|
Selected(0)Clear
Items/Page: Sort: |
| Experimental Study of Kerosene Ignition and Flame Stabilization in a Supersonic Combustor 期刊论文
International Journal of Turbo & Jet-Engines, 2022, 卷号: 39, 期号: 3, 页码: 403-410
Authors: Meng Y(孟宇) ; Gu HB(顾洪斌); Zhang XY(张新宇)
 Adobe PDF(3187Kb) |  Favorite | View/Download：288/90 | Submit date：2021/10/29 |
| 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：288/114 | Submit date：2020/11/30
Oblique detonation wave Shock/combustion interaction Shock polar analysis High-resolution simulation |
| 微波增强滑移电弧等离子体辅助超声速燃烧 期刊论文
航空学报, 2020, 卷号: 41, 期号: 2, 页码: 123345
Authors: 孟宇; 顾洪斌; 孙文明; 张新宇
 View | Adobe PDF(945Kb) | Favorite | View/Download：248/34 | Submit date：2019/12/16
超燃冲压发动机 超声速燃烧 等离子体助燃 滑移电弧 微波 |
| 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：362/127 | Submit date：2020/03/21
Hysteresis Dual-mode scramjet Supersonic combustion Mode transition Flame stabilization Combustion oscillation |
| Experimental study of mode transition characteristics of a cavity-based scramjet combustor during acceleration 期刊论文
Aerospace Science and Technology, 2019, 卷号: 93, 期号: 10, 页码: UNSP 105316
Authors: Meng Y(孟宇); Gu HB(顾洪斌); Zhuang JH(庄金衡); Sun WM(孙文明); Gao ZB(高占彪); Lian H(连欢); Yue LJ(岳连捷); Chang XY(张新宇)
View | Adobe PDF(3099Kb) | Favorite | View/Download：378/100 | Submit date：2019/10/15
Scramjet Combustor Mode Transition Liquid Kerosene Acceleration |
| 超燃冲压发动机加速过程中燃烧不稳定性研究 会议论文
中国力学大会, 中国浙江杭州, 2019年8月25-28日
Authors: 孟宇; 顾洪斌; 岳连捷; 张新宇
View | Adobe PDF(1057Kb) | Favorite | View/Download：284/80 | Submit date：2019/11/21
超燃冲压发动机 不稳定性 加速过程 直连台 实验研究 |
| 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：324/99 | Submit date：2019/05/29
Supersonic combustor Hydrocarbon Mixture fuel Flame structure Ignition |
| Experimental Study of Ignition and Flame Characteristics of Surrogate of Cracked Hydrocarbon Fuels in Supersonic Crossflow 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors: Cheng LW(程柳维); Zhong FQ(仲峰泉); Wang ZP(王知溥); Gu HB(顾洪斌); Ma SG(马素刚); Zhang XY(张新宇)
 Adobe PDF(517Kb) | Favorite | View/Download：343/112 | Submit date：2018/01/16
Combustors Cracks Diesel Engines Efficiency Ethylene Fighter Aircraft Fuels High Speed Cameras Ignition Kerosene Luminance Spacecraft Stabilization |
| Experimental study on the effect of combustor configuration on the performance of dual-mode combustor 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2015, 卷号: 42, 页码: 169-175
Authors: Wang ZP(王知溥); Li F(李飞); Gu HS; Yu XL(余西龙); Zhang XY(张新宇); Li, F (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
Adobe PDF(1112Kb) | Favorite | View/Download：567/234 | Submit date：2015/06/12
Scramjet Dual-mode Combustor Divergent Angle Cavity Location Combustion Efficiency Tdlas |
| Experimental study of combustion oscillations in a dual-mode scramjet 会议论文
20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 2015, 2015
Authors: Tian XD; Chen LH(陈立红); Gu HB(顾洪斌); Liu C; Cheng LW; Chang XY(张新宇); Chen, Lihong (lhchen@imech.ac.cn)
View | Adobe PDF(824Kb) | Favorite | View/Download：255/74 | Submit date：2017/09/04 |
