Hostname: page-component-cd9895bd7-p9bg8 Total loading time: 0 Render date: 2024-12-23T15:36:39.640Z Has data issue: false hasContentIssue false
  • English
  • Français

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
Get access

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

Access options

Get access to the full version of this content by using one of the access options below. (Log in options will check for institutional or personal access. Content may require purchase if you do not have access.)

References

REFERENCES

1.Boley, B. A., “Thermally Induced Vibrations of Beams,” Journal of the Aeronautical Science, 23, pp. 179–181. (1956).Google Scholar
2.Beam, R. M., “On the Phenomenon of Thermoelastic Instability of Booms with Open Cross Section”, NASA, TN D5-222 (1969).Google Scholar
3.Jones, J. P., “Thermoelastic Vibration of a beam,” Journal of the Acoustical Society of America, 39, pp. 542–548 (1966).CrossRefGoogle Scholar
4.Thornton, E. A. and Kim, Y. A., “Thermally Induced Bending Vibrations of a Flexible Rolled-Up Solar Array,” Journal of Spacecraft and Rockets, 30, pp. 438–448 (1993).CrossRefGoogle Scholar
5.Kraus, H., “Thermally Induced Vibrations of Thin Nonshallow Spherical Shells,” AIAA Journal, 4, pp. 500–505 (1966).CrossRefGoogle Scholar
6.Wang, J. T., Zhao, S. E., Li, K. and Liu, Y. W., “Thermally Induced Vibration Analysis of Thin-Walled Beam Considering the Material's Temperature Effect,” International Conference on Experimental Mechanics 2008. Nanjing, China, pp. 232–233 (2008).Google Scholar
7.Mason, J. B., “Analysis of Thermally Induced Structural Vibrations by Finite Element Techniques,” NASA TMX-63488 (1968).Google Scholar
8.Young, D., Xue, M. D., Cheng, L. J. and Hu, N., “Fourier-Finite Element Analysis of Temperature Fields in Space Structures,” Journal of Tsinghua University (Science and Technology), 42, pp. 198–202 (in Chinese, 2002).Google Scholar
9.Cheng, L. J., Xue, M. D., Tang, X. S. and Yao, H. M., “Thermal-Dynamic Analysis of Large Scale Space Structure by FEM,” Chinese Journal of Applied Mechanics, 21, pp. 1000–4939 (in Chinese, 2004).Google Scholar
10.Huan, Y. W., Xue, M. D., Cheng, L. J. and Zhang, Y. F., “Thermally Induced Vibration of Large Space Structure Including Thin-walled Open Beam Sections,” Journal of Tsinghua University (Science and Technology), 45, pp. 262–266 (in Chinese, 2005).Google Scholar
11.Kawamura, R., Tanigawa, Y., Kusuki, S. and Hamamura, H., “Fundamental Thermo-Elasticity Equations for Thermally Induced Flexural Vibration Problems for Inhomogeneous Plates and Thermo-Elastic Dynamical Responses to a Sinusoidally Varying Surface Temperature,” Journal of Engineering Mathematics, 61, pp. 143–160 (2008).CrossRefGoogle Scholar
12.Kumar, R., Mishra, B. K. and Jain, S. C., “Thermally Induced Vibration Control of Cylindrical Shell Using Piezoelectric Sensor and Actuator,” International Journal of Advanced Manufacturing Technology, 38, pp. 551–562 (2008).CrossRefGoogle Scholar
13.Li, J. M., Zhou, X. and Gu, H., “Dyanmics Response of Smart Composites Using a Coupled Thermo-Piezoelectric-Mechanical Model,” AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dyanmics, and Materials Conference and Exhibit, 40th, St. Louis, MO. UNITED STATES, APR. 12-15, pp. 2324–2335 (1999).Google Scholar