Free Vibration of Continuous Skin-Stringer Panels

[+] Author and Article Information
Y. K. Lin

University of Illinois, Urbana, Ill.

J. Appl. Mech 27(4), 669-676 (Dec 01, 1960) (8 pages) doi:10.1115/1.3644080 History: Received June 11, 1959; Online September 16, 2011


The determination of the natural frequencies and normal modes of vibration for continuous panels, representing more or less typical fuselage skin-panel construction for modern airplanes, is discussed in this paper. The time-dependent boundary conditions at the supporting stringers are considered. A numerical example is presented, and analytical results for a particular structural configuration agree favorably with available experimental measurements.

Copyright © 1960 by ASME
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