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| 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:391/67  |  提交时间:2021/03/03 Unsteady pressure measurement Pressure sensor Pressure transmission tube Dynamic response Compressible flow |
| 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:266/109  |  提交时间:2020/11/30 Oblique detonation wave Shock/combustion interaction Shock polar analysis High-resolution simulation |
| Numerical modeling of a high-enthalpy shock tunnel driven by gaseous detonation 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 104, 页码: 8 作者: Luo K(罗凯); Wang Q(汪球); Li JW(栗继伟); Li JP(李进平); Zhao W(赵伟) Adobe PDF(2023Kb)  |  收藏  |  浏览/下载:321/102  |  提交时间:2020/11/30 Quasi-one-dimensional Detonation Shock tunnel Shock speed |
| Investigation on rod-airfoil noise with high-order cell-centered finite difference method and acoustic analogy 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 102, 页码: 22 作者: Jin Y; Liao F(廖飞); Cai JS; Morris PJ Adobe PDF(7457Kb)  |  收藏  |  浏览/下载:245/87  |  提交时间:2020/07/06 Aeroacoustics Rod-airfoil configuration Cell-centered finite difference method Delayed detached eddy simulation FW-H acoustic analogy |
| 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:342/121  |  提交时间:2020/03/21 Hysteresis Dual-mode scramjet Supersonic combustion Mode transition Flame stabilization Combustion oscillation |
| 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:534/172  |  提交时间:2019/09/09 Fully confined supersonic jet Inclined impingement Heat transfer Boundary layer bleed Numerical simulation |
| Experimental study of flame characteristics of ethylene and its mixture with methane and hydrogen in supersonic combustor 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 86, 页码: 775-781 作者: Zhong FQ(仲峰泉); Cheng LW(程柳维); Gu HB(顾洪斌); Zhang XY(张新宇) Adobe PDF(2032Kb)  |  收藏  |  浏览/下载:303/91  |  提交时间:2019/05/29 Supersonic combustor Hydrocarbon Mixture fuel Flame structure Ignition |