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Experimental Investigation of Abrupt Change in a Scramjet with Variable Mach-Number Flow 期刊论文
AIAA JOURNAL, 2022, 页码: 9
Authors:  Wu ZJ(吴振杰);  Zhang QF(张启帆);  Zhang X(张旭);  Luo WH(罗苇航);  Gao ZB(高占彪);  Yue LJ(岳连捷)
Adobe PDF(3049Kb)  |  Favorite  |  View/Download：169/28  |  Submit date：2022/07/18
Fuel Regulation Historical Effects on Flame Stabilizations in a Cavity-Based Scramjet Combustor 期刊论文
AIAA JOURNAL, 2022, 页码: 7
Authors:  Zhang X(张旭);  Zhang QF(张启帆);  Wu ZJ(吴振杰);  Yue LJ(岳连捷);  Gao ZB(高占彪);  Luo WH(罗苇航);  Chen H(陈昊)
Adobe PDF(1382Kb)  |  Favorite  |  View/Download：162/31  |  Submit date：2022/03/22
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：359/126  |  Submit date：2020/03/21
Hysteresis  Dual-mode scramjet  Supersonic combustion  Mode transition  Flame stabilization  Combustion oscillation