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

  • Beihang University
  • The University of Hong Kong

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

Abstract

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.

Original languageEnglish
Title of host publication23rd AIAA/CEAS Aeroacoustics Conference, 2017
PublisherAmerican Institute of Aeronautics and Astronautics Inc, AIAA
ISBN (Print)9781624105043
DOIs
StatePublished - 2017
Event23rd AIAA/CEAS Aeroacoustics Conference, 2017 - Denver, United States
Duration: 5 Jun 20179 Jun 2017

Publication series

Name23rd AIAA/CEAS Aeroacoustics Conference, 2017

Conference

Conference23rd AIAA/CEAS Aeroacoustics Conference, 2017
Country/TerritoryUnited States
CityDenver
Period5/06/179/06/17

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