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A structured and unstructured remeshing method for high speed flowsAn adaptive remeshing method using both triangular and quadrilateral elements suitable for high speed flows is presented. For inviscid flows the method generates completely unstructured meshes. For viscous flows the boundary layer edge is identified adaptively and a structured mesh is generated in the boundary layer, and an unstructured mesh is generated in the inviscid region. Examples of inviscid and viscous mesh adaptations for high speed flows are presented. A comparison is made between first order and higher order finite element algorithms when used in association with the remeshing method.
Document ID
19900032777
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Vemaganti, Gururaja R.
(Lockheed Engineering and Sciences Co. Hampton, VA, United States)
Thornton, Earl A.
(Virginia, University Charlottesville, United States)
Wieting, Allan R.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 14, 2013
Publication Date
January 1, 1990
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 90-0401
Report Number: AIAA PAPER 90-0401
Accession Number
90A19832
Funding Number(s)
CONTRACT_GRANT: NSG-1321
Distribution Limits
Public
Copyright
Other

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