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- W2146398404 abstract "A major potential advantage claimed for fibrous composite materials in structural applications is that the material can be tailored by proper orientation of the fibers in the various layers so as to optimize the desired structural behavior. Yet the very nature of fibrous composites with their anisotropic elastic behavior has kept such optimal tailoring beyond the reach of most design engineers. In comparison to the numerous analyses available in the literature on buckling of anisotropic plates, very few optimal-design syntheses have been published for this problem. In 1960, Gerard (1) gave a synthesis for uniaxially compressed structurally orthotropic plates, but it was devoted only to longitudinally, transversely, or grid stiffened plates. For composite-material plates, Rothwell (2) presented a crude synthesis using netting analysis for the composite layers. Such an analysis completely neglects the contribution of the matrix material and is known to be in considerable disagreement with experimental results for laminated composite-material plates (3). Recently Hayashi (4) synthesized for maximum uniaxial buckling load in both symmetric cross-ply and symmetric angle-ply plates. However, his synthesis was based on the treatment of the number of axial half waves as a continuous rather than discrete variable. The present synthesis considers both symmetric and unsymmetric laminates subjected to uniaxial compressive loading parallel to two of the plate edges." @default.
- W2146398404 created "2016-06-24" @default.
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- W2146398404 date "1976-02-10" @default.
- W2146398404 modified "2023-09-24" @default.
- W2146398404 title "Design of Composite-Material Plates for Maximum Uniaxial Compressive Buckling Load" @default.
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