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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：221/55 | Submit date：2021/01/12 |
| 超燃冲压发动机加速过程中燃烧不稳定性研究 会议论文
中国力学大会, 中国浙江杭州, 2019年8月25-28日
Authors: 孟宇; 顾洪斌; 岳连捷; 张新宇
 View | Adobe PDF(1057Kb) | Favorite | View/Download：273/75 | Submit date：2019/11/21
超燃冲压发动机 不稳定性 加速过程 直连台 实验研究 |
| 航空煤油冲击射流强化传热的实验研究 会议论文
中国航天第三专业信息网第四十届技术交流会暨第四届空天动力联合会议, 中国云南昆明, 2019-08-14
Authors: 杜蒙蒙; 仲峰泉; 邢云绯; 张新宇
View | Adobe PDF(987Kb) | Favorite | View/Download：179/65 | Submit date：2020/09/28
实验研究 冲击射流 航空煤油 强化传热 |
| 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：36/17 | Submit date：2023/03/17 |
| Experimental Study of Ignition and Flame Characteristics of Surrogate of Cracked Hydrocarbon Fuels in Supersonic Crossflow 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors: Cheng LW(程柳维); Zhong FQ(仲峰泉); Wang ZP(王知溥); Gu HB(顾洪斌); Ma SG(马素刚); Zhang XY(张新宇)
View | Adobe PDF(517Kb) | Favorite | View/Download：331/108 | Submit date：2018/01/16
Combustors Cracks Diesel Engines Efficiency Ethylene Fighter Aircraft Fuels High Speed Cameras Ignition Kerosene Luminance Spacecraft Stabilization |
| 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：275/93 | 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：340/74 | Submit date：2018/01/16
Boundary Layer Flow Boundary Layers Spacecraft Wind Tunnels |
| Experimental study of combustion oscillations in a dual-mode scramjet 会议论文
20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 2015, 2015
Authors: Tian XD; Chen LH(陈立红); Gu HB(顾洪斌); Liu C; Cheng LW; Chang XY(张新宇); Chen, Lihong (lhchen@imech.ac.cn)
 Adobe PDF(824Kb) | Favorite | View/Download：244/70 | Submit date：2017/09/04 |
| Large eddy simulation of ignition and combustion of ethylene/air turbulent jet diffusion flame with reduced kinetic mechanism 会议论文
20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 2015, Glasgow, United kingdom, July 6, 2015 - July 9, 2015
Authors: Ma SG(马素刚); Zhong FQ(仲峰泉); Zhang XY(张新宇); Zhong, Fengquan (fzhong@imech.ac.cn)
Adobe PDF(496Kb) | Favorite | View/Download：260/75 | Submit date：2017/05/05
Combustion Pro Cess Directed Relation Graph Dynamic Evolution Fuel Injection Velocities Kinetic Mechanism Reduced Mechanisms Temperature Profiles Temporal And Spatial Evolutions |
| 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
Adobe PDF(624Kb) | Favorite | View/Download：248/66 | 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 |
