Abstract
A simple approximate solution has been derived for the stress distribution near a circular hole applicable to any orthotropic composite laminate subjected to biaxial loading. The degree of accuracy of this solution was found to be overall acceptable, but strongly dependent upon the laminate lay-up and biaxiality ratio.
| Original language | English |
|---|---|
| Pages (from-to) | 107-111 |
| Number of pages | 4 |
| Journal | Advanced Composites Letters |
| Volume | 5 |
| Issue number | 4 |
| Publication status | Published - 1996 |
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