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Interference of Wing and Fuselage from Tests of 209 Combinations in the NACA Variable-Density TunnelThis report presents the results of tests of 209 simple wing-fuselage combinations made in the NACA variable-density wind tunnel to provide information regarding the effects of aerodynamic interference between wings and fuselages at a large value of Reynolds number.
Document ID
19930091613
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Jacobs, Eastman N
Ward, Kenneth E
Date Acquired
September 6, 2013
Publication Date
January 1, 1936
Report/Patent Number
NACA-TR-540
Accession Number
93R20903
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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