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| Mitigation of Shock-Induced Separation Using Square-Shaped Micro-Serrations-A Preliminary Study 期刊论文 AEROSPACE, 2024, 卷号: 11, 期号: 2, 页码: 16 Authors: Yu FY(于方游); Gao ZB(高占彪) ; Zhang QF(张启帆) ; Yue LJ(岳连捷) ; Chen H(陈昊)![](/image/person.jpg)
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| Interaction of a shock train with inherent isentropic waves in a curved isolator 期刊论文 PHYSICS OF FLUIDS, 2022, 卷号: 34, 期号: 6, 页码: 21 Authors: He LH(贺理浩) ; Chen H(陈昊) ; Yue LJ(岳连捷) ; Zhang QF(张启帆) ; Wu WN(邬婉楠)
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| 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)
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| 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)
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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)![](/image/person.jpg)
Adobe PDF(8067Kb)  |   Favorite  |  View/Download:432/84  |  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:235/62  |  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:300/116  |  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)
Adobe PDF(3862Kb)  |   Favorite  |  View/Download:375/134  |  Submit date:2020/03/21 Hysteresis Dual-mode scramjet Supersonic combustion Mode transition Flame stabilization Combustion oscillation |
| External-Compression Supersonic Inlet Free from Violent Buzz 期刊论文 AIAA JOURNAL, 2019, 卷号: 57, 期号: 6, 页码: 2513-2523 Authors: Chen H; Tan H; Liu YZ; Zhang QF(张启帆)
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