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Acceleration to a steady state for the Euler equationsA multi-stage Runge-Kutta method is analyzed for solving the Euler equations exterior to an airfoil. Highly subsonic, transonic and supersonic flows are evaluated. Various techniques for accelerating the convergence to a steady state are introduced and analyzed.
Document ID
19840021783
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Turkel, E. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 4, 2013
Publication Date
July 1, 1984
Subject Category
Aerodynamics
Report/Patent Number
NAS 1.26:172398
ICASE-84-32
NASA-CR-172398
Report Number: NAS 1.26:172398
Report Number: ICASE-84-32
Report Number: NASA-CR-172398
Accession Number
84N29852
Funding Number(s)
PROJECT: RTOP 505-31-83
CONTRACT_GRANT: NAS1-16394
CONTRACT_GRANT: NAS1-17130
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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