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An effective multigrid method for high-speed flowsThe use is considered of a multigrid method with central differencing to solve the Navier-Stokes equations for high speed flows. The time dependent form of the equations is integrated with a Runge-Kutta scheme accelerated by local time stepping and variable coefficient implicit residual smoothing. Of particular importance are the details of the numerical dissipation formulation, especially the switch between the second and fourth difference terms. Solutions are given for 2-D laminar flow over a circular cylinder and a 15 deg compression ramp.
Document ID
19910020782
Acquisition Source
Legacy CDMS
Document Type
Preprint (Draft being sent to journal)
Authors
Swanson, R. C.
(NASA Langley Research Center Hampton, VA., United States)
Turkel, E.
(Tel-Aviv Univ. (Israel). VA., United States)
White, J. A.
(Analytical Services and Materials, Inc., Hampton)
Date Acquired
September 6, 2013
Publication Date
July 1, 1991
Subject Category
Aerodynamics
Report/Patent Number
AD-A240568
ICASE-91-56
NASA-CR-187602
NAS 1.26:187602
Report Number: AD-A240568
Report Number: ICASE-91-56
Report Number: NASA-CR-187602
Report Number: NAS 1.26:187602
Accession Number
91N30096
Funding Number(s)
CONTRACT_GRANT: NAS1-18605
PROJECT: RTOP 505-90-52-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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