Affiliation:
1. University of Illinois, Urbana, Ill.
Abstract
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.
Subject
Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics
Cited by
53 articles.
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