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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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