Abstract
The behavior under uniaxial tension of a boron-epoxy composite plate with a circular hole was studied by means of experimental stress analysis and finite-element methods. Strain distributions as a function of applied nominal stress were obtained along the axes of symmetry and around the boundary of the hole. Young's modulus and Poisson's ratio were computed from the far-field strains. Tensile and compressive strain concentrations were computed for the linear range of strain response. Experimental results were compared with those obtained by homogeneous anisotropic elasticity and by finite-element analysis.
Original language | English (US) |
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Pages (from-to) | 143-164 |
Number of pages | 22 |
Journal | ASTM Special Technical Publication |
State | Published - 1972 |
Event | ASTM Spec Tech Publ 521 1973 - San Antonio, TX, USA Duration: Apr 12 1972 → Apr 13 1972 |
ASJC Scopus subject areas
- General Engineering