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

Wyss, John A Sorenson, Robert M
naca-rm-a51j10
December 21, 1951


No Abstract Available

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http://naca.central.cranfield.ac.uk/reports/1951/naca-rm-a51j10.pdf