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Research Efforts in Development of NPARC 2D/3D CFD CodesThe objective of the research was to develop a capability in the NPARC computational fluid dynamics (CFD) code to efficiently solve for unsteady airflows with moving geometry and grids. The application of interest was the unsteady flow in a high-speed aircraft inlet operating at the supercritical condition in which a terminal shock resides within the diffuser.
Document ID
19980193206
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Slater, John W. (NASA Lewis Research Center Cleveland, OH United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1998
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA/CR-1998-207576
NAS 1.26:207576
Report Number: NASA/CR-1998-207576
Report Number: NAS 1.26:207576
Funding Number(s)
CONTRACT_GRANT: NCC3-539
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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