Dynamic Fracture in 6061-T6 Aluminum
Abstract
Gas gun impact experiments were performed on five thicknesses of 6061-T6 aluminum targets to determine the incipient spall threshold. Data obtained were compared with previous data for the same material obtained by General Motors and other laboratories. Results indicated that batch-to-batch variations in properties of a commercially 'standard' material may cause up to 15 percent differences in spall thresholds for short duration (<0.1 microsecond) shock loads. Four mathematical models of dynamic fracture were evaluated with the spall data obtained. The Hole-Growth model developed by Stanford Research Institute under contract to the Air Force Weapons Laboratory proved superior to the other models considered. This superiority was manifested in the ease of interpretation of the calculated damage levels and the physical significance of the calculations.
Document Details
- Document Type
- Technical Report
- Publication Date
- Jan 01, 1971
- Accession Number
- AD0881534
Entities
People
- James R. Kreer
Organizations
- Air Force Research Laboratory