About this document
تأثیر زوایای ترک بر شکست آلومینیوم by Mohammadreza Tavana is a document available to read on EtoBox.
This document discusses research on fatigue crack growth under combined mode I-III loading. The study examines the effect of initial crack angle (0°, 30°, 45°, 60°) on stress intensity factor (KI, KIII) and J-integral (JI, JIII) values during fatigue crack growth in aluminum alloy sheets with edge cracks under simple tension-compression loading. Results showed that as initial crack angle increases, the effect of mode III increases while mode I decreases, and fatigue crack growth life is extended.
- Author
- Mohammadreza Tavana
- Language
- EN