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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