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Automatic adaptive grid refinement for the Euler equationsA method of adaptive grid refinement for the solution of the steady Euler equations for transonic flow is presented. Algorithm automatically decides where the coarse grid accuracy is insufficient, and creates locally uniform refined grids in these regions. This typically occurs at the leading and trailing edges. The solution is then integrated to steady state using the same integrator (FL052) in the interior of each grid. The boundary conditions needed on the fine grids are examined and the importance of treating the fine/coarse grid interface conservatively is discussed. Numerical results are presented.
Document ID
19850046936
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Berger, M. J.
(New York University New York, NY, United States)
Jameson, A.
(Princeton University Princeton, NJ, United States)
Date Acquired
August 12, 2013
Publication Date
April 1, 1985
Publication Information
Publication: AIAA Journal
Volume: 23
ISSN: 0001-1452
Subject Category
Aerodynamics
Report/Patent Number
ISSN: 0001-1452
Accession Number
85A29087
Funding Number(s)
CONTRACT_GRANT: DE-AC02-76ER-03077
CONTRACT_GRANT: N00014-81-K-0379
CONTRACT_GRANT: NAG1-186
Distribution Limits
Public
Copyright
Other

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