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Investigation of a semispan tilt-wing VTOL MODEL to determine ground effect on full-span flaps used for yaw control in hoveringHovering force-test on semispan tilt-wing VTOL MODEL to determine ground effect on full-span flaps used for yaw control
Document ID
19660018440
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Grunwald, K. J. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
June 1, 1966
Subject Category
Aircraft
Report/Patent Number
NASA-TN-D-3437
Report Number: NASA-TN-D-3437
Accession Number
66N27730
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
VTOL AIRCRAFT
TILT-WING AIRCRAFT
HOVERING
SEMISPAN MODEL
GROUND EFFECT

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