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Volumn 56, Issue , 2013, Pages 95-105

Fatigue behavior of the aeronautical Al-Li (2198) aluminum alloy under constant amplitude loading

Author keywords

Aluminum alloys; Constant amplitude fatigue; Fracture; Specific properties; Tensile properties

Indexed keywords

ALUMINUM; FATIGUE OF MATERIALS; FATIGUE TESTING; FRACTURE; HARDENING; STRAIN HARDENING; STRESS-STRAIN CURVES; TENSILE PROPERTIES; TENSILE STRENGTH; YIELD STRESS;

EID: 84884902955     PISSN: 01421123     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.ijfatigue.2013.07.009     Document Type: Article
Times cited : (105)

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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.