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Computation of Acoustic Waves Through Sliding-Zone Interfaces Using an Euler/Navier-Stokes CodeThe effect of a patched sliding-zone interface on the transmission of acoustic waves is examined for two- and three-dimensional model problems. A simple but general interpolation scheme at the patched boundary passes acoustic waves without distortion, provided that a sufficiently small time step is taken. A guideline is provided for the maximum permissible time step or zone speed that gives an acceptable error introduced by the sliding-zone interface.
Document ID
19960016732
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Rumsey, Christopher L.
(NASA Langley Research Center Hampton,VA United States)
Date Acquired
September 6, 2013
Publication Date
May 1, 1996
Subject Category
Acoustics
Report/Patent Number
NASA-TM-111404
AIAA Paper 96-1752
NAS 1.15:111404
Report Number: NASA-TM-111404
Report Number: AIAA Paper 96-1752
Report Number: NAS 1.15:111404
Meeting Information
Meeting: 2nd AIAA/CEAS Aeroacoustics Conference
Location: State College, PA
Country: United States
Start Date: May 6, 1996
End Date: May 8, 1996
Accession Number
96N22314
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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