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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：259/91  |  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：354/124  |  Submit date：2020/03/21
Hysteresis  Dual-mode scramjet  Supersonic combustion  Mode transition  Flame stabilization  Combustion oscillation