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Calculation model for sound propagation in duct with circumferentially non-uniform liner

  • Beihang University
  • The University of Hong Kong

科研成果: 书/报告/会议事项章节会议稿件同行评审

摘要

Ill this paper, an efficient method is described for modeling the wave propagation in a circumferentiaUy non-uniform lined annular duct with mean flow. The cross-section space is discretized by Chebyshev spectral method, through which the equation matrix for physical field and the influence matrix of boundary condition are established. Then the issue is converted to an eigenvalue problem in terms of the acoustic propagation, where the eigenvalues stand for axial wave numbers, the eigenvectors display wave mode profiles. The sound pressure and axial velocity continuity equation is applied at the interface between different segments of the duct, through which the sound field in duct is constructed. It is shown that by using present method, which requires quite less quantity of CPU time compared with 3D numerical method, the superiority in broadband noise reduction of circumferential non-uniform liners is revealed. When sound propagates through the duct lined by circumferential non- uniform liner, the energy is scattered into modes of different orders. What is more, this method is expected to serve as an efficient approach for the optimization of non-uniform liner in the future.

源语言英语
主期刊名23rd AIAA/CEAS Aeroacoustics Conference, 2017
出版商American Institute of Aeronautics and Astronautics Inc, AIAA
ISBN(印刷版)9781624105043
DOI
出版状态已出版 - 2017
活动23rd AIAA/CEAS Aeroacoustics Conference, 2017 - Denver, 美国
期限: 5 6月 20179 6月 2017

出版系列

姓名23rd AIAA/CEAS Aeroacoustics Conference, 2017

会议

会议23rd AIAA/CEAS Aeroacoustics Conference, 2017
国家/地区美国
Denver
时期5/06/179/06/17

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