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Aerodynamic data on a large semispan tilting wing with 0.6-diameter chord, fowler flap, and single propeller rotating up at tipLongitudinal aerodynamic characteristics of semispan v/stol tilt-wing configuration with single rotating propeller
Document ID
19640004815
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Fink, M. P. (NASA Langley Research Center Hampton, VA, United States)
Mitchell, R. G. (NASA Langley Research Center Hampton, VA, United States)
White, L. C. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
February 1, 1964
Subject Category
Biosciences
Report/Patent Number
NASA-TN-D-2180
Report Number: NASA-TN-D-2180
Accession Number
64N14729
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
TILT-WING AIRCRAFT
LONGITUDINAL STABILITY AND CONTROL
V/STOL AIRCRAFT

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