Microstructure Dependent Fatigue Cracking Resistance of Ti-6.5Al-3.5Mo-1.5Zr-0.3Si Alloy

Journal of Materials Science and Technology

Volumn 28, Issue 7, 2012, Pages 614-621

  Song, Z M ^a   Lei, L M ^b,c   Zhang, B ^d   Huang, X ^c   Zhang, G P ^a  

^a INSTITUTE OF METAL RESEARCH   (China)

^b AECC COMMERCIAL AIRCRAFT ENGINE CO   (China)

^c BEIJING INSTITUTE OF AERONAUTICAL MATERIALS   (China)

^d NORTHEASTERN UNIVERSITY   (China)

Author keywords

Crack propagation; Fatigue crack initiation; Microstructure; Ti alloy

Indexed keywords

BIMODAL STRUCTURES; COOLING RATES; FATIGUE CRACK INITIATION; FATIGUE CRACKING; FATIGUE CRACKING MECHANISM; FATIGUE CRACKING RESISTANCE; FATIGUE CRACKS; LENGTH SCALE; MARTENSITE LATHS; ROOM TEMPERATURE; TI ALLOYS; TI-6.5AL-3.5MO-1.5ZR-0.3SI;

ALUMINUM; CERIUM ALLOYS; CRACK INITIATION; CRACK PROPAGATION; FATIGUE CRACK PROPAGATION; LAMELLAR STRUCTURES; MICROSTRUCTURE; MOLYBDENUM; SILICON; ZIRCONIUM;

SILICON ALLOYS;

EID: 84864591206     PISSN: 10050302     EISSN: None     Source Type: Journal    
DOI: 10.1016/S1005-0302(12)60106-6     Document Type: Article

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