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Volumn 27, Issue 6, 2005, Pages 629-638

A 'unified' and a (ΔK+·Kmax) 1/2 crack growth models for aluminum 2024-T351

Author keywords

Aluminum 2024 T351 alloy; Fatigue crack growth; Fracture mechanics; Unified approach

Indexed keywords

ALUMINUM ALLOYS; CIVIL ENGINEERING; CRACKS; FRACTURE MECHANICS; STRESS INTENSITY FACTORS; STRESSES; STRUCTURAL DESIGN;

EID: 14544281101     PISSN: 01421123     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.ijfatigue.2004.12.002     Document Type: Article
Times cited : (27)

References (26)
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.