IMECH-IR
(本次检索基于用户作品认领结果)

浏览/检索结果: 共3条,第1-3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:951/295  |  提交时间:2013/01/18
Supercritical Kerosene  Compressible Flow  Laval Nozzle  Isentropic Process  Aviation Kerosene  Combustion  Propulsion  
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:1886/705  |  提交时间:2009/08/03
Cracked Kerosene  Rocket Fuels  Combustion  Propulsion  
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:841/229  |  提交时间:2009/08/03
Entry Conditions  Kerosene  Supersonic Combustion  Thermal Cracking  Model Combustor  Propulsion  Injection