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NASA NTRS · 19820034128

Acoustic transmission in lined flow ducts - A finite element eigenvalue problem

Abstract

The problem of acoustical transmission in lined ducts with subsonic mean flow is of considerable practical interest in the context of fan noise attenuation in the ducted inlet regions of turbofan aircraft engines. If nonaxisymmetric liners are present, a loss of axial symmetry results, and the study of acoustic transmission involves the solution of a full two-dimensional eigenvalue problem. The reported investigation is concerned with such an eigenvalue problem. The employed method of solution is effectively a two-dimensional analog of an approach considered by Astley and Eversman (1979). The approach makes use of a Galerkin Finite Element Method whereby the weighting and basis functions are generated automatically by the discretization.

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BibTeXRIS

Astley, R. J., Eversman, W.. 1981-01-01. Acoustic transmission in lined flow ducts - A finite element eigenvalue problem. https://ntrs.nasa.gov/citations/19820034128

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