Design of Composite Laminates Containing Pin Loaded Holes
- 1 May 1984
- journal article
- Published by SAGE Publications in Journal of Composite Materials
- Vol. 18 (3) , 279-289
- https://doi.org/10.1177/002199838401800306
Abstract
Methods are presented for sizing composite laminates containing one, two, or several pin loaded holes, the holes being arranged either in a single row or in two parallel rows. It is shown how the design parameters (number of holes, hole diameter, hole positions) can be found, which result in the maximum failure load and in the max imum failure load per unit weight.Keywords
This publication has 1 reference indexed in Scilit:
- Failure of Composite Laminates Containing Pin Loaded Holes—Method of SolutionJournal of Composite Materials, 1984