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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 Authors: Chen KT(陈科挺); Yue LJ(岳连捷) ; Zhang XY(张新宇)![](/image/person.jpg)
Adobe PDF(511Kb)  |   Favorite  |  View/Download:242/54  |  Submit date:2022/01/12 Airbreathing engine Compression efficiency Compression quality Inlet Self-consistency |
| 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:429/83  |  Submit date:2021/03/03 Unsteady pressure measurement Pressure sensor Pressure transmission tube Dynamic response Compressible flow |
| 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:284/44  |  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)![](/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:299/116  |  Submit date:2020/11/30 Oblique detonation wave Shock/combustion interaction Shock polar analysis High-resolution simulation |
| 斜爆轰波的波角和法向速度-曲率关系初步探究 期刊论文 航空学报, 2020, 卷号: 41, 页码: 123701 Authors: 杨理; 岳连捷 ; 张新宇![](/image/person.jpg)
Adobe PDF(5656Kb)  |   Favorite  |  View/Download:201/62  |  Submit date:2021/01/29 |
| 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)
View  |   Adobe PDF(3862Kb)  |   Favorite  |  View/Download:372/133  |  Submit date:2020/03/21 Hysteresis Dual-mode scramjet Supersonic combustion Mode transition Flame stabilization Combustion oscillation |
| 内压缩波系对高超声速进气道自起动性能影响研究 期刊论文 实验流体力学, 2019, 卷号: 33, 期号: 03, 页码: 60-67 Authors: 贾轶楠; 张启帆 ; 仝晓通 ; 岳连捷 ; 张新宇![](/image/person.jpg)
View  |   Adobe PDF(2765Kb)  |   Favorite  |  View/Download:391/52  |  Submit date:2019/09/12 自起动性能 肩部膨胀扇 侧压式 边界层厚度 几何喉道 气动喉道 |
| 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:285/56  |  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 |
| 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 Authors: Yue LJ(岳连捷) ; Jia YN(贾轶南); Xu X ; Zhang XY(张新宇) ; Zhang P(张鹏)
View  |   Adobe PDF(2110Kb)  |   Favorite  |  View/Download:402/143  |  Submit date:2018/10/30 Inlet restart Cowl shock Shock wave boundary layer interactions |