NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Numerical techniques in linear duct acousticsBoth finite difference and finite element analyses of small amplitude (linear) sound propagation in straight and variable area ducts with flow, as might be found in a typical turboject engine duct, muffler, or industrial ventilation system, are reviewed. Both steady state and transient theories are discussed. Emphasis is placed on the advantages and limitations associated with the various numerical techniques. Examples of practical problems are given for which the numerical techniques have been applied.
Document ID
19800021653
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Baumeister, K. J.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1980
Subject Category
Acoustics
Report/Patent Number
NASA-TM-81553
E-513
Report Number: NASA-TM-81553
Report Number: E-513
Meeting Information
Meeting: Winter Ann. Meeting of ASME
Location: Chicago
Start Date: November 17, 1980
End Date: November 21, 1980
Accession Number
80N30154
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available