ON THE NONLINEAR FREE-VIBRATIONS OF CURVED ORTHOTROPIC PANELS

被引:17
作者
RAOUF, RA [1 ]
PALAZOTTO, AN [1 ]
机构
[1] USAF,INST TECHNOL,DEPT AERONAUT & ASTRONAUT,WRIGHT PATTERSON AFB,OH 45433
关键词
D O I
10.1016/0020-7462(94)90019-1
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
This paper studies the non-linear free vibrations of simply supported curved orthotropic panels. The panels are modeled using the Donnell-Mushtari-Vlasov shell relationships. A combination of the Galerkin procedure and the Lindstedt-Poincare perturbation technique is used to construct an approximate solution to the resulting non-linear equations of motion. Algebraic manipulations show that the panel exhibits a non-linear response only when both the involved axial and circumferential modes are axisymmetric. Numerical studies of a Graphite/Epoxy panel show that its response is softening, i.e. the non-linear natural frequency decreases as the amplitude of motion increases. They also show that the lower modes are more non-linear than the higher, mainly flexural modes. The presented results also show that for the studied panels, the non-linear effects are the strongest for shallow, thin, and short panels.
引用
收藏
页码:507 / 514
页数:8
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