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| Parameters for evaluating the efficiency of inlet compression 期刊论文 CHINESE JOURNAL OF AERONAUTICS, 2021, 卷号: 34, 期号: 12, 页码: 51-56 作者: Chen KT(陈科挺); Yue LJ(岳连捷); Zhang XY(张新宇) Adobe PDF(511Kb)  |  收藏  |  浏览/下载:216/45  |  提交时间:2022/01/12 Airbreathing engine Compression efficiency Compression quality Inlet Self-consistency |
| 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 作者: 贺理浩; 张启帆; 岳连捷; 张新宇; 王卫星; 谭慧俊 Adobe PDF(9600Kb)  |  收藏  |  浏览/下载:253/37  |  提交时间: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 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:204/51  |  提交时间: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 作者: Yang L; Yue LJ(岳连捷); Zhang QF(张启帆); Zhang XY(张新宇) Adobe PDF(5176Kb)  |  收藏  |  浏览/下载:270/111  |  提交时间: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 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) 浏览  |  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 |
| Experimental study of mode transition characteristics of a cavity-based scramjet combustor during acceleration 期刊论文 Aerospace Science and Technology, 2019, 卷号: 93, 期号: 10, 页码: UNSP 105316 作者: Meng Y(孟宇); Gu HB(顾洪斌); Zhuang JH(庄金衡); Sun WM(孙文明); Gao ZB(高占彪); Lian H(连欢); Yue LJ(岳连捷); Chang XY(张新宇) 浏览  |  Adobe PDF(3099Kb)  |  收藏  |  浏览/下载:369/98  |  提交时间:2019/10/15 Scramjet Combustor Mode Transition Liquid Kerosene Acceleration |
| Numerical study of a fully confined supersonic slot impinging jet from bleed system 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 90, 页码: 12-22 作者: Huang TL(黄庭隆); Yue LJ(岳连捷); Chang XY(张新宇) 浏览  |  Adobe PDF(3918Kb)  |  收藏  |  浏览/下载:535/172  |  提交时间:2019/09/09 Fully confined supersonic jet Inclined impingement Heat transfer Boundary layer bleed Numerical simulation |
| 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 作者: 张启帆; 岳连捷; 贾轶楠; 张新宇; 李欣; 高雄 浏览  |  Adobe PDF(1675Kb)  |  收藏  |  浏览/下载:223/47  |  提交时间: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 |
| Comment on "Mechanics of Combustion Mode Transition in a Direct-Connect Ramjet-Scramjet Experiment" 期刊论文 JOURNAL OF PROPULSION AND POWER, 2018, 卷号: 34, 期号: 2, 页码: 550-551 作者: Chen KT(陈科挺); Yue LJ(岳连捷); Chang XY(张新宇) 浏览  |  Adobe PDF(148Kb)  |  收藏  |  浏览/下载:255/86  |  提交时间:2018/10/30 |
| Effect of cowl shock on restart characteristics of simple ramp type hypersonic inlets with thin boundary layers 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2018, 卷号: 74, 页码: 72-80 作者: Yue LJ(岳连捷); Jia YN(贾轶南); Xu X; Zhang XY(张新宇); Zhang P(张鹏) 浏览  |  Adobe PDF(2110Kb)  |  收藏  |  浏览/下载:374/136  |  提交时间:2018/10/30 Inlet restart Cowl shock Shock wave boundary layer interactions |