Effect of orthotropic properties and panel width on the compression strength of graphite-epoxy laminates with holes
- 10 May 1982
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- Postbuckling and failure characteristics of selected flat rectangular graphite-epoxy plates loaded in compressionPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1981
- Strength predictions of composite laminates with unloaded fastener holesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1979
- Applications of the Average Stress Failure Criterion: Part II — CompressionJournal of Composite Materials, 1979
- Applications of the Average Stress Failure Criterion: Part I — TensionJournal of Composite Materials, 1978
- Stress Fracture Criteria for Laminated Composites Containing Stress ConcentrationsJournal of Composite Materials, 1974
- Macroscopic Fracture Mechanics of Advanced Composite MaterialsJournal of Composite Materials, 1971