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Numerical investigation of mode transition and hysteresis in a cavity-based dual-mode scramjet combustor 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 94, 页码: 10
Authors:  Zhang X(张旭);  Yue LJ(岳连捷);  Huang TL(黄庭隆);  Zhang QF(张启帆);  Zhang XY(张新宇)
Favorite  |  View/Download:3/0  |  Submit date:2020/03/21
Hysteresis  Dual-mode scramjet  Supersonic combustion  Mode transition  Flame stabilization  Combustion oscillation  
Numerical study of a fully confined supersonic slot impinging jet from bleed system 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 90, 页码: 12-22
Authors:  Huang TL(黄庭隆);  Yue LJ(岳连捷);  Chang XY(张新宇)
View  |  Adobe PDF(3918Kb)  |  Favorite  |  View/Download:30/3  |  Submit date:2019/09/09
Fully confined supersonic jet  Inclined impingement  Heat transfer  Boundary layer bleed  Numerical simulation  
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
View  |  Adobe PDF(1908Kb)  |  Favorite  |  View/Download:20/5  |  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  
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:74/21  |  Submit date:2018/01/16
Spacecraft  
单向出口的欠膨胀超声速冲击射流换热特性研究 会议论文
第九届全国流体力学学术会议, 中国江苏南京, 2016-10-20
Authors:  黄庭隆;  岳连捷;  张新宇
View  |  Adobe PDF(122Kb)  |  Favorite  |  View/Download:82/16  |  Submit date:2017/09/27
超声速冲击射流  封闭室  气动换热  数值模拟