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An Application of the Difference Potentials Method to Solving External Problems in CFDNumerical solution of infinite-domain boundary-value problems requires some special techniques that would make the problem available for treatment on the computer. Indeed, the problem must be discretized in a way that the computer operates with only finite amount of information. Therefore, the original infinite-domain formulation must be altered and/or augmented so that on one hand the solution is not changed (or changed slightly) and on the other hand the finite discrete formulation becomes available. One widely used approach to constructing such discretizations consists of truncating the unbounded original domain and then setting the artificial boundary conditions (ABC's) at the newly formed external boundary. The role of the ABC's is to close the truncated problem and at the same time to ensure that the solution found inside the finite computational domain would be maximally close to (in the ideal case, exactly the same as) the corresponding fragment of the original infinite-domain solution. Let us emphasize that the proper treatment of artificial boundaries may have a profound impact on the overall quality and performance of numerical algorithms. The latter statement is corroborated by the numerous computational experiments and especially concerns the area of CFD, in which external problems present a wide class of practically important formulations. In this paper, we review some work that has been done over the recent years on constructing highly accurate nonlocal ABC's for calculation of compressible external flows. The approach is based on implementation of the generalized potentials and pseudodifferential boundary projection operators analogous to those proposed first by Calderon. The difference potentials method (DPM) by Ryaben'kii is used for the effective computation of the generalized potentials and projections. The resulting ABC's clearly outperform the existing methods from the standpoints of accuracy and robustness, in many cases noticeably speed up the multigrid convergence, and at the same time are quite comparable to other methods from the standpoints of geometric universality and simplicity of implementation.
Document ID
19970017370
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
Ryaben 'Kii, Victor S.
(Academy of Sciences (USSR) Moscow, USSR)
Tsynkov, Semyon V.
(NASA Langley Research Center Hampton, VA United States)
Date Acquired
September 6, 2013
Publication Date
March 1, 1997
Subject Category
Aerodynamics
Report/Patent Number
NAS 1.15:110338
NASA-TM-110338
Report Number: NAS 1.15:110338
Report Number: NASA-TM-110338
Accession Number
97N19659
Funding Number(s)
PROJECT: RTOP 522-31-21-04
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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