Effect of Lamination Scheme on Buckling Load for Laminated Composite Decks Plates

Journal Title: Global Journal of Engineering Sciences - Year 2019, Vol 2, Issue 1

Abstract

New numerical results are generated for in – plane compressive biaxial buckling which serve to quantify the effects of lamination scheme on buckling loading. The results indicate that the symmetric laminate is stiffer than the anti – symmetric one. This phenomenon is caused by coupling between bending and stretching which lowers the buckling loads of symmetric laminate.

Authors and Affiliations

Osama Mohammed Elmardi Suleiman

Keywords

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  • EP ID EP592551
  • DOI 10.33552/GJES.2019.02.000529
  • Views 89
  • Downloads 0

How To Cite

Osama Mohammed Elmardi Suleiman (2019). Effect of Lamination Scheme on Buckling Load for Laminated Composite Decks Plates. Global Journal of Engineering Sciences, 2(1), 1-9. https://europub.co.uk/articles/-A-592551