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FLIGHT INVESTIGATION OF THE LONGITUDINAL STABILITY AND CONTROL CHARACTERISTICS OF A FOUR-PROPELLER TILT-WING VTOL MODEL WITH A PROGRAMMED FLAPFlight investigation of the longitudinal stability and control characteristics of a four-propeller tilt-wing vtol model with programmed flap
Document ID
19620005161
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Newsom, W. A., Jr. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
September 1, 1962
Subject Category
Space Vehicles
Report/Patent Number
NASA-TN-D-1390
Report Number: NASA-TN-D-1390
Accession Number
62N15161
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
LONGITUDINAL STABILITY AND CONTROL
AIR
FLAP
TILT-WING AIRCRAFT
VTOL AIRCRAFT
PROPELLER

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