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Implicit method for the computation of unsteady flows on unstructured gridsAn implicit method for the computation of unsteady flows on unstructured grids is presented. Following a finite difference approximation for the time derivative, the resulting nonlinear system of equations is solved at each time step by using an agglomeration multigrid procedure. The method allows for arbitrarily large time steps and is efficient in terms of computational effort and storage. Inviscid and viscous unsteady flows are computed to validate the procedure. The issue of the mass matrix which arises with vertex-centered finite volume schemes is addressed. The present formulation allows the mass matrix to be inverted indirectly. A mesh point movement and reconnection procedure is described that allows the grids to evolve with the motion of bodies. As an example of flow over bodies in relative motion, flow over a multi-element airfoil system undergoing deployment is computed.
Document ID
19960001963
Acquisition Source
Legacy CDMS
Document Type
Preprint (Draft being sent to journal)
Authors
Venkatakrishnan, V.
(Institute for Computer Applications in Science and Engineering Hampton, VA, United States)
Mavriplis, D. J.
(Institute for Computer Applications in Science and Engineering Hampton, VA, United States)
Date Acquired
September 6, 2013
Publication Date
August 1, 1995
Subject Category
Numerical Analysis
Report/Patent Number
NASA-CR-198206
NAS 1.26:198206
ICASE-95-60
Report Number: NASA-CR-198206
Report Number: NAS 1.26:198206
Report Number: ICASE-95-60
Accession Number
96N11971
Funding Number(s)
CONTRACT_GRANT: NAS1-19480
PROJECT: RTOP 505-90-52-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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