Stresses Around Partial Contact Pin-Loaded Holes in FRP Composite Plates
- 1 January 1984
- journal article
- Published by SAGE Publications in Journal of Reinforced Plastics and Composites
- Vol. 3 (1), 69-84
- https://doi.org/10.1177/073168448400300104
Abstract
Results of a linear elastic, plane stress finite element investigation of the stress distribution around pin-loaded holes are presented for isotropic as well as several fibre reinforced plastic (FRP) composite materials. The case of full contact (contact angle = 180°) and that of partial contact (contact angle < 180°) between the pin and the hole have been considered. Important conclusions regarding the peak stress distribution around the pin-loaded hole are made specially with respect to the anisotropy (axial to transverse elastic stiffness ratio, E1/E2) introduced in the materials by way of fibre reinforcements and laminating schemes, geometrical parameters (hole diameter to plate width ratio) and the contact angle between the pin and hole.Keywords
This publication has 2 references indexed in Scilit:
- Behavior of Kevlar 49 fabric/epoxy laminates subjected to pin bearing loadsPublished by Office of Scientific and Technical Information (OSTI) ,1977
- The strength of bolted joints in multi-directional cfrp laminatesComposites, 1977