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Navier-Stokes Computations On Zonal GridsReport describes numerical simulations of transonic flow of air about isolated wing and about wing and fuselage (not tail assembly) of F-16A aircraft. Fast, diagonalized Beam-Warming numerical-integration algorithm for solution of Euler and Navier-Stokes equations applied via Transonic Navier-Stokes computer program, using computational grids divided into zones of coarse and finer meshes.
Document ID
19910000669
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Flores, Jolen (NASA Ames Research Center, Moffett Field, CA.)
Date Acquired
August 14, 2013
Publication Date
December 1, 1991
Publication Information
Publication: NASA Tech Briefs
Volume: 15
Issue: 12
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
ARC-12447
ISSN: 0145-319X
Report Number: ARC-12447
Accession Number
91B10669
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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