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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)
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| 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)
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| 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
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| 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
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| 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 |