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Some aerodynamic considerations related to wind tunnel model surface definitionThe aerodynamic considerations related to model surface definition are examined with particular emphasis in areas of fabrication tolerances, model surface finish, and orifice induced pressure errors. The effect of model surface roughness texture on skin friction is also discussed. It is shown that at a given Reynolds number, any roughness will produce no skin friction penalty.
Document ID
19800023868
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Gloss, B. B.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 4, 2013
Publication Date
September 1, 1980
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NASA-TM-81820
Report Number: NASA-TM-81820
Accession Number
80N32376
Funding Number(s)
PROJECT: RTOP 505-43-23-06
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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