This paper focuses on the formulation of the dynamic problem of laminated composite thick- and thin-walled, single-cell beams of arbitrary cross-section and on the investigation of their associated free vibration behavior. The structural model considered herein incorporates a number of non-classical
β¦ LIBER β¦
Free vibration analysis of anisotropic thin-walled closed-section beams
β Scribed by Armanios, Erian A.; Badir, Ashraf M.
- Book ID
- 120575578
- Publisher
- American Institute of Aeronautics and Astronautics
- Year
- 1995
- Tongue
- English
- Weight
- 619 KB
- Volume
- 33
- Category
- Article
- ISSN
- 0001-1452
- DOI
- 10.2514/3.12744
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