Effects of modifications to a control surface on a 6-percent-thick unswept wing on the transonic control-surface flutter derivatives

Wyss, John A., Sorenson, Robert M., Gambucci, Bruno J.
naca-rm-a58b04
1958


Flutter derivatives were detemined from pressure-cell measurements on sinusoidally oscillating control surfaces mounted on a wing having an aspect ratio of 3, wing-thickness ratio of 0.06, and taper ratio of 0.6

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