Free vibration analysis of anisotropic thin-walled closed-section beams-Reference-Cited by-同舟云学术

Free vibration analysis of anisotropic thin-walled closed-section beams

Published:1995-10 Issue:10 Volume:33 Page:1905-1910
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Armanios Erian A.¹,Badir Ashraf M.²

Affiliation:

1. Georgia Institute of Technology, Atlanta, Georgia 30332-0150

2. Clark Atlanta University, Atlanta, Georgia 30314

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.12744

Reference17 articles.

1. Review of composite rotor blade modeling

2. Pure Bending, Stretching, and Twisting of Anisotropic Cylindrical Shells

3. 4Atilgan, A. R. "Towards A Unified Analysis Methodology For Composite Rotor Blades," Ph.D. Dissertation, School of Aerospace Engineering,Georgia Inst. of Technology, Atlanta,GA, Aug. 1989.

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