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Identification and localization of airfoil noise sources at low angles of attack

  • Beihang University

科研成果: 书/报告/会议事项章节会议稿件同行评审

摘要

Phased microphone array technique has received much attention for the localization of sound sources. In this paper, this technique is applied to investigate the airfoil self-noise based on a Computational Aeroacoustics (CAA) database. Two dimensional Direct Numerical Simulation (DNS) is conducted of flow over NACA0012 airfoil at low angles of attack and a moderate Reynolds number. Both the mean flow and acoustics results agree well with previous experimental and numerical data. The numerical data then served as an input for the noise identification and localization process. Three beamfoming algorithms are considered. The results of the phased array calculations show that the tonal noise is the dominant source for NACA0012 airfoil operating at low angles of attack and a moderate Reynolds number. With angle of attack increasing, the tonal sources move upstream and the noise strength is enhanced.

源语言英语
主期刊名52nd Aerospace Sciences Meeting
出版商American Institute of Aeronautics and Astronautics Inc.
ISBN(电子版)9781624102561
DOI
出版状态已出版 - 2014
活动52nd Aerospace Sciences Meeting 2014 - National Harbor, 美国
期限: 13 1月 201417 1月 2014

出版系列

姓名52nd Aerospace Sciences Meeting

会议

会议52nd Aerospace Sciences Meeting 2014
国家/地区美国
National Harbor
时期13/01/1417/01/14

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