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An investigation of several numerical procedures for time-asymptotic compressible Navier-Stokes solutionsThe status of an investigation of four numerical techniques for the time-dependent compressible Navier-Stokes equations is presented. Results for free shear layer calculations in the Reynolds number range from 1000 to 81000 indicate that a sequential alternating-direction implicit (ADI) finite-difference procedure requires longer computing times to reach steady state than a low-storage hopscotch finite-difference procedure. A finite-element method with cubic approximating functions was found to require excessive computer storage and computation times. A fourth method, an alternating-direction cubic spline technique which is still being tested, is also described.
Document ID
19760002934
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Rudy, D. H.
(NASA Langley Research Center Hampton, VA, United States)
Morris, D. J.
(NASA Langley Research Center Hampton, VA, United States)
Blanchard, D. K.
(NASA Langley Research Center Hampton, VA, United States)
Cooke, C. H.
(Old Dominion Univ.)
Rubin, S. G.
(Polytechnic Inst. of New York)
Date Acquired
August 8, 2013
Publication Date
January 1, 1975
Publication Information
Publication: Aerodynamic Analyses Requiring Advanced Computers, Pt. 1
Subject Category
Aerodynamics
Accession Number
76N10022
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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