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Thermo-fluidic characteristics and performance in a distribute heating bubble pump generator 期刊论文
INTERNATIONAL JOURNAL OF REFRIGERATION, 2022, 卷号: 133, 页码: 181-190
Authors:  Yang, Honghai;  Chen, Yuping;  Wu, Yiwei;  Yang FC(杨丰畅);  Huang, Xinyu;  Xu, Yue;  Duan, Wenli
Favorite  |  View/Download：35/0  |  Submit date：2022/02/17
Bubble pump generator  Distribute heating  Multiple lift tubes  Flow pattern evolution  Lift performance  Flow stability  
Numerical investigation on flow nonuniformity-induced hysteresis in scramjet isolator 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2020, 卷号: 33, 期号: 12, 页码: 3176-3188
Authors:  Huang TL(黄庭隆);  Yue LJ(岳连捷);  Ma SH(马生虎);  Zhang QF(张启帆);  Zhang, Peng;  Zhang XY(张新宇)
Adobe PDF(3937Kb)  |  Favorite  |  View/Download：25/1  |  Submit date：2021/03/30
Adverse pressure gradient  Back pressure  Hysteresis effects  Non-uniform flow  Shock train  
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)
View  |  Adobe PDF(3862Kb)  |  Favorite  |  View/Download：167/52  |  Submit date：2020/03/21
Hysteresis  Dual-mode scramjet  Supersonic combustion  Mode transition  Flame stabilization  Combustion oscillation  
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：84/18  |  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：130/35  |  Submit date：2018/01/16
Spacecraft  
Combustion of kerosene in a supersonic stream 会议论文
38th Aerospace Sciences Meeting and Exhibit 2000, Reno, NV, United states, January 10, 2000 - January 13, 2000
Authors:  Li JG(李建国);  Yu G(俞刚);  Zhang XY(张新宇);  Huang QS
View  |  Adobe PDF(519Kb)  |  Favorite  |  View/Download：68/34  |  Submit date：2017/06/01
Cavity Flame Holders  Combustion Efficiencies  Combustor Performance  Equivalence Ratios  Modular Structures  Optimized Conditions  Stagnation Pressures  Supersonic Combustors