Effect of bolt load proportioning on the capacity of multiple-bolt composite joints
- 1 February 1988
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 25 (2) , 184-189
- https://doi.org/10.2514/3.45560
Abstract
No abstract availableKeywords
This publication has 15 references indexed in Scilit:
- Stress analysis method for a clearance-fit bolt under bearing loadsAIAA Journal, 1986
- Stresses around holes in pin-loaded orthotropic platesJournal of Aircraft, 1985
- Contact stresses in pin-loaded orthotropic platesInternational Journal of Solids and Structures, 1985
- Failure of Composite Laminates Containing Pin Loaded Holes—Method of SolutionJournal of Composite Materials, 1984
- Strength of Mechanically Fastened Composite JointsJournal of Composite Materials, 1982
- Stress distribution around a single bolt in fibre-reinforced plasticComposites, 1982
- Single- and multiple-bolted joints in orthotropic materialsComposites, 1982
- A Finite Element Analysis of Single and Two-Hole Bolted Joints in Fibre Reinforced PlasticJournal of Composite Materials, 1981
- Failure Analysis of Composite Laminates with a Fastener HolePublished by ASTM International ,1981
- Static Strength Prediction of Bolted Joint in Composite MaterialAIAA Journal, 1980