Uncertain eigenvalue problem of linear vibration is analyzed by means of the stochastic finite element method, the basis of which utilizes mean-centered second order perturbation technique. Attention is paid to the fluctuation of the stacking sequence, that is, fiber orientation and layer thickness of FRP laminated plates. The stacking sequence is expressed in terms of probabilistic variables. The eigenvalue problem is formulated based on the Kirchhoff-Love’s theory of thin plate, the stretching, coupled and bending stiffnesses of which are uncertain due to the stacking sequence. The numerical analyses deal with the vibration of simply-supported graphite/epoxy plates. The sensitivity of the input stacking sequence and the correlation coefficients of the probabilistic variables are evaluated quantitatively.
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February 1987
This article was originally published in
Journal of Engineering for Industry
Research Papers
Uncertain Eigenvalue Analysis of Composite Laminated Plates by the Stochastic Finite Element Method
S. Nakagiri,
S. Nakagiri
Institute of Industrial Science, University of Tokyo, Tokyo, Japan
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H. Takabatake,
H. Takabatake
Takamatsu Technical College, Kagawa, Japan
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S. Tani
S. Tani
Mitsubishi Electric Corporation, Tokyo, Japan
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S. Nakagiri
Institute of Industrial Science, University of Tokyo, Tokyo, Japan
H. Takabatake
Takamatsu Technical College, Kagawa, Japan
S. Tani
Mitsubishi Electric Corporation, Tokyo, Japan
J. Eng. Ind. Feb 1987, 109(1): 9-12
Published Online: February 1, 1987
Article history
Received:
April 1, 1986
Online:
July 30, 2009
Citation
Nakagiri, S., Takabatake, H., and Tani, S. (February 1, 1987). "Uncertain Eigenvalue Analysis of Composite Laminated Plates by the Stochastic Finite Element Method." ASME. J. Eng. Ind. February 1987; 109(1): 9–12. https://doi.org/10.1115/1.3187096
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