Stress-Concentration Factors for Finite Orthotropic Laminates with a Circular Hole and Uniaxial Loading.

Abstract

Stresses were calculated for finite width orthotropic laminates with a circular hole and remote uniaxial loading using a two dimensional finite element analysis with both uniform stress and uniform displacement boundary conditions. Five different laminates were analyzed: quasi-isotropic 0/+/-45/9O deg), 0, 90, 0/90 DEGs, and +/-45 DEG5. Computed results are presented for selected combinations of hole diameter sheet width ratio d/w and length to width ratio L/w. For small L/w values, the stress concentration factors K(tn) were significantly different for the uniform stress and uniform displacement boundary conditions. Typically, for the uniform stress condition, the Ktn values were much larger than for the infinite strip reference condition; however, for the uniform displacement condition, they were only slightly smaller than for this reference. The results for long strips are also presented as width correction factors. For d/w < or = 0.33, these width correction factors are nearly equal for all five laminates.

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Document Details

Document Type
Technical Report
Publication Date
May 01, 1979
Accession Number
ADA304543

Entities

People

  • C. S. Hong
  • John H. Crews Jr.

Organizations

  • Langley Research Center

Tags

DTIC Thesaurus Topics

  • Boundaries
  • Cartesian Coordinates
  • Composite Materials
  • Computer Programs
  • Contrast
  • Department Of Defense
  • Diameters
  • Displacement
  • Epoxy Laminates
  • Finite Element Analysis
  • Laminates
  • Literature
  • Modulus Of Elasticity
  • Shear Modulus
  • Stress Concentration
  • Stresses
  • Two Dimensional

Readers

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