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Inhomogeneous Radiation Boundary Conditions Simulating Incoming Acoustic Waves for Computational AeroacousticsA set of nonhomogeneous radiation and outflow conditions which automatically generate prescribed incoming acoustic or vorticity waves and, at the same time, are transparent to outgoing sound waves produced internally in a finite computation domain is proposed. This type of boundary condition is needed for the numerical solution of many exterior aeroacoustics problems. In computational aeroacoustics, the computation scheme must be as nondispersive ans nondissipative as possible. It must also support waves with wave speeds which are nearly the same as those of the original linearized Euler equations. To meet these requirements, a high-order/large-stencil scheme is necessary The proposed nonhomogeneous radiation and outflow boundary conditions are designed primarily for use in conjunction with such high-order/large-stencil finite difference schemes.
Document ID
19970011050
Acquisition Source
Langley Research Center
Document Type
Reprint (Version printed in journal)
Authors
Tam, Christopher K. W.
(Florida State Univ. Tallahassee, FL United States)
Fang, Jun
(Florida State Univ. Tallahassee, FL United States)
Kurbatskii, Konstantin A.
(Florida State Univ. Tallahassee, FL United States)
Date Acquired
September 6, 2013
Publication Date
December 1, 1996
Subject Category
Acoustics
Report/Patent Number
NASA-CR-203008
NAS 1.26:203008
Report Number: NASA-CR-203008
Report Number: NAS 1.26:203008
Meeting Information
Meeting: Fluid Dynamics and Propulsion
Location: Cairo
Country: Egypt
Start Date: December 29, 1996
End Date: December 31, 1996
Accession Number
97N16099
Funding Number(s)
CONTRACT_GRANT: NAG1-1776
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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