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Unstructured mesh solution of the Euler and Navier-Stokes equationsMesh generation procedures as well as solution algorithms for solving the Euler and Navier-Stokes equations on unstructured meshes are presented. The solution algorithms discussed utilize approximate Riemann solver, upwind differencing to achieve high spatial accuracy. Numerical results for Euler flow over single and multi-element airfoils are presented.
Document ID
19910001579
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Barth, Timothy J. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 6, 2013
Publication Date
September 1, 1989
Publication Information
Publication: NASA Computational Fluid Dynamics Conference. Volume 2: Sessions 7-12
Subject Category
Aerodynamics
Accession Number
91N10892
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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