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LONGITUDINAL STABILITY AND CONTROL OF A TILT-WING VTOL AIRCRAFT WITH RIGID AND FLAPPING PROPELLER BLADESLongitudinal stability and control of a tilt-wing vtol aircraft model with rigid and flapping propeller blades
Document ID
19620003850
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Tosti, L. P. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
July 1, 1962
Subject Category
Space Vehicles
Report/Patent Number
NASA-TN-D-1365
Report Number: NASA-TN-D-1365
Accession Number
62N13850
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
WING
LONGITUDINAL STABILITY AND CONTROL
PROPELLER BLADE
VTOL AIRCRAFT
TILT-WING AIRCRAFT

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