In Part I of this paper, a system of shear constitutive relations was proposed for a first-order shear deformation theory of laminated anisotropic plates and shells. For laminated anisotropic structures, these shear constitutive equations involved the concept of generalized shear planes. Herein, an extensive parametric study is presented to assess the modeling capability of these shear constitutive relations in a class of laminated composite and sandwich cylinders. Classical theory results are also given in order to fully understand the influence of anisotropy on the accuracy and ranges of validity of both first-order shear deformation theory and classical theory. It is seen that the proposed system of shear constitutive relations provides highly accurate frequency results over the range of anisotropy considered.
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June 1992
Research Papers
Shear Constitutive Relations for Laminated Anisotropic Shells and Plates: Part II—Vibrations of Composite Cylinders
C. K. Chun,
C. K. Chun
Civil Engineering Department, University of California, Los Angeles, CA 90024
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S. B. Dong
S. B. Dong
Civil Engineering Department, University of California, Los Angeles, CA 90024
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C. K. Chun
Civil Engineering Department, University of California, Los Angeles, CA 90024
S. B. Dong
Civil Engineering Department, University of California, Los Angeles, CA 90024
J. Appl. Mech. Jun 1992, 59(2): 380-389 (10 pages)
Published Online: June 1, 1992
Article history
Received:
December 12, 1990
Revised:
May 20, 1991
Online:
March 31, 2008
Connected Content
This is a companion to:
Shear Constitutive Relations for Laminated Anisotropic Shells and Plates: Part I—Methodology
Citation
Chun, C. K., and Dong, S. B. (June 1, 1992). "Shear Constitutive Relations for Laminated Anisotropic Shells and Plates: Part II—Vibrations of Composite Cylinders." ASME. J. Appl. Mech. June 1992; 59(2): 380–389. https://doi.org/10.1115/1.2899531
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