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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 作者: Tong XT(仝晓通); Yue LJ(岳连捷); Wu WN(邬婉楠); Zhang QF(张启帆); Chen H(陈昊) 收藏  |  浏览/下载:37/0  |  提交时间: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 作者: 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)  |  收藏  |  浏览/下载:152/38  |  提交时间:2022/11/28 |
| 高马赫数燃烧强化的激波风洞试验研究 期刊论文 力学学报, 2022, 卷号: 54, 期号: 05, 页码: 1403-1413 作者: 张旭; 张启帆; 岳连捷; 孟东东; 罗苇航; 于江鹏; 张晓源; 李进平; 陈宏; 李飞 Adobe PDF(3069Kb)  |  收藏  |  浏览/下载:244/43  |  提交时间:2022/08/11 高马赫数 超声速燃烧 燃烧强化 小支板 JF-24激波风洞 |
| 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 作者: 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)  |  收藏  |  浏览/下载:544/99  |  提交时间: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 作者: 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)  |  收藏  |  浏览/下载:154/27  |  提交时间: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 作者: Huang TL(黄庭隆); Zhang QF(张启帆); Yue LJ(岳连捷); Zhang P; Zhao QJ Adobe PDF(2961Kb)  |  收藏  |  浏览/下载:216/44  |  提交时间: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 作者: Tong XT(仝晓通); Zhang QF(张启帆); Yue LJ(岳连捷); Zhang XY(张新宇) Adobe PDF(8067Kb)  |  收藏  |  浏览/下载:392/67  |  提交时间: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 作者: 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)  |  收藏  |  浏览/下载:203/51  |  提交时间:2021/03/30 Adverse pressure gradient Back pressure Hysteresis effects Non-uniform flow Shock train |
| High-order simulation solving Navier-Stokes equations with Spalart–Allmaras turbulence model 会议论文 4th International Conference on Fluid Mechanics and Industrial Applications, FMIA 2020,, Asian Union of Information Technology, June 27, 2020 - June 28, 2020 作者: Yang L; 岳连捷; 张启帆; 张新宇 Adobe PDF(1289Kb)  |  收藏  |  浏览/下载:212/51  |  提交时间:2021/01/12 |
| 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 作者: 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)  |  收藏  |  浏览/下载:344/121  |  提交时间:2020/03/21 Hysteresis Dual-mode scramjet Supersonic combustion Mode transition Flame stabilization Combustion oscillation |