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Transonic Flutter Investigation of Models of the Sweptback Wing of a Fighter AirplaneTransonic flutter characteristics of sweptback fighter airplane wing models
Document ID
19660027826
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Research Memorandum
Authors
Boswinkle, R. W., Jr. (NASA Langley Research Center Hampton, VA, United States)
Smith, S. L., III (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
April 15, 1958
Subject Category
Aerodynamics
Report/Patent Number
NACA-RM-L58A15
Report Number: NACA-RM-L58A15
Accession Number
66N37116
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
FIGHTER AIRCRAFT
TRANSONIC FLUTTER
SWEPTBACK WING

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