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Simulation of transonic viscous wing and wing-fuselage flows using zonal methodsThe thin-layer Navier-Stokes equations are coupled with a zonal scheme (or domain-decomposition method) to develop the Transonic Navier-Stokes (TNS) wing-alone code. The TNS has a total of 4 zones and is extended to a total of 16 zones for the wing-fuselage version of the code. Results are compared on the Cray X-MP-48 and compared with experimental data.
Document ID
19870010809
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Flores, Jolen (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 5, 2013
Publication Date
March 1, 1987
Subject Category
Aerodynamics
Report/Patent Number
NAS 1.15:89421
A-87066
NASA-TM-89421
Report Number: NAS 1.15:89421
Report Number: A-87066
Report Number: NASA-TM-89421
Accession Number
87N20242
Funding Number(s)
PROJECT: RTOP 505-60-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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