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Fan XueJun

Fan XueJun

E-mail:xfan@imech.ac.cn
TEL:82544052
P.C.:100190
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[1] Zhong FQ,Fan XJ,Yu G,et al. Heat Transfer Of Aviation Kerosene At Supercritical Conditions[J]. Journal Of Thermophysics And Heat Transfer,2009-01-01,23(3):543-550.
View/Download:1091/284
[2] Li XF,Huai XL,Cai J,et al. Convective Heat Transfer Characteristics Of China Rp-3 Aviation Kerosene At Supercritical Pressure[J]. Applied Thermal Engineering,2011-01-01,31(14-15):2360-2366.
View/Download:949/276
[3] Fan XJ,Yu G. Analysis Of Thermophysical Properties Of Daqing Rp-3 Aviation Kerosene[J]. Journal Of Propulsion Technology,2006-01-01,27(2):187-192.
View/Download:936/404
[4] Li L,Wang J,Fan XJ. Development Of Integrated High Temperature Sensor For Simultaneous Measurement Of Wall Heat Flux And Temperature[J]. Review Of Scientific Instruments,2012-07-01,83(7):074901.
View/Download:786/225
[5] Zhong FQ,Fan XJ,Yu G,et al. Thermal Cracking And Heat Sink Capacity Of Aviation Kerosene Under Supercritical Conditions[C]. Journal Of Thermophysics And Heat Transfer.1801 Alexander Bell Drive, Ste 500, Reston, Va 22091-4344 Usa.Amer Inst Aeronaut Astronaut.2011-01-01,450-456.
View/Download:775/195
[6] Zhong FQ,Fan XJ,Yu G,et al. Thermal Cracking Of Aviation Kerosene For Scramjet Applications[J]. Science In China Series E-technological Sciences,2009-01-01,52(9):2644-2652.
View/Download:726/122
[7] Fan XJ,Yu G,Li JG,et al. Investigation Of Vaporized Kerosene Injection And Combustion In A Supersonic Model Combustor[C]. Journal Of Propulsion And Power.2004-07-11,103-110.
View/Download:714/183
[8] Zhong FQ,Fan XJ,Yu G,et al. Thermal Cracking And Heat Sink Capacity Of Aviation Kerosene Under Supercritical Conditions[J]. Journal Of Thermophysics And Heat Transfer,2011-01-01,25(3):450-456.
View/Download:671/204
[9] Fan XJ,Zhong FQ,Yu G,et al. Catalytic Cracking And Heat Sink Capacity Of Aviation Kerosene Under Supercritical Conditions[J]. Journal Of Propulsion And Power,2009-01-01,25(6):1226-1232.
View/Download:649/144
[10] Lu Y,Li L,Fan XJ. A Thermal Analysis Method For Fuel-cooled Combustor Structure Based On Heat Flux Measurement[C]. Yang Lu,long Li,xuejun Fan. A Thermal Analysis Method For Fuel-cooled Combustor Structure Based On Heat Flux Measurement[c].2012.2012-01-01.
View/Download:635/299
[11] Fan XJ,Yu G,Li JG. Combustion And Ignition Of Thermally Cracked Kerosene In Supersonic Model Combustors[J]. Journal Of Propulsion And Power,2007-01-01,23(2):317-324.
View/Download:630/204
[12] Fan XJ,Brown GL. Probe For Measurements Of Density/conductivity In Flows Of Conducting Fluids[J]. Review Of Scientific Instruments,2006-01-01,77(4):045104.
View/Download:625/141
Total Pages:11,Current Page:1   1                    

Research Topics

超声速燃烧[16] Combustion[8] 航空煤油[8] 超临界态[7] Spacecraft[6] 主动冷却[6] Large eddy simulation[5] Supersonic combustion[4] 超燃冲压发动机[4] 碳氢燃料[4] 火焰稳定[3] Sensitivity analysis[3] Supersonic aircraft[3] 大涡模拟[3] 超声速燃烧室[3]

Research Outputs

Co-author[TOP 5]

 

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