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Hypersonic, nonequilibrium flow over a cylindrically blunted 6 deg wedgeThe numerical simulation of hypersonic flow in chemical nonequilibrium over cylindrically blunted 6 degree wedge is described. The simulation was executed on a Cray C-90 with Program LAURA 92-vl. Code setup procedures and sample results, including grid refinement studies and variations of species number are discussed. This simulation relates to a study of wing leading edge heating on transatmospheric vehicles.
Document ID
19940008099
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Gnoffo, Peter A. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 6, 2013
Publication Date
August 1, 1993
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NAS 1.15:108994
NASA-TM-108994
Report Number: NAS 1.15:108994
Report Number: NASA-TM-108994
Accession Number
94N12571
Funding Number(s)
PROJECT: RTOP 506-40-91-02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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