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Wind-tunnel force and flow visualization data at Mach numbers from 1.6 to 4.63 for a series of bodies of revolution at angles of attack from minus 4 deg to 60 degFlow visualization and force data for a series of six bodies of revolution are presented without analysis. The data were obtained in the Langley Unitary Plan wind tunnel for angles of attack from -4 deg to 60 deg. The Reynolds number used for these tests was 6,600,000 per meter.
Document ID
19790013871
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Landrum, E. J. (NASA Langley Research Center Hampton, VA, United States)
Babb, C. D. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 3, 2013
Publication Date
March 1, 1979
Subject Category
Aerodynamics
Report/Patent Number
L-12639
NASA-TM-78813
Accession Number
79N22042
Funding Number(s)
PROJECT: RTOP 505-11-23-04
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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