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Accession Number:
ADA210986
Title:
Fracture and Three Dimensional Stress Analyses of 7075 Aluminum Projectile Components Under Spin and Inertia Load
Descriptive Note:
Final technical rept.
Corporate Author:
ARMY ARMAMENT RESEARCH DEVELOPMENT AND ENGINEERING CENTER WATERVLIET NY BENET LABS
Report Date:
1989-06-01
Pagination or Media Count:
27.0
Abstract:
A fracture case study of a high strength aluminum projectile component subjected to inertial and spin loading during launch from a cannon is presented. A three-dimensional finite element model was used to calculate the projectile stresses and to determine which of the several types of loading was the primary cause of failure. A design change to minimize spin loading resulted in a significantly reduced failure incidence. Mechanical and fracture mechanics tests of the aluminum were performed in order to determine material specifications which could prevent failures in the future. An energy-to-failure test similar to the Charpy test was found to be the most discriminating.
Distribution Statement:
APPROVED FOR PUBLIC RELEASE