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Similarity Analysis on Two-Dimensional Hypersonic Inlets Unstart 期刊论文
AIAA JOURNAL, 2023, 卷号: 61, 期号: 2, 页码: 555-572./通讯作者:Yue, Lian-jie
Authors:  Tong XT(仝晓通);  Yue LJ(岳连捷);  Chen H(陈昊);  Zhang QF(张启帆);  He CM(何成明)
Adobe PDF(6058Kb)  |  Favorite  |  View/Download:270/95  |  Submit date:2022/11/28
Numerical study on wave configuration of wedge-induced oblique detonation wave: Reactive boundary layer effect 期刊论文
PHYSICS OF FLUIDS, 2022, 卷号: 34, 期号: 11, 页码: 11./通讯作者:Yue, Lianjie
Authors:  Yang L(杨理);  Yue LJ(岳连捷);  Yu, Dehai;  Chen, Zheng
Adobe PDF(4548Kb)  |  Favorite  |  View/Download:273/81  |  Submit date:2022/12/29
Experimental Investigation of Abrupt Change in a Scramjet with Variable Mach-Number Flow 期刊论文
AIAA JOURNAL, 2022, 页码: 9./通讯作者:Zhang, Qifan
Authors:  Wu ZJ(吴振杰);  Zhang QF(张启帆);  Zhang X(张旭);  Luo WH(罗苇航);  Gao ZB(高占彪);  Yue LJ(岳连捷)
Adobe PDF(3049Kb)  |  Favorite  |  View/Download:225/70  |  Submit date:2022/07/18
Fuel Regulation Historical Effects on Flame Stabilizations in a Cavity-Based Scramjet Combustor 期刊论文
AIAA JOURNAL, 2022, 页码: 7./通讯作者:Zhang, Qifan, Yue LJ
Authors:  Zhang X(张旭);  Zhang QF(张启帆);  Wu ZJ(吴振杰);  Yue LJ(岳连捷);  Gao ZB(高占彪);  Luo WH(罗苇航);  Chen H(陈昊)
Adobe PDF(1382Kb)  |  Favorite  |  View/Download:235/82  |  Submit date:2022/03/22
Onset of Oblique Detonation Waves for a Cavity-Based Wedge 期刊论文
AIAA JOURNAL, 2022, 页码: 14
Authors:  Yang, Li;  Yue LJ(岳连捷);  Zhang QF(张启帆)
Adobe PDF(5573Kb)  |  Favorite  |  View/Download:270/69  |  Submit date:2022/03/05
Parameters for evaluating the efficiency of inlet compression 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2021, 卷号: 34, 期号: 12, 页码: 51-56./通讯作者:Yue, Lianjie
Authors:  Chen KT(陈科挺);  Yue LJ(岳连捷);  Zhang XY(张新宇)
Adobe PDF(511Kb)  |  Favorite  |  View/Download:338/78  |  Submit date:2022/01/12
Airbreathing engine  Compression efficiency  Compression quality  Inlet  Self-consistency  
Hysteresis of Shock Train Movement in the Isolator with a Ramp 期刊论文
AIAA JOURNAL, 2021, 卷号: 59, 期号: 10, 页码: 3873-3882./通讯作者:Yue, Lianjie
Authors:  Huang TL(黄庭隆);  Zhang QF(张启帆);  Yue LJ(岳连捷);  Zhang P;  Zhao QJ
Adobe PDF(2961Kb)  |  Favorite  |  View/Download:312/71  |  Submit date:2022/02/17
Flow structure of pressure transmission tube and its influence on unsteady pressure measuring results in compressible flow 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 108, 页码: 22./通讯作者:Zhang, Qifan
Authors:  Tong XT(仝晓通);  Zhang QF(张启帆);  Yue LJ(岳连捷);  Zhang XY(张新宇)
Adobe PDF(8067Kb)  |  Favorite  |  View/Download:498/105  |  Submit date:2021/03/03
Unsteady pressure measurement  Pressure sensor  Pressure transmission tube  Dynamic response  Compressible flow  
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./通讯作者:Yue, Lianjie
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:329/111  |  Submit date:2021/03/30
Adverse pressure gradient  Back pressure  Hysteresis effects  Non-uniform flow  Shock train  
Numerical study on the shock/combustion interaction of oblique detonation waves 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 104, 页码: 13./通讯作者:Yue, Lianjie
Authors:  Yang L;  Yue LJ(岳连捷);  Zhang QF(张启帆);  Zhang XY(张新宇)
Adobe PDF(5176Kb)  |  Favorite  |  View/Download:419/168  |  Submit date:2020/11/30
Oblique detonation wave  Shock/combustion interaction  Shock polar analysis  High-resolution simulation  
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