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Rolling stability derivatives of a variable- sweep tactical fighter model at subsonic and transonic speedsRolling stability derivatives of variable sweep tactical fighter aircraft model at subsonic and transonic speeds
Document ID
19670008821
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Gainer, T. G. (NASA Langley Research Center Hampton, VA, United States)
Henderson, W. P. (NASA Langley Research Center Hampton, VA, United States)
Phillips, W. P. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
February 1, 1967
Subject Category
Aircraft
Report/Patent Number
NASA-TN-D-3845
Report Number: NASA-TN-D-3845
Accession Number
67N18150
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
VARIABLE SWEEP
FIGHTER AIRCRAFT
SUBSONIC SPEED
TRANSONIC SPEED
AIRCRAFT STABILITY

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