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Equations for the application of wind-tunnel wall corrections to pitching moments caused by the tail of an aircraft modelMathematical expressions derived for application of wind tunnel wall corrections to pitching moments caused by tail of aircraft model
Document ID
19670002485
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Heyson, H. H. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
November 1, 1966
Subject Category
Aerodynamics
Report/Patent Number
NASA-TN-D-3738
Report Number: NASA-TN-D-3738
Accession Number
67N11814
Funding Number(s)
CONTRACT_GRANT: 721-01-00-18-23
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
AIRCRAFT MODEL
WIND TUNNEL WALL
PITCHING MOMENT
TAIL

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