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A Robust Absorbing Boundary Condition for Compressible FlowsAn absorbing non-reflecting boundary condition (NRBC) for practical computations in fluid dynamics and aeroacoustics is presented with theoretical proof. This paper is a continuation and improvement of a previous paper by the author. The absorbing NRBC technique is based on a first principle of non reflecting, which contains the essential physics that a plane wave solution of the Euler equations remains intact across the boundary. The technique is theoretically shown to work for a large class of finite volume approaches. When combined with the hyperbolic conservation laws, the NRBC is simple, robust and truly multi-dimensional; no additional implementation is needed except the prescribed physical boundary conditions. Several numerical examples in multi-dimensional spaces using two different finite volume schemes are illustrated to demonstrate its robustness in practical computations. Limitations and remedies of the technique are also discussed.
Document ID
20050237890
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Loh, Ching Y.
(NASA Glenn Research Center Cleveland, OH, United States)
orgenson, Philip C. E.
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
September 7, 2013
Publication Date
October 1, 2005
Subject Category
Fluid Mechanics And Thermodynamics
Report/Patent Number
NASA/TM-2005-213654
E-15143
AIAA Paper 2005-4716
Meeting Information
Meeting: 17th Computational Fluid Dynamics Conference
Location: Toronto, Ontario
Country: Canada
Start Date: June 6, 2005
End Date: June 9, 2005
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
CONTRACT_GRANT: NAS3-0702
OTHER: 22-781-30-69
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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