Vibrations and buckling of cross-ply nonsymmetric laminated composite beams-Reference-Cited by-同舟云学术

Vibrations and buckling of cross-ply nonsymmetric laminated composite beams

Published:1996-05 Issue:5 Volume:34 Page:1064-1069
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Abramovich H.¹,Eisenberger M.¹,Shulepov O.¹

Affiliation:

1. Technion—Israel Institute of Technology, Haifa 32000, Israel

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.13188

Reference10 articles.

1. Shear deformation and rotary inertia effects of vibrating composite beams

2. Natural frequencies of Timoshenko beams under compressive axial loads

3. Random response of symmetric cross-ply composite beams with arbitrary boundary conditions

4. 4Shulepov, O. "Vibrations of Laminated Beams Using the Dynamic Stiffness Method," M.Sc. Thesis, Faculty of Aerospace Engineering, Technion-Israel Inst. of Technology, Haifa,Israel, Oct. 1993.

5. Derivation of shape functions for an exact 4-D.O.F. Timoshenko beam element

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