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| 基于动态分区概念的高超声速燃烧大涡模拟 期刊论文 力学学报, 2022, 卷号: 54, 期号: 04, 页码: 954-974 Authors: 姚卫; 刘杭; 张政; 肖雅彬; 岳连捷 Adobe PDF(1875Kb)  |  Favorite  |  View/Download:301/71  |  Submit date:2022/06/10 高超声速燃烧 动态分区火焰面 分区自适应化学 分区并行自适应建表 改进延迟分离涡模拟 |
| Performance analysis of a strut-aided hypersonic scramjet by full-scale IDDES modeling 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 117, 页码: 14 Authors: Yao W(姚卫); Liu H(刘杭); Yue LJ(岳连捷); Xiao YB(肖雅彬) Adobe PDF(2954Kb)  |  Favorite  |  View/Download:291/67  |  Submit date:2021/11/15 Hypersonic combustion Hydrogen Improved Delayed Detached Eddy Simulation (IDDES) Dynamic zone flamelet model Scramjet |
| Iso-contraction-ratio methodology for the design of hypersonic inward turning inlets with shape transition 会议论文 18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference 2012, Tours, France, SEP 24-28, 2012 Authors: Xiao YB(肖雅彬); Yue LJ(岳连捷); Chen LH(陈立红); Zhang XY(张新宇); Xiao YB(肖雅彬) View  |  Adobe PDF(1674Kb)  |  Favorite  |  View/Download:458/120  |  Submit date:2014/02/24 |
| 优化NURBS内转式进气道设计与流场研究 会议论文 LHD2011夏季学术研讨会, 内蒙赤峰, 2011 Authors: 肖雅彬; 岳连捷; 陈立红; 张新宇 Adobe PDF(1354Kb)  |  Favorite  |  View/Download:585/215  |  Submit date:2014/01/23 高超声速 进气道 内转式 边界层抽吸 |
| 侧壁后切二元高超声速进气道性能研究 会议论文 LHD2011夏季学术研讨会, 内蒙赤峰, 2011 Authors: 张晓嘉; 岳连捷; 肖雅彬; 陈立红; 张新宇 Adobe PDF(703Kb)  |  Favorite  |  View/Download:493/165  |  Submit date:2014/01/23 二元高超进气道 侧壁后切 不起动 再起动(自起动) 反压 超燃冲压发动机 |
| 超燃冲压发动机三维变截面尾喷管设计 会议论文 第三届高超声速科技学术会议, 江苏·无锡 Authors: 卢鑫; 岳连捷; 肖雅彬; 张新宇 Adobe PDF(356Kb)  |  Favorite  |  View/Download:569/165  |  Submit date:2010/11/25 |
| 高超声速流线追踪进气道基准流场设计 会议论文 第二届高超声速科技学术会议, 中国安徽黄山, 2009-11-02 Authors: 岳连捷; 肖雅彬; 陈立红; 张新宇 Adobe PDF(734Kb)  |  Favorite  |  View/Download:765/248  |  Submit date:2010/11/25 高超声速 流线追踪进气道 基准流场 |
| 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:867/179  |  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:220/85  |  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 |
| 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:257/77  |  Submit date:2015/09/21 |