Modeling the fatigue crack growth behavior of Ti-6Al-4V by considering grain size and stress ratio

Materials Science and Engineering: A

Volumn 528, Issue 18, 2011, Pages 5983-5992

  Oberwinkler, Bernd ^a  

^a UNIVERSITY OF LEOBEN   (Austria)

Author keywords

Fatigue crack growth; Microstructure; Stress ratio; Titanium alloys

Indexed keywords

AEROSPACE APPLICATIONS; ALUMINUM ALLOYS; CRACK CLOSURE; FATIGUE CRACK PROPAGATION; FRACTURE; GRAIN GROWTH; GRAIN SIZE AND SHAPE; MICROSTRUCTURE; SURFACE ROUGHNESS; TERNARY ALLOYS; VANADIUM ALLOYS;

CRACK GROWTH BEHAVIOR; CRACK GROWTH THRESHOLD; CRACKS PROPAGATION; FATIGUE CRACK GROWTH BEHAVIOR; GRAINSIZE; LONG CRACKS; NEAR THRESHOLDS; SIZE RATIO; STRESS RATIO; TITANIUM (ALLOYS);

TITANIUM ALLOYS;

EID: 79956303204     PISSN: 09215093     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.msea.2011.04.046     Document Type: Article

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