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| Numerical investigation for subsonic performance of the high-pressure capturing wing configuration with wing dihedral 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2024, 卷号: 144, 页码: 16 Authors: Chang SY(常思源); Xiao Y(肖尧); Li GL(李广利) ; Tian ZW(田中伟); Cui K(崔凯)![](/image/person.jpg)
![](/themes/default/image/downing1.png) Favorite  |  View/Download:101/0  |  Submit date:2024/01/22 High-pressure capturing wing Subsonic Numerical simulation Wing dihedral Stability |
| Effect of combustion mode on thrust performance in a symmetrical tandem-cavity scramjet combustor 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2022, 卷号: 130, 页码: 11 Authors: Liu, Mingjiang; Sun, Mingbo; Zhao, Guoyan; Meng Y(孟宇) ; Huang, Yuhui; Ma, Guangwei; Wang, Hongbo
Adobe PDF(3841Kb)  |   Favorite  |  View/Download:129/29  |  Submit date:2022/12/20 Tandem-cavity Scramjet combustor Combustion mode Thrust performance |
| 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:427/82  |  Submit date:2021/03/03 Unsteady pressure measurement Pressure sensor Pressure transmission tube Dynamic response Compressible flow |
| Numerical investigation of a Mach 9 oblique detonation engine with fuel pre-injection 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 105, 页码: 9 Authors: Zhang ZJ(张子健); Ma KF(马凯夫); Zhang WS(张文硕) ; Han X(韩鑫); Liu YF(刘云峰) ; Jiang ZL(姜宗林)![](/image/person.jpg)
Adobe PDF(2608Kb)  |   Favorite  |  View/Download:282/123  |  Submit date:2020/11/30 Oblique detonation engine Pre-injection Detonative combustion Mixing Hydrogen |
| 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:295/116  |  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)![](/image/person.jpg)
Adobe PDF(2023Kb)  |   Favorite  |  View/Download:364/112  |  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:279/96  |  Submit date:2020/07/06 Aeroacoustics Rod-airfoil configuration Cell-centered finite difference method Delayed detached eddy simulation FW-H acoustic analogy |
| Combustion performance of a novel hybrid rocket fuel grain with a nested helical structure 期刊论文 AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 97, 页码: 8 Authors: Wang ZZ(王泽众) ; Lin X(林鑫) ; Li F(李飞) ; Yu XL(余西龙)![](/image/person.jpg)
Adobe PDF(1961Kb)  |   Favorite  |  View/Download:300/114  |  Submit date:2020/05/18 Hybrid rocket engine Paraffin-based fuel Acrylonitrile-butadiene-styrene Regression rate Combustion efficiency |
| 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)
Adobe PDF(3862Kb)  |   Favorite  |  View/Download:370/132  |  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)
Adobe PDF(3918Kb)  |   Favorite  |  View/Download:554/181  |  Submit date:2019/09/09 Fully confined supersonic jet Inclined impingement Heat transfer Boundary layer bleed Numerical simulation |