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Aerodynamic data on large semispan tilting wing with 0.5-diameter chord, single-slotted flap, and single propeller 0.08 chord below wingLongitudinal aerodynamic characteristics of large scale semispan V/STOL tilt-wing configuration having single propeller
Document ID
19670025877
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Kink, M. P. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
July 1, 1967
Subject Category
Aerodynamics
Report/Patent Number
NASA-TN-D-4030
Report Number: NASA-TN-D-4030
Accession Number
67N35206
Funding Number(s)
CONTRACT_GRANT: 721-01-00-11-23
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
AERODYNAMIC CHARACTERISTICS
V/STOL AIRCRAFT
LONGITUDINAL STABILITY
TILT-WING AIRCRAFT

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