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TECHNICAL PAPERS

Nonlinear Transient Response of Thermally Loaded Laminated Panels

[+] Author and Article Information
D. C. D. Oguamanam

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

J. S. Hansen

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

G. R. Heppler

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

J. Appl. Mech 71(1), 49-56 (Mar 17, 2004) (8 pages) doi:10.1115/1.1631033 History: Received September 18, 2002; Revised May 01, 2003; Online March 17, 2004
Copyright © 2004 by ASME
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References

Tauchert,  T. R., 1991, “Thermally Induced Flexure, Buckling, and Vibration of Plates,” Appl. Mech. Rev., 44(8), pp. 347–360.
Thornton,  E. A., 1992, “Thermal Structures: Four Decades of Progress,” J. Aircr., 29(3), pp. 485–498.
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.
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.
Chang,  J-S. C., and Shyong,  J-W., 1994, “Thermally Induced Vibration of Laminated Circular Cylinderical Shell Panels,” Compos. Technol., 51, pp. 419–427.
Feldman,  E., and Gilat,  R., 1999, “On the Dynamic Response of Metal Matrix Composite Panels to Uniform Temperature Loading,” Compos. Struct., 47(1–4), pp. 619–624.
Librescu,  L., and Lin,  W., 1997, “Vibration of Thermomechanically Loaded Flat and Curved Panels Taking Into Account Geometric Imperfections and Tangential Edge Restraints,” Int. J. Solids Struct., 34(17), pp. 2161–2181.
Johnston,  J. D., and Thornton,  E. A., 1998, “Thermally Induced Attitude Dynamics of a Spacecraft With a Flexible Appendage,” J. Guid. Control Dyn., 21(4), pp. 581–587.
Jones, R. M., 1975, Mechanics of Composite Materials, Scripta Book Company, Washington, DC.
Bathe, K-J., 1996, Finite Element Procedures, Prentice-Hall, Englewood Cliffs, NJ.
Heppler,  G. R., and Hansen,  J. S., 1986, “A Mindlin Element for Thick and Deep Shells,” Comput. Methods Appl. Mech. Eng., 54, pp. 21–47.
Rajeskaran,  S., and Murray,  D. W., 1973, “Incremental Finite Element Matrices,” J. Struct. Div. ASCE, 99(ST12), pp. 2423–2438.
Mallet,  R. H., and Marcal,  P. V., 1968, “Finite Element Analysis of Nonlinear Structures,” J. Struct. Div. ASCE, 94(ST9), pp. 2081–2105.
Mallet,  R. H., and Marcal,  P. V., 1970, closure and errata to “Finite Element Analysis of Nonlinear Structures,” J. Struct. Div. ASCE, 96(ST1), pp. 132–133.

Figures

Grahic Jump Location
Cantilevered cylindrical panel
Grahic Jump Location
Effect of nonlinearity on elastic displacements (0/90/0/90/0)s
Grahic Jump Location
Effect of nonlinearity on hub angular rotation (0/90/0/90/0)s
Grahic Jump Location
Effect of hub inertia on elastic displacements (0/90/0/90/0)s
Grahic Jump Location
Effect of hub inertia on hub angular rotation (0/90/0/90/0)s
Grahic Jump Location
Effect of panel shallowness on elastic displacements (0/90/0/90/0)s
Grahic Jump Location
Effect of panel shallowness on hub angular rotation (0/90/0/90/0)s

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