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FORCE-TEST INVESTIGATION OF THE STABILITY AND CONTROL CHARACTERISTICS OF A FOUR-PROPELLER TILT-WING VTOL MODEL WITH A PROGRAMED FLAPStability and control characteristics of a four propeller tilt wing vtol model with programmed flap
Document ID
19620005247
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-1389
Report Number: NASA-TN-D-1389
Accession Number
62N15247
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
VTOL AIRCRAFT
STABILITY AND CONTROL
TILT-WING AIRCRAFT
FLAP

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