先进的分析风扇噪声测量支持的理论来源模型

IF 1.2 4区 工程技术 Q3 ACOUSTICS
Lukas Klähn, A. Moreau, L. Caldas, Robert Jaron, U. Tapken
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引用次数: 2

摘要

为了进一步了解风机噪声源的主要机理,在低速风机试验台上进行了全面的实验研究。对一种新型叶片集成盘(Blisk)转子,在系统改变轴速和节流的情况下,测量了风扇的气动图和声学特性。对实验结果的解释得到了一个基于物理的风机噪声预测分析内部工具的模拟的支持。对于声学测量,在入口部分使用了一组壁面冲洗麦克风。利用径向模态分析技术,计算了各工作点的宽带声功率和调频声功率。在获得的综合数据库中,发现音调和宽带声功率随流量的系统变化。这些模式只能部分地与旋翼叶片入射角的变化有关。通过比较实测噪声和分析模型的模态分布,可以得出转子-定子相互作用和流-转子相互作用的主要噪声源。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Advanced analysis of fan noise measurements supported by theoretical source models
With the objective to improve the understanding of the dominant fan noise source mechanisms, a comprehensive experimental study was conducted at a low speed fan test rig. The aerodynamic fan map as well as the acoustic characteristics of the fan was measured for a new blade integrated disk (Blisk) rotor with systematic variation of the shaft speed and throttling. The interpretation of the results is supported by simulations of the experiment with a physics-based analytical in-house tool for fan noise prediction. For the acoustic measurements, an array of wall-flushed microphones was used in the inlet section. By means of radial mode analysis techniques, the broadband and tonal sound powers are calculated for each operating point. In the obtained comprehensive database, systematic variations of the tonal and broadband sound power with the flow rate are found. These patterns can only partly be correlated to the varying incidence angle of the rotor blades. Comparing the mode distributions of the measured noise and the analytical models then allows conclusions on the predominant noise sources of rotor–stator interaction and inflow-rotor interaction.
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来源期刊
International Journal of Aeroacoustics
International Journal of Aeroacoustics ACOUSTICS-ENGINEERING, AEROSPACE
CiteScore
2.10
自引率
10.00%
发文量
38
审稿时长
>12 weeks
期刊介绍: International Journal of Aeroacoustics is a peer-reviewed journal publishing developments in all areas of fundamental and applied aeroacoustics. Fundamental topics include advances in understanding aeroacoustics phenomena; applied topics include all aspects of civil and military aircraft, automobile and high speed train aeroacoustics, and the impact of acoustics on structures. As well as original contributions, state of the art reviews and surveys will be published. Subtopics include, among others, jet mixing noise; screech tones; broadband shock associated noise and methods for suppression; the near-ground acoustic environment of Short Take-Off and Vertical Landing (STOVL) aircraft; weapons bay aeroacoustics, cavity acoustics, closed-loop feedback control of aeroacoustic phenomena; computational aeroacoustics including high fidelity numerical simulations, and analytical acoustics.
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