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Introduction to computational aero-acousticsComputational aeroacoustics (CAA) is introduced, by presenting its definition, advantages, applications, and initial challenges. The effects of Mach number and Reynolds number on CAA are considered. The CAA method combines the methods of aeroacoustics and computational fluid dynamics.
Document ID
19960053067
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Hardin, Jay C. (NASA Langley Research Center Hampton, VA United States)
Date Acquired
August 17, 2013
Publication Date
January 1, 1996
Publication Information
Publication: Applied Aero-Acoustics: Prediction Methods
Subject Category
Acoustics
Accession Number
96N36000
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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