On the mechanism of acoustic resonances from a leading-edge slat

被引:16
|
作者
Li, Weipeng [1 ]
Guo, Yongheng [2 ]
Liu, Wanglin [2 ]
机构
[1] Shanghai Jiao Tong Univ, Dept Aeronaut & Astronaut, Shanghai 200240, Peoples R China
[2] China Aerodynam Res & Dev Ctr, Mianyang 621000, Sichuan, Peoples R China
基金
中国国家自然科学基金;
关键词
Slat noise; Acoustic resonances; Fluid-acoustic feedback; Noise generation mechanism; FINITE-DIFFERENCE SCHEMES; EDDY SIMULATION; NOISE; FLOW; DYNAMICS; MODEL;
D O I
10.1016/j.ast.2021.106711
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Implicit large-eddy simulations are performed to investigate the acoustic resonances from a leading-edge slat at two different Reynolds numbers. Three types of acoustic waves are identified in the vicinity of the slat, but only one is found to be amplified by fluid-acoustic feedback mechanism. With phase-averaged flow-fields, we clearly identify that the vortical structures in the slat cove are formed at the same frequencies of the observed acoustic tones. A fluid-acoustic feedback loop is confirmed between the formation of the discrete vortices and the radiation of low-frequency acoustic waves. A theoretical model is proposed and validated to predict the frequencies of low-frequency resonances at three angles of attack. High-frequency acoustic waves are also found to emanate from the slat-wake region and the suction side of the main wing. (C) 2021 Elsevier Masson SAS. All rights reserved.
引用
收藏
页数:11
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