Experimental Investigation on the Circular Cylindrical Cavity Noise at the Locked-on State

被引:0
作者
Sun, Yifeng [1 ]
Liu, Peiqing [1 ]
Fan, Fengzhi [1 ]
Guo, Hao [1 ]
机构
[1] Beihang Univ, Sch Aeronaut Sci & Engn, Beijing 100191, Peoples R China
来源
2023 ASIA-PACIFIC INTERNATIONAL SYMPOSIUM ON AEROSPACE TECHNOLOGY, VOL I, APISAT 2023 | 2024年 / 1050卷
基金
中国国家自然科学基金;
关键词
Cavity noise; Locked-on state; Dominant mode frequency; Overall sound pressure level; Aeroacoustics; FLOW; RESONANCE; LAYER;
D O I
10.1007/978-981-97-3998-1_123
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
In the locked-on state, the ratio of resonant frequency to the fundamental frequency of self-sustained oscillation is suggested to play a key role in predicting the dominant tonal noise for the square cavity. In this paper, we similarly investigate the mechanism of coupled self-excited oscillation and acoustic resonance aerodynamic noise in cylindrical cavities with different depths at low speeds. The experimental noise field results are described for a circular cavity with a diameter of 78 mm and a depth ranging from 70 mm to 120 mm at an incoming flow velocity of 5 to 35 m/s. A strong self-excited oscillatory discrete noise is generated in this cylindrical cavity flow at the locked-on state and the parameter R-d is also well proofed to evaluate and predict the dominant mode order and the total sound pressure level peak.
引用
收藏
页码:1577 / 1590
页数:14
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