Flutter analysis of rectangular wings of very low aspect ratio

Robert W. Fralich, John M. Hedgepeth
naca-tn-4245
Jun 1958


A flutter analysis, employing slender-body aerodynamic theory and thin-plate theory, is made for rectangular wings of very low aspect ratio with a constant thickness. The spanwise variation of wing deflection is assumed to be given by a parabola, and the chordwise variation is allowed complete freedom.

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