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| 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 Authors: 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)  |  Favorite  |  View/Download:256/48  |  Submit date: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 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:560/104  |  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(陈昊) Adobe PDF(1382Kb)  |  Favorite  |  View/Download:158/28  |  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:224/44  |  Submit date:2022/02/17 |
| 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:262/38  |  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:213/54  |  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:282/113  |  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) View  |  Adobe PDF(3862Kb)  |  Favorite  |  View/Download:356/125  |  Submit date:2020/03/21 Hysteresis Dual-mode scramjet Supersonic combustion Mode transition Flame stabilization Combustion oscillation |
| 真实气体效应对Ma10级进气道流动的影响 期刊论文 推进技术, 2019, 卷号: 40, 期号: 05, 页码: 1042-1050 Authors: 张启帆; 岳连捷; 贾轶楠; 张新宇; 李欣; 高雄 View  |  Adobe PDF(1675Kb)  |  Favorite  |  View/Download:242/48  |  Submit date:2019/09/12 真实气体效应 高马赫数进气道 化学非平衡气体模型 热完全气体模型 前缘钝化 再起动性能 |