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Flutter Investigation in the High Subsonic and Transonic Speed Range on Cantilever Delta-wing Plan Forms with Leading-edge Sweepback of 60 Degrees, 53 Degrees 8', and 45 Degrees
Document ID
19930089666
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Lauten, William T , Jr
Burgess, Marvin F
Date Acquired
August 16, 2013
Publication Date
January 31, 1957
Report/Patent Number
NACA-RM-L56K26
Report Number: NACA-RM-L56K26
Accession Number
93R18956
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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