Fatigue Behavior and Life Prediction of Composite Laminates.
Abstract
This report presents a survey of some of the available data on the effects of fatigue in composite laminates. Both static and fatigue behaviors of unidirectional laminae are discussed in terms of the static failure and fatigue limit strains of the constituents as well as of the loading conditions. Subcritical failure modes in multidirectional laminates are delineated and correlated with the material responses such as temperature increase, modulus change, and fatigue notch insensitivity. Also included are the effects of test frequency and compression. Methods of predicting the fatigue strengths of off-axis laminae and of angle-ply laminates are summarized. Finally, two statistical life prediction models are discussed using the material 'age'. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Apr 01, 1978
- Accession Number
- ADA060548
Entities
People
- H. Thomas Hahn
Organizations
- Air Force Research Laboratory