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• W2163565618 abstract "Numerical methods to investigate the e utter response and aeroelastic stability of plates made of composite materials, wherein microcracking occurs in the matrix material, are presented. The analytical modeling of the modulus reduction due to microcracks is based on a self-consistent method with a two-phase model and yields reduced moduli of the composites as functions of the crack density distribution. Both a e nite difference and a e nite element formulation are presented for two-dimensional laminated plates in supersonic e ow. From the numerical results, it is shown that the microcracking in composites results in a loss of aeroelastic stability through nonlinear bimodular oscillation as well as by a direct reduction in the bending stiffness. For three-dimensional e utter problems, however, reduction in thetorsionalrigidity and changes in elasticcouplings may furtherdecrease the stability." @default.
• W2163565618 created "2016-06-24" @default.
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• W2163565618 date "1998-04-01" @default.
• W2163565618 modified "2023-09-24" @default.
• W2163565618 title "Modeling of Microcrack Damaged Composite Plates Undergoing Nonlinear Bimodular Flutter Oscillations" @default.
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• W2163565618 doi "https://doi.org/10.2514/2.411" @default.
• W2163565618 hasPublicationYear "1998" @default.
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