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An investigation of the control-surface flutter derivatives of an NACA 65(sub 1)-213 airfoil in the Ames 16-foot high-speed wind tunnel
Author:
Wyss, John A.
Year:
1951
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-A51J10
Link:
https://digital.library.unt.edu/ark:/67531/metadc59172/
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