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三面压缩式高超声速进气道流动结构研究 期刊论文
实验流体力学, 2008, 卷号: 22, 期号: 2, 页码: 64-67
Authors:  肖雅彬;  岳连捷;  龚鹏;  王世芬;  陈立红;  张新宇
Adobe PDF(413Kb)  |  Favorite  |  View/Download：875/181  |  Submit date：2010/05/03
超声速进气道  流动结构  油滴显示  数值模拟  
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：224/86  |  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  
侧压式超燃进气道流场特性研究 期刊论文
力学与实践, 2007, 卷号: 29, 期号: 3, 页码: 7-10
Authors:  向安宇;  岳连捷;  肖雅彬;  王世芬;  陈立红;  张新宇
Adobe PDF(390Kb)  |  Favorite  |  View/Download：614/141  |  Submit date：2010/05/03
超燃冲压发动机  侧压式进气道  流场显示  
Research on three-dimensional scramjet inlet 会议论文
14th AIAA/AHI Space Planes and Hypersonic Systems and Technologies Conference, 2006, Beijing, China, 20-23 April 2006
Authors:  Yue LJ(岳连捷);  Xiao YB(肖雅彬);  Chen LH(陈立红);  Xiang AY(向安宇);  Zhang XY(张新宇)
View  |  Adobe PDF(1265Kb)  |  Favorite  |  View/Download：263/80  |  Submit date：2015/09/21