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Shuttle vertical fin flowfield by the direct simulation Monte Carlo methodThe flow properties in a model flowfield, simulating the shuttle vertical fin, determined using the Direct Simulation Monte Carlo method. The case analyzed corresponds to an orbit height of 225 km with the freestream velocity vector orthogonal to the fin surface. Contour plots of the flowfield distributions of density, temperature, velocity and flow angle are presented. The results also include mean molecular collision frequency (which reaches 1/60 sec near the surface), collision frequency density (approaches 7 x 10 to the 18/cu m sec at the surface) and the mean free path (19 m at the surface).
Document ID
19860003783
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hueser, J. E.
(Old Dominion Univ. United States)
Brock, F. J.
(Old Dominion Univ. United States)
Melfi, L. T.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 12, 2013
Publication Date
September 1, 1985
Publication Information
Publication: NASA. Marshall Space Flight Center 2d Workshop on Spacecraft Glow
Subject Category
Space Sciences (General)
Accession Number
86N13251
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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