Flutter calculations in three degrees of freedom
Description:
From Summary: "The present paper is a continuation of the general study of flutter published in NACA reports nos. 496 and 685. The paper is mainly devoted to flutter in three degrees of freedom (bending, torsion, and aileron) for which a number of selected cases have been calculated and presented in graphical form. The results are analyzed and discussed with regard to the effects of structural damping, of fractional-span ailerons, and of mass-balancing. The analysis shows that more emphasis sho…
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Date:
June 7, 1941
Creator:
Theodorsen, Theodore & Garrick, I. E.
Item Type:
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Partner:
UNT Libraries Government Documents Department