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Static and dynamic longitudinal stability derivatives of a powered 1/9-scale model of a tilt-wing V/STOL transportForce tests to determine static and dynamic longitudinal stability derivatives of powered scale model of tilt-wing V/STOL transport aircraft
Document ID
19660027742
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Chambers, J. R. (NASA Langley Research Center Hampton, VA, United States)
Grafton, S. B. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
September 1, 1966
Subject Category
Aircraft
Report/Patent Number
NASA-TN-D-3591
Report Number: NASA-TN-D-3591
Accession Number
66N37032
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
TILT-WING AIRCRAFT
DYNAMIC STABILITY
V/STOL AIRCRAFT
TRANSPORT AIRCRAFT
LONGITUDINAL STABILITY
STATIC STABILITY

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