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A fourth-order scheme for the unsteady compressible Navier-Stokes equationsA computational scheme is described which is second-order accurate in time and fourth-order accurate in space (2-4). This method is applied to study the stability of compressible boundary layers. The laminar compressible Navier-Stokes equations are solved with a time harmonic inflow superimposed on the steady state solution. This results in spatially unstable modes. It is shown that the second-order methods are inefficient for calculating the growth rates and phases of the unstable modes. In contrast the fourth-order method yields accurate results on relatively course meshes.
Document ID
19860004751
Acquisition Source
Legacy CDMS
Document Type
Preprint (Draft being sent to journal)
Authors
Bayliss, A.
(NASA Langley Research Center Hampton, VA, United States)
Parikh, P.
(NASA Langley Research Center Hampton, VA, United States)
Maestrello, L.
(NASA Langley Research Center Hampton, VA, United States)
Turkel, E.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 5, 2013
Publication Date
October 1, 1985
Subject Category
Aerodynamics
Report/Patent Number
NASA-CR-177994
NAS 1.26:177994
ICASE-85-44
Accession Number
86N14221
Funding Number(s)
CONTRACT_GRANT: NAS1-17070
CONTRACT_GRANT: NAS1-17130
PROJECT: RTOP 505-31-83-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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