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A multistage time-stepping scheme for the Navier-Stokes equationsA class of explicit multistage time-stepping schemes is used to construct an algorithm for solving the compressible Navier-Stokes equations. Flexibility in treating arbitrary geometries is obtained with a finite-volume formulation. Numerical efficiency is achieved by employing techniques for accelerating convergence to steady state. Computer processing is enhanced through vectorization of the algorithm. The scheme is evaluated by solving laminar and turbulent flows over a flat plate and an NACA 0012 airfoil. Numerical results are compared with theoretical solutions or other numerical solutions and/or experimental data.
Document ID
19850037321
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Swanson, R. C.
(NASA Langley Research Center Theoretical Aerodynamics Branch, Hampton, VA, United States)
Turkel, E.
(Tel Aviv University Tel Aviv, Israel)
Date Acquired
August 12, 2013
Publication Date
January 1, 1985
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 85-0035
Report Number: AIAA PAPER 85-0035
Accession Number
85A19472
Funding Number(s)
CONTRACT_GRANT: NAS1-17070
Distribution Limits
Public
Copyright
Other

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