Size effect on the fatigue crack growth rate threshold of alloy 718

ASTM Special Technical Publication

Volumn , Issue 1372, 2000, Pages 155-174

  Garr, K R ^a   Hresko III, G C ^b  

^a BOEING COMPANY   (United States)

^b Fracture System Research   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AGE HARDENING; ANNEALING; CRACK PROPAGATION; FATIGUE TESTING; NICKEL ALLOYS; STRESS ANALYSIS; SUPERALLOYS;

ALLOY 718; BIAXIALITY RATIO; CRACK CLOSURE; FATIGUE THRESHOLD;

FATIGUE OF MATERIALS;

EID: 0033888831     PISSN: 10403094     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (21)

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