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- W2313779716 abstract "A finite element time domain-modal approach is presented for determining the nonlinear flutter characteristics of composite panels at elevated temperatures. The von Karman large-deflection strain-displacement relations, quasi-steady first-order piston theory aerodynamics, and quasi-steady thermal stress theory are used to formulate the nonlinear panel flutter finite element equations of motion in nodal displacements. A set of nonlinear modal equations of motion of much smaller degrees-offreedom for the facilitation in time numerical integration is then obtained through a modal transformation and reduction. All five types of panel behavior: flat, buckled, limit-cycle, periodic and chaotic motions can be determined. Examples show the accuracy, convergence and versatility of the present approach." @default.
- W2313779716 created "2016-06-24" @default.
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- W2313779716 date "1994-04-18" @default.
- W2313779716 modified "2023-10-03" @default.
- W2313779716 title "A finite element time domain - Modal formulation for nonlinear flutter of composite panels at elevated temperatures" @default.
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- W2313779716 doi "https://doi.org/10.2514/6.1994-1424" @default.
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