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Implicit boundary conditions for the solution of the parabolized Navier-Stokes equations for supersonic flowsA fully implicit set of boundary conditions is developed for the solution of the parabolized Navier-Stokes equations for supersonic flow in two dimensions. Shock fitting is employed at the shock and the body has no-slip and specified temperature conditions. A specified heat transfer condition at the wall can be handled in a similar manner. In addition, the shock location is advanced in space in a fully implicit manner by utilizing the Rankine-Hugoniot conditions along with global conservation of mass.
Document ID
19810025332
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Barnett, M. (NASA Ames Research Center Moffett Field, CA, United States)
Davis, R. T. (NASA Ames Research Center Moffett Field, CA, United States)
Rakich, J. V. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 11, 2013
Publication Date
October 1, 1981
Publication Information
Publication: Numerical Boundary Condition Procedures
Subject Category
Numerical Analysis
Accession Number
81N33875
Funding Number(s)
CONTRACT_GRANT: NCA2-OR130-101
CONTRACT_GRANT: NCA2-OR130-901
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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