INFLUENCE OF CONSTITUENT PARTICLES ON FATIGUE CRACK PROPAGATION IN ALUMINUM ALLOYS,
Abstract
The fracture surfaces of two controlled chemistry 7178 aluminum alloys, containing a volume fraction of inclusions of 0.38% and 4.78%, were studied by electron microscopy. Local crack propagation in the matrix, as determined by measurement of spacing of crack arrest lines, was observed to be slower than the overall crack growth. This difference is shown to be due to extensive cracking of brittle second phase particles ahead of the main crack. The extent of this cracking is shown to depend on the size of the plastic zone at the crack tip and interparticle spacing. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Sep 01, 1963
- Accession Number
- AD0423026
Entities
People
- Regis M. N. Pelloux
Organizations
- Boeing