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Flutter studies of simplified component models of a variable-sweep-wing airplane at Mach numbers up to 3.0Wind tunnel flutter analysis of simplified component models of variable-sweep-wing airplane at Mach numbers up to 3
Document ID
19660021918
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Abel, I. (NASA Langley Research Center Hampton, VA, United States)
Ruhlin, C. L. (NASA Langley Research Center Hampton, VA, United States)
Sanford, M. C. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
July 1, 1966
Subject Category
Aerodynamics
Report/Patent Number
NASA-TN-D-3501
Report Number: NASA-TN-D-3501
Accession Number
66N31208
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
SWEPTBACK WING
FLUTTER ANALYSIS
VARIABLE SWEEP
SUPERSONIC WIND TUNNEL

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