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Two-boundary grid generation for the solution of the three dimensional compressible Navier-Stokes equationsA grid generation technique called the two boundary technique is developed and applied for the solution of the three dimensional Navier-Stokes equations. The Navier-Stokes equations are transformed from a cartesian coordinate system to a computational coordinate system, and the grid generation technique provides the Jacobian matrix describing the transformation. The two boundary technique is based on algebraically defining two distinct boundaries of a flow domain and the distribution of the grid is achieved by applying functions to the uniform computational grid which redistribute the computational independent variables and consequently concentrate or disperse the grid points in the physical domain. The Navier-Stokes equations are solved using a MacCormack time-split technique. Grids and supersonic laminar flow solutions are obtained for a family of three dimensional corners and two spike-nosed bodies.
Document ID
19810019313
Acquisition Source
Legacy CDMS
Document Type
Thesis/Dissertation
Authors
Smith, R. E.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 4, 2013
Publication Date
May 1, 1981
Subject Category
Numerical Analysis
Report/Patent Number
NASA-TM-83123
Report Number: NASA-TM-83123
Accession Number
81N27851
Funding Number(s)
PROJECT: RTOP 505-31-83-02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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