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Flight investigation of dynamic stability and control characteristics of a 0.18-scale model of a fan-in-wing VTOL airplaneDynamic stability and control characteristics of 0.18 scale model of fan-in-wing VTOL aircraft
Document ID
19660023651
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Chambers, J. R. (NASA Langley Research Center Hampton, VA, United States)
Kirby, R. H. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
August 1, 1966
Subject Category
Aircraft
Report/Patent Number
NASA-TN-D-3412
Report Number: NASA-TN-D-3412
Accession Number
66N32941
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
FLIGHT TEST
STABILITY AND CONTROL
FAN-IN-WING AIRCRAFT
VTOL AIRCRAFT

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