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Three-Dimensional, Subsonic, Turbulent Juncture Region FlowCMC3DPNS predicts three-dimensional, subsonic, turbulent aerodynamic juncture region flow. Versatile program for comprehensive flow-field analysis applies finite-element methodology to nonlinear field problems. Order-ofmagnitude analysis of subsonic, three-dimensional, steady time-averaged NavierStokes equations for semibounded aerodynamic juncture geometries yields para bolic Navier-Stokes equations. CMC3DPNS solves these equations to predict juncture-region flow.
Document ID
19850000540
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Baker, A. J. (Computational Mechanics Consultants)
Manhardt, P. D. (Computational Mechanics Consultants)
Orzechowski, J. A. (Computational Mechanics Consultants)
Date Acquired
August 12, 2013
Publication Date
March 1, 1986
Publication Information
Publication: NASA Tech Briefs
Volume: 9
Issue: 4
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
LAR-13263
ISSN: 0145-319X
Report Number: LAR-13263
Accession Number
85B10540
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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