Nonlinear Transient Response of Thermally Loaded Laminated Panels1-Reference-Cited by-同舟云学术

Nonlinear Transient Response of Thermally Loaded Laminated Panels1

Published:2004-01-01 Issue:1 Volume:71 Page:49-56
ISSN:0021-8936
Container-title:Journal of Applied Mechanics
language:en
Short-container-title:

Author:

Oguamanam D. C. D.¹,Hansen J. S.²,Heppler G. R.³

Affiliation:

1. Department of Mechanical and Industrial Engineering, Ryerson University, Toronto, ON M5B 2K3, Canada

2. Institute for Aerospace Studies, University of Toronto, 4925 Dufferin Street, Toronto, ON M3H 5T6, Canada

3. Systems Design Engineering, University of Waterloo, Waterloo, ON N2L 3G1, Canada

Abstract

The nonlinear response of a composite laminated panel that is suddenly exposed to a heat flux is examined using the finite element method. The panel is cantilevered onto a rigid hub, the rotation motion of which is either fully or partially restrained. The panel elastic deformations are assumed large and are modeled via the von Ka´rma´n strain-displacement relationship while the rigid-body angular rotation, for the case of a rotating rigid hub, is assumed small. The system of nonlinear governing equations is solved by the Newton-Raphson method in conjunction with the Newmark time integration scheme. The panel deformation is observed to be sensitive to the motion of the base.

Publisher

ASME International

Subject

Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics

Link

http://asmedigitalcollection.asme.org/appliedmechanics/article-pdf/71/1/49/5471076/49_1.pdf

Reference14 articles.

1. Tauchert, T. R. , 1991, “Thermally Induced Flexure, Buckling, and Vibration of Plates,” Appl. Mech. Rev., 44(8), pp. 347–360.

2. Thornton, E. A. , 1992, “Thermal Structures: Four Decades of Progress,” J. Aircr., 29(3), pp. 485–498.

3. Heppler, G. R., 1986, “On the Analysis of Shell Structures Subjected to a Blast Environment: A Finite Element Approach,” University of Toronto Institute for Aerospace Studies Report No. 302, Feb.

4. Chandrashekhara, K., and Tenneti, R., 1994, “Non-linear Static and Dynamic Analysis of Heated Laminated Plates: A Finite Element Approach,” Compos. Technol., 51, pp. 85–94.

5. Chang, J-S. C., and Shyong, J-W., 1994, “Thermally Induced Vibration of Laminated Circular Cylinderical Shell Panels,” Compos. Technol., 51, pp. 419–427.

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