IMECH-IR
(本次检索基于用户作品认领结果)

浏览/检索结果: 共6条,第1-6条 帮助

限定条件            
已选(0)清除 条数/页:   排序方式:
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:957/297  |  提交时间:2013/01/18
Supercritical Kerosene  Compressible Flow  Laval Nozzle  Isentropic Process  Aviation Kerosene  Combustion  Propulsion  
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:858/192  |  提交时间:2011/03/01
Supersonic Combustion  Staged Injection  Combustion Efficiency  Supercritical Kerosene  
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:1893/708  |  提交时间:2009/08/03
Cracked Kerosene  Rocket Fuels  Combustion  Propulsion  
Thermal cracking of aviation kerosene for scramjet applications 期刊论文
Science in China Series E-Technological Sciences, 2009, 卷号: 52, 期号: 9, 页码: 2644-2652
作者:  Zhong FQ(仲峰泉);  Fan XJ(范学军);  Yu G(俞刚);  Li JG(李建国);  Fan XJ
Adobe PDF(722Kb)  |  收藏  |  浏览/下载:1169/246  |  提交时间:2009/08/03
Thermal Cracking  Aviation Kerosene  Lumped Model  Scramjet Applications  Combustion  Dodecane  
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
作者:  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.
Adobe PDF(1524Kb)  |  收藏  |  浏览/下载:843/230  |  提交时间:2009/08/03
Entry Conditions  Kerosene  Supersonic Combustion  Thermal Cracking  Model Combustor  Propulsion  Injection  
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
作者:  Fan XJ(范学军);  Yu G(俞刚);  Li JG(李建国)
Adobe PDF(315Kb)  |  收藏  |  浏览/下载:229/60  |  提交时间: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