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| High-order simulation solving Navier-Stokes equations with Spalart–Allmaras turbulence model 会议论文
4th International Conference on Fluid Mechanics and Industrial Applications, FMIA 2020,, Asian Union of Information Technology, June 27, 2020 - June 28, 2020
Authors: Yang L; 岳连捷 ; 张启帆; 张新宇
 Adobe PDF(1289Kb) |  Favorite | View/Download：215/53 | Submit date：2021/01/12 |
| Numerical Study of Heat Transfer on Confined Under-Expanded Impinging Jet from Slot into a Plenum 会议论文
31st International Symposium on Shock Waves, Nagoya, Japan, 2017-07-9~14
Authors: Huang TL(黄庭隆); Yue LJ(岳连捷); Zhang XY(张新宇)
Adobe PDF(714Kb) | Favorite | View/Download：35/16 | Submit date：2023/03/17 |
| Downstream pressure variation induced hysteresis in the scramjet isolator 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors: Huang TL(黄庭隆); Yue LJ(岳连捷); Ma SH; Jia YN(贾轶南); Zhang XY(张新宇); Yue, Lianjie(yuelj@imech.ac.cn)
 View | Adobe PDF(704Kb) | Favorite | View/Download：272/93 | Submit date：2018/01/16
Spacecraft |
| The Phenomena of Sudden Change in Hypersonic Inlets Self-Starting Capability 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors: Jia YN(贾轶南); Yue LJ(岳连捷); Zhang XY(张新宇); Jia, Yinan(yuelj@imech.ac.cn)
View | Adobe PDF(566Kb) | Favorite | View/Download：337/74 | Submit date：2018/01/16
Boundary Layer Flow Boundary Layers Spacecraft Wind Tunnels |
| 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：449/117 | Submit date：2014/02/24 |
| 高超声速二元进气道循环气流边界层控制方法研究 会议论文
LHD2011夏季学术研讨会, 内蒙赤峰, 2011
Authors: 岳连捷; 叶青; 张晓嘉; 陈立红; 张新宇
Adobe PDF(837Kb) | Favorite | View/Download：443/211 | Submit date：2014/01/23
高超声速进气道 边界层分离 流动控制 循环气流控制 |
| 三面压缩高超进气道附面层抽吸研究 会议论文
第三届高超声速科技学术会议, 江苏·无锡
Authors: 岳连捷; 徐显坤; 叶青; 王世芬; 陈立红; 张新宇
Adobe PDF(2153Kb) | Favorite | View/Download：627/165 | Submit date：2010/11/25 |
| 总压特性及边界层抽吸对超燃冲压发动机推力的影响 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: 徐显坤; 岳连捷; 张新宇
Adobe PDF(830Kb) | Favorite | View/Download：607/152 | Submit date：2010/11/25
总压恢复 边界层抽吸 发动机推力 |
| 溢流槽道位置对二元高超声速进气道性能研究 会议论文
第二届高超声速科技学术会议, 安徽·黄山
Authors: 张晓嘉; 岳连捷; 陈立红; 张新宇
Adobe PDF(5127Kb) | Favorite | View/Download：494/126 | Submit date：2010/11/25 |
| 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：251/75 | Submit date：2015/09/21 |
