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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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张新宇 [9]
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Document Type:会议论文
Author:张新宇
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Experimental Study of Ignition and Flame Characteristics of Surrogate of Cracked Hydrocarbon Fuels in Supersonic Crossflow
会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:
Cheng LW(程柳维)
;
Zhong FQ(仲峰泉)
;
Wang ZP(王知溥)
;
Gu HB(顾洪斌)
;
Ma SG(马素刚)
;
Zhang XY(张新宇)
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Submit date:2018/01/16
Combustors
Cracks
Diesel Engines
Efficiency
Ethylene
Fighter Aircraft
Fuels
High Speed Cameras
Ignition
Kerosene
Luminance
Spacecraft
Stabilization
Large eddy simulation of ignition and combustion of ethylene/air turbulent jet diffusion flame with reduced kinetic mechanism
会议论文
20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 2015, Glasgow, United kingdom, July 6, 2015 - July 9, 2015
Authors:
Ma SG(马素刚)
;
Zhong FQ(仲峰泉)
;
Zhang XY(张新宇)
;
Zhong, Fengquan (fzhong@imech.ac.cn)
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Submit date:2017/05/05
Combustion Pro
Cess
Directed Relation Graph
Dynamic Evolution
Fuel Injection Velocities
Kinetic Mechanism
Reduced Mechanisms
Temperature Profiles
Temporal And Spatial Evolutions
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
定向关系图法在碳氢化合物机理简化中的应用研究
会议论文
LHD2013夏季学术研讨会, 河北平山, 2013
Authors:
仲峰泉
;
马素刚
;
陈立红
;
张新宇
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Submit date:2014/01/23
简化机理
直接关系图法
碳氢燃料
点火延迟时间
Three-Dimensional heat transfer analysis and optimized design of actively cooled strut for scramjet applications
会议论文
48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2012, Atlanta, GA, United states, JUL 30-AUG 01, 2012
Authors:
Zhong FQ(仲峰泉)
;
Chen TY(陈同银)
;
Fan XJ(范学军)
;
Chen LH(陈立红)
;
Zhang XY(张新宇)
;
Zhong FQ(仲峰泉)
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Submit date:2014/02/24
超临界态煤油圆管湍流的流阻特性研究
会议论文
LHD2012夏季学术研讨会, 吉林延吉, 2012
Authors:
党国鑫
;
仲峰泉
;
陈立红
;
张新宇
Adobe PDF(1631Kb)
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Submit date:2014/01/23
煤油
超临界
流阻
雷诺相似
数值研究
Performance of a Supersonic Model Combustor using Vaporized Kerosene Injection
会议论文
40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Fort Lauderdale, Florida, July 11-14, 2004, Florida, July 11-14, 2004
Authors:
Fan XJ(范学军)
;
Yu G(俞刚)
;
Li JG(李建国)
;
Zhang XY(张新宇)
;
Sun ZR(孙知人)
;
Fan XJ(范学军)
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Submit date:2007/12/18
Investigation of Vaporized Kerosene Injection and Combustion in a Supersonic Model Combustor
会议论文
AIAA/ASME/SAE/ASEE 40th Joint Propulsion Conference
Authors:
Fan XJ(范学军)
;
Yu G(俞刚)
;
Li JG(李建国)
;
Zhang XY(张新宇)
;
Sung CJ
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Submit date:2007/12/18
Combustion of kerosene in a supersonic stream
会议论文
38th Aerospace Sciences Meeting and Exhibit 2000, Reno, NV, United states, January 10, 2000 - January 13, 2000
Authors:
Li JG(李建国)
;
Yu G(俞刚)
;
Zhang XY(张新宇)
;
Huang QS
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Submit date:2017/06/01
Cavity Flame Holders
Combustion Efficiencies
Combustor Performance
Equivalence Ratios
Modular Structures
Optimized Conditions
Stagnation Pressures
Supersonic Combustors