Selected(0)Clear
Items/Page: Sort: |
| Experimental Investigation of Abrupt Change in a Scramjet with Variable Mach-Number Flow 期刊论文 AIAA JOURNAL, 2022, 页码: 9 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)![](/image/person.jpg)
Adobe PDF(3049Kb)  |   Favorite  |  View/Download:169/28  |  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 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:164/32  |  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)![](/image/person.jpg)
Adobe PDF(5573Kb)  |   Favorite  |  View/Download:211/52  |  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
Adobe PDF(2961Kb)  |   Favorite  |  View/Download:232/44  |  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)![](/image/person.jpg)
Adobe PDF(8067Kb)  |   Favorite  |  View/Download:419/77  |  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 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)![](/image/person.jpg)
Adobe PDF(3937Kb)  |   Favorite  |  View/Download:222/58  |  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)![](/image/person.jpg)
Adobe PDF(5176Kb)  |   Favorite  |  View/Download:288/114  |  Submit date:2020/11/30 Oblique detonation wave Shock/combustion interaction Shock polar analysis High-resolution simulation |
| 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)![](/image/person.jpg)
View  |   Adobe PDF(3862Kb)  |   Favorite  |  View/Download:362/127  |  Submit date:2020/03/21 Hysteresis Dual-mode scramjet Supersonic combustion Mode transition Flame stabilization Combustion oscillation |