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Jet-Driven Unstart Process of a Hypersonic Inlet with Ramp Mass Injection 期刊论文
AIAA JOURNAL, 2022, 页码: 5
Authors:  Li JJ(李江江);  Chen H(陈豪);  Tong XT(仝晓通);  Gao X;  Zhang QF(张启帆);  Yue LJ(岳连捷)
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Fuel Regulation Historical Effects on Flame Stabilizations in a Cavity-Based Scramjet Combustor (Feb,& nbsp;10.2514/1.J061306, 2022)

期刊论文

AIAA JOURNAL, 2022, 页码: 1
Authors:  Zhang X(张旭);  Zhang QF(张启帆);  Wu WJ(吴文杰);  Yue LJ(岳连捷);  Gao ZB(高占彪);  Luo WH(罗苇航);  Chen H(陈豪)
Favorite  |  View/Download:2/0  |  Submit date:2022/06/11
高马赫数超燃冲压发动机技术研究进展 期刊论文
力学学报, 2022, 卷号: 54, 期号: 02, 页码: 263-288
Authors:  岳连捷;  张旭;  张启帆;  陈科挺;  李进平;  陈昊;  姚卫;  仲峰泉;  李飞;  王春;  陈宏
Adobe PDF(2622Kb)  |  Favorite  |  View/Download:70/18  |  Submit date:2022/03/16
高马赫数  超燃冲压发动机  热化学非平衡  超声速燃烧  低雷诺数流动  激波风洞  飞行试验  
Fuel Regulation Historical Effects on Flame Stabilizations in a Cavity-Based Scramjet Combustor 期刊论文
AIAA JOURNAL, 2022, 页码: 7
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(陈豪)
Favorite  |  View/Download:34/0  |  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, Lianjie;  Zhang, Qifan
Favorite  |  View/Download:29/0  |  Submit date:2022/03/05
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
Authors:  Huang TL(黄庭隆);  Zhang QF(张启帆);  Yue LJ(岳连捷);  Zhang P;  Zhao QJ
Favorite  |  View/Download:24/0  |  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
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:175/8  |  Submit date:2021/03/03
Unsteady pressure measurement  Pressure sensor  Pressure transmission tube  Dynamic response  Compressible flow  
高速进气道低马赫数不起动特性及马赫数影响规律 期刊论文
推进技术, 2020, 卷号: 42, 期号: 10, 页码: 2207-2217
Authors:  贺理浩;  张启帆;  岳连捷;  张新宇;  王卫星;  谭慧俊
Adobe PDF(9600Kb)  |  Favorite  |  View/Download:33/1  |  Submit date:2021/11/12
高速进气道  低马赫数不起动  非定常  气动力  自起动  
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 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
Authors:  Yang L;  Yue LJ(岳连捷);  Zhang QF(张启帆);  Zhang XY(张新宇)
Adobe PDF(5176Kb)  |  Favorite  |  View/Download:58/19  |  Submit date:2020/11/30
Oblique detonation wave  Shock/combustion interaction  Shock polar analysis  High-resolution simulation