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可变几何轴对称进气道初步设计 期刊论文
燃气轮机技术, 2008, 期号: 3, 页码: 21-24+28
Authors:  张辉;  伊卫林;  岳连捷;  季路成
Adobe PDF(606Kb)  |  Favorite  |  View/Download:648/202  |  Submit date:2010/05/03
轴对称进气道  变几何结构  超声速段  吸气  一维优化设计  
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:881/184  |  Submit date:2010/05/03
超声速进气道  流动结构  油滴显示  数值模拟  
带中心支板侧压进气道流场特性研究 期刊论文
实验流体力学, 2008, 卷号: 22, 期号: 1, 页码: 31-35
Authors:  龚鹏;  岳连捷;  肖雅斌;  王世芬;  张新宇
Adobe PDF(621Kb)  |  Favorite  |  View/Download:493/123  |  Submit date:2010/05/03
超燃冲压发动机  高超声速进气道  侧压式进气道  支板  
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:228/87  |  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