EFFECTS OF SPECIMEN GEOMETRY AND GRAIN STRUCTURE ON STRESS-CORROSION CRACKING BEHAVIOR OF ALUMINUM ALLOYS,
Abstract
Effects of side grooves, grain structure, and thickness on the growth behavior of stress-corrosion cracks in double cantilever beam (DCB) specimens of aluminum alloys are discussed briefly. Problems encountered in testing DCB specimens from aluminum die forgings are also discussed. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Nov 01, 1969
- Accession Number
- AD0709046
Entities
People
- Michael V. Hyatt
Organizations
- Boeing Commercial Airplanes