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Investigation on a truncated streamline-traced hypersonic Busemann inlet 会议论文
15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Dayton, OH, United states, April 28, 2008 - May 1, 2008
Authors:  Xiao YB(肖雅彬);  Yue LJ(岳连捷);  Gong P;  Chang XY(张新宇)
View  |  Adobe PDF(3472Kb)  |  Favorite  |  View/Download：223/86  |  Submit date：2017/06/01
Boundary Layer Corrections  Busemann Inlet  Core Flow  Correction Method  Design Points  Finite Differential Methods  Internal Contraction Ratio  Internal Flows  Mass Flow  
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.
Adobe PDF(1524Kb)  |  Favorite  |  View/Download：867/241  |  Submit date：2009/08/03
Entry Conditions  Kerosene  Supersonic Combustion  Thermal Cracking  Model Combustor  Propulsion  Injection  
Research on three-dimensional scramiet inlet 会议论文
14th AIAA/AHI International Space Planes and Hypersonics Systems Technologies Conference, Canberra, Australia, November 6, 2006 - November 9, 2006
Authors:  Yue LJ(岳连捷);  Chen LH(陈立红);  Xiao YB;  Gong P;  Chang XY(张新宇)
Adobe PDF(1267Kb)  |  Favorite  |  View/Download：163/57  |  Submit date：2017/06/01
Capture Ratio  Mass Flow  Surface Oil Dot Visualization  Three-dimensional Scramjet Inlet