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Incompressible viscous flow simulations of the NFAC wind tunnelThe capabilities of an existing 3-D incompressible Navier-Stokes flow solver, INS3D, are extended and improved to solve turbulent flows through the incorporation of zero- and two-equation turbulence models. The two-equation model equations are solved in their high Reynolds number form and utilize wall functions in the treatment of solid wall boundary conditions. The implicit approximate factorization scheme is modified to improve the stability of the two-equation solver. Applications to the 3-D viscous flow inside the 80 by 120 feet open return wind tunnel of the National Full Scale Aerodynamics Complex (NFAC) are discussed and described.
Document ID
19880005587
Acquisition Source
Legacy CDMS
Document Type
Preprint (Draft being sent to journal)
Authors
Champney, Joelle Milene
(Applied and Theoretical Mechanics, Inc. Oakland, CA, United States)
Date Acquired
September 5, 2013
Publication Date
June 1, 1986
Subject Category
Aerodynamics
Report/Patent Number
ATM-FR-25-012
NAS 1.26:177431
NASA-CR-177431
Report Number: ATM-FR-25-012
Report Number: NAS 1.26:177431
Report Number: NASA-CR-177431
Accession Number
88N14969
Funding Number(s)
PROJECT: RTOP 507-05-01
CONTRACT_GRANT: NAS2-12187
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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