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Blowout limits of supercritical kerosene in supersonic combustors 会议论文
49th AIAA/ASME/SAE/ASEE Joint PropulsionConference, San Jose, CA, United states, JUL 14-17, 2013
Authors:  Zhang TC(张泰昌);  Wang J(王晶);  Yuan YM(袁越明);  Li JG(李建国);  Yu G(俞刚);  Fan XJ(范学军);  Zhang TC(张泰昌)
View  |  Adobe PDF(619Kb)  |  Favorite  |  View/Download:627/209  |  Submit date:2014/02/24
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  
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:1198/291  |  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  
Pulsed combustion of hydrocarbon fuels in a supersonic model combustor 会议论文
47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2011, San Diego, CA, United states, JUL 31-AUG 03, 2011
Authors:  Zhang TC(张泰昌);  Fan XJ(范学军);  Wang J(王晶);  Li JG(李建国);  Yu G(俞刚);  Zhang TC(张泰昌)
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Measurements of the blowout limits of supercritical aviation kerosene in a supersonic combustor 会议论文
47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 2011, San Diego, CA, United states, JUL 31-AUG 03, 2011
Authors:  Wang J(王晶);  Fan XJ(范学军);  Zhang TC(张泰昌);  Yu G(俞刚);  Li JG(李建国);  Wang J(王晶)
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Effects of entry conditions on cracked kerosene-fueled supersonic combustor performance 期刊论文
Combustion Science and Technology, 2007, 卷号: 179, 期号: 10, 页码: 2199-2217
Authors:  Fan XJ(范学军);  Yu G(俞刚);  Li JG(李建国);  Yue LJ(岳连捷);  Zhang XY(张新宇);  Sung CJ;  Fan, XJ (reprint author), Chinese Acad Sci, Inst Mech, Beijing 100080, Peoples R China.
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Entry Conditions  Kerosene  Supersonic Combustion  Thermal Cracking  Model Combustor  Propulsion  Injection  
Performance of supersonic model combustors with distributed injection of supercritical kerosene 会议论文
43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Cincinnati, OH, United states, July 8, 2007 - July 11, 2007
Authors:  Fan XJ(范学军);  Yu G(俞刚);  Li JG(李建国);  Lu XN;  Sung CJ
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Stagnation Temperatures  Supercritical Kerosene  Supersonic Model Combustors  
Flow rate analyses and calibrations of kerosene cracking for supersonic combustion 会议论文
41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Tucson, AZ, United states, July 10, 2005 - July 13, 2005
Authors:  Fan XJ(范学军);  Yu G(俞刚);  Li JG(李建国)
View  |  Adobe PDF(315Kb)  |  Favorite  |  View/Download:270/74  |  Submit date:2017/06/01
Average Molecular Weight  Chemical Formulae  Cracking Model  Gaseous Products  High Temperature  Ideal Gas Law  Ideal Gas Mixtures  Mass Flow Rate  Mole Fraction  Residence Time  Room Temperature  Sonic Nozzle  Supercritical Condition  Supersonic Combustion  Temperature Dependencies  Thermal Cracking  Three-component  
Combustion of kerosene in a supersonic stream 会议论文
38th Aerospace Sciences Meeting and Exhibit 2000, Reno, NV, United states, January 10, 2000 - January 13, 2000
Authors:  Li JG(李建国);  Yu G(俞刚);  Zhang XY(张新宇);  Huang QS
View  |  Adobe PDF(519Kb)  |  Favorite  |  View/Download:209/110  |  Submit date:2017/06/01
Cavity Flame Holders  Combustion Efficiencies  Combustor Performance  Equivalence Ratios  Modular Structures  Optimized Conditions  Stagnation Pressures  Supersonic Combustors