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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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仲峰泉 [10]
张新宇 [10]
reprint au... [4]
邢云绯 [4]
张永江 [2]
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Creator:张新宇
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Date Issued:2015
Author:张新宇
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Numerical study of combustion and convective heat transfer of a Mach 2.5 supersonic combustor
期刊论文
APPLIED THERMAL ENGINEERING, 2015, 卷号: 89, 页码: 883-896
Authors:
Wang X
;
Zhong FQ(仲峰泉)
;
Gu HB(顾宏斌)
;
Zhang XY(张新宇)
;
Zhong, FQ (reprint author), 15 Beisihuanxi Rd, Beijing 100190, Peoples R China.
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Submit date:2016/01/08
Supersonic Combustor
Convective Heat Transfer
Numerical Study
Wall Heat Flux
Development of efficient and accurate skeletal mechanisms for hydrocarbon fuels and kerosene surrogate
期刊论文
ACTA MECHANICA SINICA, 2015, 卷号: 31, 期号: 5, 页码: 732-740
Authors:
Zhong FQ(仲峰泉)
;
Ma SG
;
Zhang XY(张新宇)
;
Sung CJ
;
Niemeyer KE
;
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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Submit date:2016/01/08
Reduced Chemistry
Hydrocarbons
Directed Relation Graph
Ignition Delay Time
Numerical study of heat transfer deterioration of turbulent supercritical kerosene flow in heated circular tube
期刊论文
INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER, 2015, 卷号: 85, 页码: 1003-1011
Authors:
Dang GX
;
Zhong FQ(仲峰泉)
;
Zhang YJ
;
Zhang XY(张新宇)
;
Zhong, FQ (reprint author), Chinese Acad Sci, Inst Mech, Bei Si Huan Xi Rd 15, Beijing 100190, Peoples R China.
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Submit date:2015/06/12
Supercritical Kerosene
Convective Heat Transfer
Turbulent Flow
Numerical Study
Numerical analysis on the heat transfer of three types of nozzles for the hypersonic long-run wind tunnel
期刊论文
Science China-Technological Sciences, 2015, 卷号: 58, 期号: 3, 页码: 470-475
Authors:
Xing YF(邢云绯)
;
Zhong FQ(仲峰泉)
;
Li DX(李东霞)
;
Zhang XY(张新宇)
;
Zhong, FQ (reprint author), Chinese Acad Sci, Inst Mech, Natl Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
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Submit date:2015/04/28
Hypersonic Scramjet Test Tunnel
Nozzle
Aerodynamic Heating
Convective Heat Transfer
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
基于简化机理的乙烯/空气非预混燃烧过程的大涡模拟研究
会议论文
中国力学大会-2015, 中国上海, 2015-08-16
Authors:
马素刚
;
仲峰泉
;
张新宇
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Submit date:2016/08/16
预混燃烧
点火延迟时间
关系图法
大涡模拟
层流火焰
敏感度分析
敏感性分析
误差传递
超临界态煤油弯管内湍流流动与对流传热数值研究
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:
张永江
;
仲峰泉
;
邢云绯
;
张新宇
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Submit date:2016/08/16
对流传热
湍流流动
弯管
超临界态
低雷诺数流动
对应状态
入口温度
输运特性
传热恶化
二次流动
入口参数变化条件下超声速燃烧室流动与燃烧特性数值研究
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:
程柳维
;
仲峰泉
;
张新宇
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Submit date:2016/08/16
超声速燃烧
燃烧特性
特性数值
释热
湍流模型
凹腔
流动分离
总温
空气混合
模拟飞行
超临界态煤油直角弯管内湍流流动与对流传热数值研究
会议论文
中国力学大会-2015, 中国上海, 2015-08-16
Authors:
张永江
;
仲峰泉
;
邢云绯
;
张新宇
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Submit date:2016/08/16
超临界态
对流传热
湍流流动
方形管
弯管
影响特性
超临界态煤油冲击射流的数值研究
会议论文
中国力学大会-2015, 中国上海, 2015-08-16
Authors:
邢云绯
;
仲峰泉
;
张新宇
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Submit date:2016/08/16
冲击射流
超临界态
冷却结构
航空煤油
离散求解
有限体积法
Stokes
Navier
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