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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：235/62 | 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：38/18 | Submit date：2023/03/17 |
| 反压引起的带尖楔矩形隔离段流动分离迟滞现象实验研究 会议论文
中国航天第三专业信息网第三十八届技术交流会暨第二届空天动力联合会议, 中国辽宁大连, 2017-08-23
Authors: 黄庭隆; 岳连捷; 张新宇
Adobe PDF(1908Kb) | Favorite | View/Download：204/62 | Submit date：2018/12/12
隔离段 反压 尖楔 分离区 流动分离 边界层分离 迟滞现象 激波串 纹影图像 |
| 关于Fotia隔离段流动突变理论分析的看法 会议论文
中国航天第三专业信息网第三十八届技术交流会暨第二届空天动力联合会议, 中国辽宁大连, 2017-08-23
Authors: 陈科挺; 岳连捷; 张新宇
 View |  Adobe PDF(623Kb) | Favorite | View/Download：383/62 | Submit date：2018/12/12
隔离段 流动模型 出口 对外贸易 Fotia 核心流 |
| 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：289/99 | 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：349/77 | Submit date：2018/01/16
Boundary Layer Flow Boundary Layers Spacecraft Wind Tunnels |
| Role of wall temperature on shock train in a rectangular isolator 会议论文
52nd AIAA/SAE/ASEE Joint Propulsion Conference, 2016, Salt Lake City, UT, United states, July 25, 2016 - July 27, 2016
Authors: Lu HB; Wang D; Chen X; Yue LJ(岳连捷); Ji, Feng (yuelj@imech.ac.cn)
View | Adobe PDF(560Kb) | Favorite | View/Download：289/99 | Submit date：2017/05/05
Aero Heating Dual Mechanisms On Flow Shock Train Specific Heat Ratio Total Pressure Total Temperatures Wall Temperatures |
| 带有边界层流动控制的内转式进气道 会议论文
第八届全国高超声速科技学术会议, 中国黑龙江哈尔滨, 2015-12-28
Authors: 肖雅彬; 岳连捷; 张新宇
View | Adobe PDF(624Kb) | Favorite | View/Download：259/71 | Submit date：2016/08/16
流场品质 隔离段 边界层流动 流向涡 斜激波 横向流动 唇口 压力梯度 收缩段 边界层控制 |
| 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：477/127 | Submit date：2014/02/24 |
| 局部收缩比处处一致的变截面高超声速内转式进气道设计方法 会议论文
LHD2012夏季学术研讨会, 吉林延吉, 2012
Authors: 肖雅彬; 岳连捷; 高占彪; 陈立红; 张新宇
Adobe PDF(2046Kb) | Favorite | View/Download：588/233 | Submit date：2014/01/23 |
