NASA NTRS · 19910051739
Free vibrations of thin-walled semicircular graphite-epoxy composite frames
Abstract
A detailed study is made of the effects of variations in lamination and material parameters of thin-walled composite frames on their vibrational characteristics. The structures considered are semicircular thin-walled frames with I and J sections. The flanges and webs of the frames are modeled by using two-dimensional shell and plate finite elements. A mixed formulation is used with the fundamental unknowns consisting of both the generalized displacements and stress resultants in the frame. The frequencies and modes predicted by the two-dimensional finite-element model are compared with those obtained from experiments, as well as with the predictions of a one-dimensional, thin-walled-beam, finite-element model. A detailed study is made of the sensitivity of the vibrational response to variations in the fiber orientation, material properties of the individual layers, and boundary conditions.
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Noor, Ahmed K., Carden, Huey D., Peters, Jeanne M.. 1991-04-01. Free vibrations of thin-walled semicircular graphite-epoxy composite frames. https://ntrs.nasa.gov/citations/19910051739
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