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Thermally Induced Vibration Analysis of Laminated Plate Considering Radiation by Finite Element Method

Published online by Cambridge University Press:  07 December 2011

S. G. Zhao ,
J. T. Wang ,
K. Li  and
D. F. Wu
S. G. Zhao*
Affiliation:
School of Aeronautic Science and Technology, Beijing University of Aeronautics and Astronautics, Beijing 100191, China
J. T. Wang
Affiliation:
School of Aeronautic Science and Technology, Beijing University of Aeronautics and Astronautics, Beijing 100191, China
K. Li
Affiliation:
Beijing Institute of Control Engineering, Beijing 100080, China
D. F. Wu
Affiliation:
School of Aeronautic Science and Technology, Beijing University of Aeronautics and Astronautics, Beijing 100191, China
*
*Associate Professor, corresponding author
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Abstract

Transient temperature field of laminated plate which considering radiation is analyzed by laying temperature lines in every layer in this paper. Finite element equations are established by using high-order displacement field which considering shear effect based on the temperature analysis. Then thermally induced vibration of laminated plate is investigated by solving the finite element equation with numerical method. Compared with numerical results of ANSYS by using 3-D coupled element (SOLID5), the methods presented in this paper have a satisfied precision and better efficiency. It can give reference to the thermally induced vibration analysis of thin-large flexible laminated appendages of spacecraft.

Keywords

Laminated plateRadiationThermally induced vibrationFEM
Type
Technical Note
Information
Journal of Mechanics , Volume 27 , Issue 4 , December 2011 , pp. N33 - N37
Copyright
Copyright © The Society of Theoretical and Applied Mechanics, R.O.C. 2011

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References

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