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Towards Arbitrary Accuracy Inviscid Surface Boundary ConditionsInviscid nonlinear surface boundary conditions are currently limited to third order accuracy in time for non-moving surfaces and actually reduce to first order in time when the surfaces move. For steady-state calculations it may be possible to achieve higher accuracy in space, but high accuracy in time is required for efficient simulation of multiscale unsteady phenomena. A surprisingly simple technique is shown here that can be used to correct the normal pressure derivatives of the flow at a surface on a Cartesian grid so that arbitrarily high order time accuracy is achieved in idealized cases. This work demonstrates that nonlinear high order time accuracy at a solid surface is possible and desirable, but it also shows that the current practice of only correcting the pressure is inadequate.
Document ID
20030003723
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Dyson, Rodger W.
(NASA Glenn Research Center Cleveland, OH United States)
Hixon, Ray
(NASA Lewis Research Center Cleveland, OH United States)
Date Acquired
September 7, 2013
Publication Date
July 1, 2002
Subject Category
Acoustics
Report/Patent Number
ICOMP-2002-04
E-13368
NAS 1.15:211583
AIAA Paper 2002-2438
NASA/TM-2002-211583
Meeting Information
Meeting: Eight Aeroacoustics Conference
Location: Breckenridge, CO
Country: United States
Start Date: June 17, 2002
End Date: June 19, 2002
Sponsors: American Inst. of Aeronautics and Astronautics, Confederation of European Aerospace Societies
Funding Number(s)
PROJECT: RTOP 780-30-11
Distribution Limits
Public
Copyright
Public Use Permitted.
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