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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
作者:  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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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
作者:  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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Reduced Chemistry  Hydrocarbons  Directed Relation Graph  Ignition Delay Time  
Identification of the Conformational transition pathway in PIP2 Opening Kir Channels 期刊论文
SCIENTIFIC REPORTS, 2015, 卷号: 5, 页码: 11289
作者:  Li JW;  Lv SQ(吕守芹);  Liu YZ;  Pang CL;  Chen YF;  Zhang SH;  Yu H;  Long M(龙勉);  Zhang HL;  Logothetis DE;  Zhan Y;  An HL;  An, HL (reprint author), Hebei Univ Technol, Inst Biophys, Sch Sci, Key Lab Mol Biophys, Tianjin 300401, Hebei Province, Peoples R China.
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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
作者:  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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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
作者:  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.
浏览  |  Adobe PDF(860Kb)  |  收藏  |  浏览/下载:441/189  |  提交时间:2015/04/28
Hypersonic Scramjet Test Tunnel  Nozzle  Aerodynamic Heating  Convective Heat Transfer  
A biopolymer-like metal enabled hybrid material with exceptional mechanical prowess 期刊论文
Scientific Reports, 2015, 卷号: 5, 页码: 8357
作者:  Zhang JS;  Cui LS;  Jiang DQ;  Liu YN;  Hao SJ;  Ren Y;  Han XD;  Liu ZY;  Wang YZ;  Yu C;  Huan Y(郇勇);  Zhao XQ;  Zheng YJ;  Xu HB;  Ren XB;  Li XD;  Cui, LS (reprint author), China Univ Petr, State Key Lab Heavy Oil Proc, Beijing 102249, Peoples R China.
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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
作者:  Ma SG(马素刚);  Zhong FQ(仲峰泉);  Zhang XY(张新宇);  Zhong, Fengquan (fzhong@imech.ac.cn)
浏览  |  Adobe PDF(496Kb)  |  收藏  |  浏览/下载:247/74  |  提交时间: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
作者:  马素刚;  仲峰泉;  张新宇
浏览  |  Adobe PDF(243Kb)  |  收藏  |  浏览/下载:213/64  |  提交时间: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
作者:  张永江;  仲峰泉;  邢云绯;  张新宇
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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
作者:  程柳维;  仲峰泉;  张新宇
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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