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) |
|---|---|
| Pages (from-to) | 143-164 |
| Number of pages | 22 |
| Journal | ASTM Special Technical Publication |
| State | Published - Jan 1 1972 |
| Event | ASTM Spec Tech Publ 521 1973 - San Antonio, TX, USA Duration: Apr 12 1972 → Apr 13 1972 |
ASJC Scopus subject areas
- Engineering(all)