MATERIALS - 7075-T6 ALUMINUM ALLOY - CUMULATIVE DAMAGE EFFECTS - INVESTIGATION OF -.
Abstract
The S-Ncurves and the results of various multiple loadings on individual specimens from a single plate of 7075-T6 aluminum alloy are presented as empirical data for the evaluation of methods of cumulative fatigue damage assessment. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Jan 15, 1964
- Accession Number
- AD0430152
Entities
Organizations
- General Dynamics