Some Wind-Tunnel Results of an Investigation of the Flutter of Sweptback- and Triangular-Wing Models at Mach Number 1.3

Author: Tuovila, W. J.
Year: 1952
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-L52C13
Link: https://digital.library.unt.edu/ark:/67531/metadc59218/

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