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Fatigue and Fracture of Engineering Materials and Structures

Volumn 25, Issue 2, 2002, Pages 111-125

Initiation and early growth of fatigue cracks in an aerospace aluminium alloy

(4) Barter, S A a Sharp, P K a Holden, G a Clark, G a

a AERO AND MAR RESEARCH LABORATORY (Australia)

Author keywords

7050 aluminium alloy; Crack closure; Crack growth; EIFS; Fatigue life; Full scale fatigue testing; Initiation; Quantitative fractography; Spectrum fatigue testing

Indexed keywords

AIRCRAFT MATERIALS; CRACK INITIATION; CRACK PROPAGATION; CRACKS; ETCHING; FATIGUE OF MATERIALS; FATIGUE TESTING; FRACTOGRAPHY; GRAIN BOUNDARIES; INCLUSIONS; STRESS CONCENTRATION; STRESS INTENSITY FACTORS;

CRACK CLOSURE; CRACK LENGTH; EQUIVALENT INITIAL FLAW SIZE; EQUIVALENT PRECRACK SIZE; INITIAL CRACK SIZE;

ALUMINUM ALLOYS;

EID: 0036466153 PISSN: 8756758X EISSN: None Source Type: Journal
DOI: 10.1046/j.1460-2695.2002.00482.x Document Type: Article

Times cited : (67)

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