NASA NTRS · 19960053067
Introduction to computational aero-acoustics
Abstract
Computational 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.
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Hardin, Jay C.. 1996-01-01. Introduction to computational aero-acoustics. https://ntrs.nasa.gov/citations/19960053067
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