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Aerodynamic damping and oscillatory stability in pitch for a model of a typical subsonic jet-transport airplaneAerodynamic damping and oscillatory stability in pitch for model of typical swept wing subsonic jet transport
Document ID
19660005466
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Brower, M. L. (NASA Langley Research Center Hampton, VA, United States)
Wright, B. R. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
January 1, 1966
Subject Category
Aerodynamics
Report/Patent Number
NASA-TN-D-3159
Report Number: NASA-TN-D-3159
Accession Number
66N14755
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
SWEPT WING
JET TRANSPORT
PITCH CONTROL
DAMPING
STABILITY
SUBSONIC AIRCRAFT

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