On the use of critical distance theories for the prediction of the high cycle fatigue limit stress in notched Ti-6Al-4V

International Journal of Fatigue

Volumn 27, Issue 1, 2005, Pages 45-57

  Lanning, David B ^a   Nicholas, Theodore ^b   Haritos, George K ^c  

^a EMBRY RIDDLE AERONAUTICAL UNIVERSITY   (United States)

^b AIR FORCE INSTITUTE OF TECHNOLOGY   (United States)

^c AUBURN UNIVERSITY   (United States)

Author keywords

Critical distance; High cycle fatigue; Notches; Stress distribution; Titanium alloys

Indexed keywords

FATIGUE OF MATERIALS; FINITE ELEMENT METHOD; NOTCHED BAR TENSILE TESTING; STRESS ANALYSIS; STRESS CONCENTRATION; STRESS RELAXATION;

CRITICAL DISTANCE; HIGH CYCLE FATIGUE (HCF); NOTCHES; STEP-LOADING TECHNIQUES; STRESS DISTRIBUTIONS;

TITANIUM ALLOYS;

EID: 7444265835     PISSN: 01421123     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.ijfatigue.2004.06.002     Document Type: Article

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