Failure analysis for composite laminates
- 14 May 1984
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- Strength Predictions of Composite Laminates with Unloaded Fastener HolesAIAA Journal, 1980
- Application of the Cubic Polynomial Strength Criterion to the Failure Analysis of Composite MaterialsJournal of Composite Materials, 1980
- Evaluation of the Tensor Polynomial Failure Criterion for Composite MaterialsJournal of Composite Materials, 1978
- Fatigue failure of angle ply laminatesAIAA Journal, 1976
- A Fatigue Failure Criterion for Fiber Reinforced MaterialsJournal of Composite Materials, 1973
- A General Theory of Strength for Anisotropic MaterialsJournal of Composite Materials, 1971