Steel and Composite Structures

  • 제3권6호
  • /
  • Pages.439-450
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  • 2003
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  • 1229-9367(pISSN)
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  • 1598-6233(eISSN)
테크노프레스 (Techno-Press)
권호 표지
DOI QR코드

DOI QR Code

Buckling and vibration of symmetric laminated composite plates with edges elastically restrained

  • Ashour, Ahmed S. (Faculty of Engineering, International Islamic University Malaysia)
  • Received : 2002.11.18
  • Accepted : 2003.05.15
  • Published : 2003.12.25
⟨ 이전 논문 다음 논문 ⟩

Abstract

The finite strip transition matrix technique, a semi analytical method, is employed to obtain the buckling loads and the natural frequencies of symmetric cross-ply laminated composite plates with edges elastically restrained against both translation and rotation. To illustrate the accuracy and the validation of the method several example of cross play laminated composite plates were analyzed. The buckling loads and the frequency parameters are presented and compared with available results in the literature. The convergence study and the excellent agreement with known results show the reliability of the purposed technique.

Keywords

References

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