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Hypersonic, nonequilibrium flow over the FIRE 2 forebody at 1634 secThe numerical simulation of hypersonic flow in thermochemical nonequilibrium over the forebody of the FIRE 2 vehicle at 1634 sec in its trajectory is described. The simulation was executed on a Cray C90 with the program Langley Aerodynamic Upwind Relaxation Algorithm (LAURA) 4.0.2. Code setup procedures and sample results, including grid refinement studies, are discussed. This simulation relates to a study of radiative heating predictions on aerobrake type vehicles.
Document ID
19940032947
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Chambers, Lin Hartung (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 6, 2013
Publication Date
July 1, 1994
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NAS 1.15:109141
NASA-TM-109141
Report Number: NAS 1.15:109141
Report Number: NASA-TM-109141
Accession Number
94N37455
Funding Number(s)
PROJECT: RTOP 232-01-04-04
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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