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Longitudinal stability and control characteristics of a powered model of a twin-propeller deflected-slipstream STOL AIRPLANE configurationLongitudinal stability and control characteristics of powered model of twin-propeller deflected-slipstream STOL aircraft configuration
Document ID
19660021916
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Gentry, G. L. (NASA Langley Research Center Hampton, VA, United States)
Hammond, A. D. (NASA Langley Research Center Hampton, VA, United States)
Margason, R. J. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
July 1, 1966
Subject Category
Aircraft
Report/Patent Number
NASA-TN-D-3438
Report Number: NASA-TN-D-3438
Accession Number
66N31206
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
STOL AIRCRAFT
LONGITUDINAL STABILITY AND CONTROL
PROPELLER SLIPSTREAM

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