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Study on heat transfer coupling mechanism of direct thermoelectric conversion with regenerative cooling for supersonic combustor applications 期刊论文
APPLIED THERMAL ENGINEERING, 2024, 卷号: 238, 页码: 15
作者:  Gao EK(高尔康);  Zhong FQ(仲峰泉)
收藏  |  浏览/下载：28/0  |  提交时间：2024/02/26
Direct thermoelectric conversion  Regenerative cooling  Supersonic combustor  Analytical model  Genetic algorithm  
CH* Luminance Distribution Application and a One-Dimensional Model of the Supersonic Combustor Heat Release Quantization 期刊论文
INTERNATIONAL JOURNAL OF TURBO & JET-ENGINES, 2019, 卷号: 36, 期号: 1, 页码: 45-50
作者:  Wang ZP(王知溥);  Gu HB(顾洪斌);  Cheng L W;  Zhong FQ(仲峰泉);  Zhang XY(张新宇)
浏览  |  Adobe PDF(2630Kb)  |  收藏  |  浏览/下载：251/76  |  提交时间：2019/04/11
supersonic combustion  one-dimensional modelling  heat release  CH* chemiluminescence  
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
作者:  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.
浏览  |  Adobe PDF(1162Kb)  |  收藏  |  浏览/下载：329/81  |  提交时间：2016/09/14
Dual-mode Scramjet  Engine Performance  Thrust  Optimization  Heat Release Distribution  Simulated Annealing Algorithm  
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.
浏览  |  Adobe PDF(1318Kb)  |  收藏  |  浏览/下载：289/91  |  提交时间：2016/01/08
Reduced Chemistry  Hydrocarbons  Directed Relation Graph  Ignition Delay Time  
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
作者:  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.
Adobe PDF(1454Kb)  |  收藏  |  浏览/下载：1414/482  |  提交时间：2013/05/03
Ethylene  Ignition  Numerical Simulation  Reduced Kinetic Mechanism  Supersonic Combustion  
Characteristics of compressible flow of supercritical kerosene 期刊论文
ACTA MECHANICA SINICA, 2012, 卷号: 28, 期号: 1, 页码: 8-13
作者:  Zhong FQ(仲峰泉);  Fan XJ(范学军);  Wang J(王晶);  Yu G(俞刚);  Li JG(李建国);  Fan, XJ;  Chinese Acad Sci, Inst Mech, LHD, Beijing 100190, Peoples R China.
Adobe PDF(484Kb)  |  收藏  |  浏览/下载：961/299  |  提交时间：2013/01/18
Supercritical Kerosene  Compressible Flow  Laval Nozzle  Isentropic Process  Aviation Kerosene  Combustion  Propulsion  
Convective heat transfer characteristics of China RP-3 aviation kerosene at supercritical pressure 期刊论文
Applied Thermal Engineering, 2011, 卷号: 31, 期号: 14-15, 页码: 2360-2366
作者:  Li XF;  Huai XL;  Cai J;  Zhong FQ(仲峰泉);  Fan XJ(范学军);  Guo ZX;  Huai, XL (reprint author), Chinese Acad Sci, Inst Engn Thermophys, Beijing 100190, Peoples R China
Adobe PDF(289Kb)  |  收藏  |  浏览/下载：1285/406  |  提交时间：2012/04/01
Supercritical Pressure  Aviation Kerosene  Convective Heat Transfer  Numerical Study  Cracked Kerosene  Tubes  Water  Flows  
Performance of supersonic model combustors with staged injections of supercritical aviation kerosene 期刊论文
Acta Mechanica Sinica, 2010, 卷号: 26, 期号: 5, 页码: 661-668
作者:  Zhong FQ(仲峰泉);  Fan XJ(范学军);  Yu G(俞刚);  Li JG(李建国);  Sung CJ;  Zhong FQ
Adobe PDF(680Kb)  |  收藏  |  浏览/下载：860/193  |  提交时间：2011/03/01
Supersonic Combustion  Staged Injection  Combustion Efficiency  Supercritical Kerosene  
Catalytic Cracking and Heat Sink Capacity of Aviation Kerosene Under Supercritical Conditions 期刊论文
Journal of Propulsion and Power, 2009, 卷号: 25, 期号: 6, 页码: 1226-1232
作者:  Fan XJ(范学军);  Zhong FQ(仲峰泉);  Yu G(俞刚);  Li JG(李建国);  Sun CJ;  Fan XJ
Adobe PDF(2295Kb)  |  收藏  |  浏览/下载：1065/335  |  提交时间：2009/08/03
Fueled Supersonic Combustor  Model Combustor  Injection  
Heat Transfer of Aviation Kerosene at Supercritical Conditions 期刊论文
Journal of Thermophysics and Heat Transfer, 2009, 卷号: 23, 期号: 3, 页码: 543-550
作者:  Zhong FQ(仲峰泉);  Fan XJ(范学军);  Yu G(俞刚);  Li JG(李建国);  Sung CJ;  Zhong FQ
Adobe PDF(674Kb)  |  收藏  |  浏览/下载：1895/708  |  提交时间：2009/08/03
Cracked Kerosene  Rocket Fuels  Combustion  Propulsion