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Aerodynamic data on large semispan tilting wing with 0.5-diameter chord, single-slotted flap, and single propeller 0.19 chord below wingWind tunnel tests to determine longitudinal aerodynamic characteristics of large scale semispan V/STOL tilt-wing configuration with single propeller
Document ID
19670014464
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Fink, M. P. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
April 1, 1967
Subject Category
Aerodynamics
Report/Patent Number
NASA-TN-D-3884
Report Number: NASA-TN-D-3884
Accession Number
67N23793
Funding Number(s)
CONTRACT_GRANT: 721-01-00-11-23
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
V/STOL AIRCRAFT
LONGITUDINAL STABILITY AND CONTROL
TILT-WING AIRCRAFT
WIND TUNNEL

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