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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
Authors:  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.
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Supercritical Kerosene  Compressible Flow  Laval Nozzle  Isentropic Process  Aviation Kerosene  Combustion  Propulsion  
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)
View  |  Adobe PDF(2023Kb)  |  Favorite  |  View/Download:557/117  |  Submit date:2014/02/24
Thermal Cracking and Heat Sink Capacity of Aviation Kerosene Under Supercritical Conditions 会议论文
AIAA/ASME/SAE/ASEE 45th Joint Propulsion Conference and Exhibit, Denver, CO, AUG 02-08, 2009
Authors:  Zhong FQ(仲峰泉);  Fan XJ(范学军);  Yu G(俞刚);  Li JG(李建国);  Sung CJ;  Zhong, FQ (reprint author), Chinese Acad Sci, Inst Mech, Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China
View  |  Adobe PDF(57Kb)  |  Favorite  |  View/Download:1162/283  |  Submit date:2012/04/01
Thermal Cracking and Heat Sink Capacity of Aviation Kerosene Under Supercritical Conditions 期刊论文
Journal of Thermophysics and Heat Transfer, 2011, 卷号: 25, 期号: 3, 页码: 450-456
Authors:  Zhong FQ(仲峰泉);  Fan XJ(范学军);  Yu G(俞刚);  Li JG(李建国);  Sung CJ;  Zhong, FQ (reprint author), Chinese Acad Sci, Inst Mech, Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China
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Tetralin  Decalin  
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
Authors:  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)  |  Favorite  |  View/Download:1302/413  |  Submit date:2012/04/01
Supercritical Pressure  Aviation Kerosene  Convective Heat Transfer  Numerical Study  Cracked Kerosene  Tubes  Water  Flows  
气动加热对主动冷却超声速燃烧室热结构的影响 会议论文
第四届高超声速科技学术会议, 中国海南三亚, 2011
Authors:  宋宏伟;  吴臣武;  仲峰泉;  孙泉华;  范学军;  樊菁
View  |  Adobe PDF(74Kb)  |  Favorite  |  View/Download:920/206  |  Submit date:2012/04/01
主动冷却  超声速燃烧  气动热  热结构  隔热  
测量热流和温度的传感器及高温下测量热流与温度的方法 专利
发明专利. 测量热流和温度的传感器及高温下测量热流与温度的方法, 专利号: ZL2009100853677, 申请日期: 2009-05-21, 授权日期: 2012-12-28
Inventors:  李龙;  范学军;  仲峰泉;  王晶
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采用简化机理模拟乙烯在超声速气流中自点火燃烧过程 会议论文
第三届高超声速科技学术会议, 江苏·无锡
Authors:  仲峰泉;  范学军;  俞刚;  张新宇
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三维冷却结构中航空煤油对流传热特性实验研究 会议论文
第三届高超声速科技学术会议, 江苏·无锡
Authors:  王永鹏;  范学军;  仲峰泉;  陆阳
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超临界压力下航空煤油水平管内对流换热特性数值研究 期刊论文
航空动力学报, 2010, 卷号: 25, 期号: 8, 页码: 1690-1697
Authors:  李勋锋;  仲峰泉;  范学军;  淮秀兰;  蔡军
Adobe PDF(1187Kb)  |  Favorite  |  View/Download:823/227  |  Submit date:2010/05/03
超临界压力  航空煤油  数值研究  浮升力  强化传热