
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View/Download:343/87
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Submit date:2016/09/14
Dual-mode Scramjet
Engine Performance
Thrust
Optimization
Heat Release Distribution
Simulated Annealing Algorithm
Experimental study of combustion oscillations in a dual-mode scramjet
会议论文
20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 2015, 2015
Authors:
Tian XD
;
Chen LH(陈立红)
;
Gu HB(顾洪斌)
;
Liu C
;
Cheng LW
;
Chang XY(张新宇)
;
Chen, Lihong (lhchen@imech.ac.cn)
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Submit date:2017/09/04
Quasi-One-Dimensional Multimodes Analysis for Dual-Mode Scramjet
期刊论文
JOURNAL OF PROPULSION AND POWER, 2014, 卷号: 30, 期号: 6, 页码: 1559-1567
Authors:
Tian L
;
Chen LH(陈立红)
;
Chen Q(陈强)
;
Li F(李飞)
;
Zhang XY(张新宇)
;
Tian, L (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:2014/12/18
Plasma-assisted ignition for a kerosene fueled scramjet at Mach 1.8
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2013, 卷号: 28, 期号: 1, 页码: 72-78
Authors:
Li F(李飞)
;
Yu XL(余西龙)
;
Tong YG(仝颖刚)
;
Shen Y(沈岩)
;
Chen J(陈健)
;
Chen LH(陈立红)
;
Zhang XY(张新宇)
;
Yu, XL (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
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Submit date:2013/07/30
Scramjet
Kerosene Fuel
Plasma Torch
Ignition
Numerical simulation of ignition and combustion of ethylene in a supersonic model combustor with a reduced kinetic mechanism
期刊论文
COMBUSTION SCIENCE AND TECHNOLOGY, 2013, 卷号: 185, 期号: 4, 页码: 548-563
Authors:
Zhong FQ(仲峰泉)
;
Chen LH(陈立红)
;
Li F(李飞)
;
Zhang XY(张新宇)
;
Sung CJ
;
Zhong, FQ (reprint author), Chinese Acad Sci, State Key Lab High Temp Gas Dynam, Inst Mech, Beijing 100190, Peoples R China.
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View/Download:1430/487
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Submit date:2013/05/03
Ethylene
Ignition
Numerical Simulation
Reduced Kinetic Mechanism
Supersonic Combustion
Study on Judgment Method of Combustion Mode on Dual-mode Scramjet
会议论文
7th Asian-Pacific Conference on Aerospace Technology and Science, 7th APCATS 2013, Taiwan, China, MAY 23-26, 2013
Authors:
Chen Q(陈强)
;
Chen LH(陈立红)
;
Gu HB(顾洪斌)
;
Zhang XY(张新宇)
;
Wang P
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Submit date:2014/03/11
Combustion Mode
Scramjet
Artificial Neural Network
Study on Judgment Method of Combustion Mode on Dual-mode Scramjet
期刊论文
Procedia Engineering, 2013, 卷号: 67, 页码: 147-154
Authors:
Chen Q(陈强)
;
Chen LH(陈立红)
;
Gu HB(顾洪斌)
;
Zhang XY(张新宇)
;
Wang P
Adobe PDF(771Kb)
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Submit date:2015/09/24
Scramjet
Artificial Neural Network
A compact sensor based on near infrared absorption spectroscopy for flow diagnostics in a low density hydrogen and oxygen combustion driven shock tube
期刊论文
Lasers in Engineering, 2012, 卷号: 23, 期号: 1-2, 页码: 1-17
Authors:
Yu XL(余西龙)
;
Li F(李飞)
;
Chen LH(陈立红)
;
Chang XY(张新宇)
Adobe PDF(1693Kb)
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Submit date:2012/12/04
Tunable Diode-laser
Water-vapor
Scramjet Combustor
Temperature
Gases
H2o
Co
Oh
Tunable Diode Laser Absorption Spectroscopy (Tdlas)
Combustion
Rapid Time-division-multiplexing (Tdm)
Temperature
Water Vapour Concentration
Low Density Shock Tube
A coupled heat transfer analysis with effects of thermal/catalytic cracking of kerosene for regenerative cooled supersonic combustor
会议论文
23rd International Congress of Theoretical and Applied Mechanics, 中国北京/Beijing, China, 2012-08-19
Authors:
Wang X(王曦)
;
Zhong FQ(仲峰泉)
;
Chen LH(陈立红)
;
Zhang XY(张新宇)
Adobe PDF(113Kb)
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Submit date:2014/04/02
Kerosene
Combustor
Thermal
Regenerative
Coupled
Catalytic
Cracking
Analysis
Supersonic
Transfer
Cooled
Effects
Board
Solving
Extra
Through
Differ
Energy
Cooling
Model
Modeling and measurements of heat release distributions in dual-mode scramjet combustor
会议论文
18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference 2012, Tours, France, SEP 24-28, 2012
Authors:
Tian L(田璐)
;
Chen LH(陈立红)
;
Chen Q(陈强)
;
Li F(李飞)
;
Zhang XY(张新宇)
;
Tian L(田璐)
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Adobe PDF(677Kb)
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View/Download:627/199
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Submit date:2014/02/24