Failure Mechanisms of Composite Structures
Abstract
This report contains details of technical work accomplished and results obtained in Prediction of Failure Mechanisms and Repair of Damages of Composite Aircraft Structures. This report contains detailed results of the following completed research works: (1) Mixed-Mode Fracture of Notched Unidirectional and Off-Axis Laminates under Tensile Loading. (2) Thermo-Elastic Model for Multidirectional Coated Fiber Composites: Traction Formulation. (3) Constrained Matrix Cracking. Keywords: Composite structure; Composite laminate; Graphite epoxy composites; Failure mechanisms; Failure prediction; Mechanical properties.
Document Details
- Document Type
- Technical Report
- Publication Date
- Sep 01, 1989
- Accession Number
- ADA217193
Entities
People
- Barbara Woolsey
- G. P. Tandon
- L. Roundy
- Lisa Wilson
- S. C. Tan
- S. R. Soni
- T. Hsiao