NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Transmission in flow ducts with peripherally varying liningsA 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' sub-parametric 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.
Document ID
19800051802
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Astley, R. J.
(Canterbury, University Christchurch, New Zealand)
Walkington, N. J.
(Canterbury Univ. Christchurch, New Zealand)
Eversman, W.
(Missouri-Rolla, University Rolla, Mo., United States)
Date Acquired
August 10, 2013
Publication Date
June 1, 1980
Subject Category
Acoustics
Report/Patent Number
AIAA PAPER 80-1015
Meeting Information
Meeting: Aeroacoustics Conference
Location: Hartford, CT
Start Date: June 4, 1980
End Date: June 6, 1980
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
80A35972
Funding Number(s)
CONTRACT_GRANT: NSG-3231
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available