Transmission in Flow Ducts with Peripherally Varying Linings
Abstract
A finite element Galerkin formulation is used for the calculation of acoustical modes in uniform ducts with arbitrary geometry, mean flow and lining configuration. Hermitian “non-conforming” subparametric elements are used and the dimensionality of the resulting eigenmatrix is reduced by the use of a condensation scheme based on the compatible eigenvectors in the case with no mean flow. Results are presented for simple circular and rectangular configurations for which exact comparison results are readily calculable. Computer graphics routines required to interpret modal data are described and sample results shown.
Recommended Citation
R. J. Astley et al., "Transmission in Flow Ducts with Peripherally Varying Linings," AIAA Paper, American Institute of Aeronautics and Astronautics (AIAA), Jan 1980.
The definitive version is available at https://doi.org/10.2514/6.1980-1015
Department(s)
Mechanical and Aerospace Engineering
Document Type
Article - Journal
Document Version
Citation
File Type
text
Language(s)
English
Rights
© 1980 American Institute of Aeronautics and Astronautics (AIAA), All rights reserved.
Publication Date
01 Jan 1980