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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
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：399/69 | Submit date：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
Authors: Yang L; Yue LJ(岳连捷); Zhang QF(张启帆); Zhang XY(张新宇)
Adobe PDF(5176Kb) | Favorite | View/Download：277/113 | Submit date：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
Authors: 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) | Favorite | View/Download：330/105 | Submit date：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
Authors: Jin Y; Liao F(廖飞); Cai JS; Morris PJ
Adobe PDF(7457Kb) | Favorite | View/Download：258/90 | Submit date：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
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：351/124 | Submit date：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
Authors: Huang TL(黄庭隆); Yue LJ(岳连捷); Chang XY(张新宇)
View | Adobe PDF(3918Kb) | Favorite | View/Download：539/173 | Submit date：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
Authors: Zhong FQ(仲峰泉); Cheng LW(程柳维); Gu HB(顾洪斌); Zhang XY(张新宇)
Adobe PDF(2032Kb) | Favorite | View/Download：308/93 | Submit date：2019/05/29
Supersonic combustor Hydrocarbon Mixture fuel Flame structure Ignition |
