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Inuence of shear flow on liner impedance computed by multimodal method

科研成果: 书/报告/会议事项章节会议稿件同行评审

摘要

A numerical method is proposed to compute the liner impedance under shear grazing flow. The flow-acoustic coupling that mainly occurs at the perforations is simulated using multimodal method. The Floquet-Bloch theorem is utilized to educe the liner impedance after the multimodal computation. Such simple calculation gives results that are in agreement with the empirical model in the order of magnitude of the changes in impedance with flow speed. Furthermore, the proposed method allows to take into account the thickness of the boundary layer. Results indicate that the shear flow eduction gives better predictions than the uniform eduction with Ingard-Myers condition, particularly for a relatively thick boundary layer. The liner resistance is shown to maintain the no-flow value until flow speed reaches a threshold value. After the threshold, the resistance increases almost linearly with flow Mach number, and with a larger slope in the case of a thinner boundary layer. It is also found that as flow conditions vary, the change of resistance is consistent with the variation in the level of flow-acoustic coupling, which indicates that the flow inuence on liner impedance results from such coupling.

源语言英语
主期刊名22nd AIAA/CEAS Aeroacoustics Conference
出版商American Institute of Aeronautics and Astronautics Inc, AIAA
ISBN(印刷版)9781624103865
DOI
出版状态已出版 - 2016
已对外发布
活动22nd AIAA/CEAS Aeroacoustics Conference, 2016 - Lyon, 法国
期限: 30 5月 20161 6月 2016

出版系列

姓名22nd AIAA/CEAS Aeroacoustics Conference, 2016

会议

会议22nd AIAA/CEAS Aeroacoustics Conference, 2016
国家/地区法国
Lyon
时期30/05/161/06/16

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