EFFECT OF NUMBER OF LAYERS ON THE NON-DIMENSIONAL BUCKLING FACTOR FOR SYMMETRIC CROSS-PLY SQUARE PLATES

  • Unique Paper ID: 177009
  • Volume: 2
  • Issue: 8
  • PageNo: 133-138
  • Abstract:
  • In order to offer a precise solution for the buckling of simply supported symmetrical cross-ply composite square plates that are subjected to a linearly variable edge stress, the objective of this article is to provide a solution that will provide a solution. The purpose of this essay is to provide a solution to the problem. During the process of its creation, the theory of shear deformation of the first order served as the foundation for its application. It was used on laminated plates that had a thickness that was relatively modest. With the help of this inquiry, we will be able to determine the buckling loads of cross-ply square plates that have a range of aspect ratios that are different from one another. Furthermore, the effects of varying the intensity of the load as well as the arrangement of the layup on the buckling load are explored. This is done in addition to the previous point. The computer is equipped with a piece of software known as ABAQUS, which is used in order to accomplish the goal of guaranteeing that the findings are correct.

Cite This Article

  • ISSN: 2349-6002
  • Volume: 2
  • Issue: 8
  • PageNo: 133-138

EFFECT OF NUMBER OF LAYERS ON THE NON-DIMENSIONAL BUCKLING FACTOR FOR SYMMETRIC CROSS-PLY SQUARE PLATES

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