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Line relaxation methods for the solution of 2D and 3D compressible flowsAn implicit finite element based algorithm for the compressible Navier-Stokes equations is outlined, and the solution of the resulting equation by a line relaxation on general meshes of triangles or tetrahedra is described. The problem of generating and adapting unstructured meshes for viscous flows is reexamined, and an approach for both 2D and 3D simulations is proposed. An efficient approach appears to be the use of an implicit/explicit procedure, with the implicit treatment being restricted to those regions of the mesh where viscous effects are known to be dominant. Numerical examples demonstrating the computational performance of the proposed techniques are given.
Document ID
19930061062
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hassan, O.
(NASA Langley Research Center Hampton, VA, United States)
Probert, E. J.
(NASA Langley Research Center Hampton, VA, United States)
Morgan, K.
(Univ. College Swansea, United Kingdom)
Peraire, J.
(Imperial College of Science, Technology, and Medicine London, United Kingdom)
Date Acquired
August 16, 2013
Publication Date
January 1, 1993
Publication Information
Publication: In: AIAA Computational Fluid Dynamics Conference, 11th, Orlando, FL, July 6-9, 1993, Technical Papers. Pt. 2 (A93-44994 18-34)
Publisher: American Institute of Aeronautics and Astronautics
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 93-3366
Accession Number
93A45059
Funding Number(s)
CONTRACT_GRANT: NAGW-1809
Distribution Limits
Public
Copyright
Other

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