Comment on "Derivation of Axisymmetric Flexural Vibration Equations of a Cylindrically Aeolotropic Circular Plate"
Author:
Affiliation:
1. Kansas State University, Manhattan, Kansas
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.49888
Reference6 articles.
1. The Bending of the Cylindrically Aeolotropic Plate
2. Conway, H. D. "Note on the Bending of Circular Plates'of Variable Thickness/' Journal of Applied Mechanics, Vol.71, 1949, pp.209-210.
3. Minkarah, I. A. and Hoppmann, W. H., II, "Flexural Vibration of Cylindrically Aeolotropic Circular Plates/7The Journal of the Acoustical Society of America, Vol.36, 1964, pp.470-475.
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1. Asymmetric buckling of layered orthotropic circular and annular plates of varying thickness using a computationally economic semianalytical finite element approach;Computers & Structures;1996-04
2. Buckling of tapered orthotropic circular plates using a computationally economic approach;Computers & Structures;1993-02
3. Vibration of cylindrically orthotropic circular plates.;AIAA Journal;1972-12
4. Nonlinear axisymmetric flexural vibration equations of a cylindrically anisotropic circular plate.;AIAA Journal;1972-10
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