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On the effect of subsonic trailing edges on damping in roll and pitch of thin sweptback wings in a supersonic stream
Document ID
19930082764
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Ribner, Herbert Spencer
Date Acquired
August 16, 2013
Publication Date
August 1, 1950
Report/Patent Number
NACA-TN-2146
Report Number: NACA-TN-2146
Accession Number
93R12054
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
DAMPING IN ROLL
THEORIES - FLOW
SUPERSONIC
LINEAR
CONICAL
THEORIES - WINGS
DAMPING IN PITCH
WINGS, SWEPTBACK - STABILITY
THEORIES - FLOW
WINGS - TRAILING EDGES

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