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Aerodynamic data on large semispan tilting wing with 0.4-diameter chord, single-slotted flap, and single propeller 0.22 chord below wingAerodynamic characteristics of large semi-span V/STOL tilt-wing with single propeller tested for modes of propeller rotation
Document ID
19690007980
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
January 1, 1969
Subject Category
Aerodynamics
Report/Patent Number
NASA-TN-D-5016
Report Number: NASA-TN-D-5016
Accession Number
69N17312
Funding Number(s)
CONTRACT_GRANT: 721-01-00-11-23
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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