Small Crack Growth and Its Influence in Near Alpha-Titanium Alloys
Abstract
Small fatigue cracks are known to propagate at rates much greater than large cracks in the same material at an equivalent crack driving force. The review clarifies the small crack problem and the reasons for its existence. Some recent models, incorporating large scale plasticity, crack closure and microstructural dissimilitude, are introduced. Small crack behaviour in near alphatitanium alloys is examined. Great Britain. (AW)
Document Details
- Document Type
- Technical Report
- Publication Date
- Jun 01, 1989
- Accession Number
- ADA216838
Entities
People
- M. C. Hardy
Organizations
- Royal Aircraft Establishment