|
Selected(0)Clear
Items/Page: Sort: |
| Coupling Effect of Multicavity on Flame Stabilization Mode Transitions in Scramjet Combustor 期刊论文
JOURNAL OF PROPULSION AND POWER, 2023
Authors: Wu ZJ(吴振杰); Zhang QF(张启帆) ; Yu FY(于方游); Luo WH(罗苇航); Gao ZB(高占彪); Yue LJ(岳连捷)
 Adobe PDF(582Kb) |  Favorite | View/Download：56/7 | Submit date：2023/06/15
Scramjet Engines Combustor Design flame stabilization mode transition path dependence |
| 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：413/75 | 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：271/41 | 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：218/56 | 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：286/113 | Submit date：2020/11/30
Oblique detonation wave Shock/combustion interaction Shock polar analysis High-resolution simulation |
| 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
Authors: Yang L; 岳连捷; 张启帆; 张新宇
Adobe PDF(1289Kb) | Favorite | View/Download：230/59 | Submit date：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
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：361/126 | Submit date：2020/03/21
Hysteresis Dual-mode scramjet Supersonic combustion Mode transition Flame stabilization Combustion oscillation |
| 一种进气道定堵塞度自起动试验装置 专利
发明专利. 一种进气道定堵塞度自起动试验装置, 专利号: ZL201710941567.2, 申请日期: 2017-10-11,
Inventors: 张启帆; 彭辉; 岳连捷; 南轶楠; 张新宇
Adobe PDF(502Kb) | Favorite | View/Download：164/30 | Submit date：2020/02/10 |
| 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
Adobe PDF(2765Kb) | Favorite | View/Download：369/47 | 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
Adobe PDF(1675Kb) | Favorite | View/Download：258/50 | 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 |
