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| Self-similar unstart characteristics of supersonic contraction duct with an expansion corner 期刊论文 PHYSICS OF FLUIDS, 2024, 卷号: 36, 期号: 1, 页码: 20 Authors: Tong XT(仝晓通); Yue LJ(岳连捷); Wu WN(邬婉楠); Zhang QF(张启帆); Chen H(陈昊) Favorite  |  View/Download:44/0  |  Submit date:2024/03/11 |
| 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 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:163/41  |  Submit date:2022/11/28 |
| 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:156/27  |  Submit date:2022/03/22 |
| 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:223/44  |  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) Adobe PDF(8067Kb)  |  Favorite  |  View/Download:402/71  |  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) Adobe PDF(3937Kb)  |  Favorite  |  View/Download:212/53  |  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:278/113  |  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) Adobe PDF(3862Kb)  |  Favorite  |  View/Download:354/124  |  Submit date:2020/03/21 Hysteresis Dual-mode scramjet Supersonic combustion Mode transition Flame stabilization Combustion oscillation |