Degradation of residual strength in SCS-6/Ti-15-3 due to fully reversed fatigue

Metallurgical and Materials Transactions A: Physical Metallurgy and Materials Science

Volumn 30, Issue 2, 1999, Pages 307-313

  Calcaterra, J R ^a   Mall, S ^b   Coghlan, S C ^c  

^a AIR FORCE RESEARCH LABORATORY   (United States)

^b Air Force Institute of Technology   (United States)

^c WRIGHT PATTERSON AIR FORCE BASE   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

CERAMIC FIBERS; CERMETS; CRACK INITIATION; FATIGUE OF MATERIALS; FATIGUE TESTING; FIBER REINFORCED METALS; HARDENING; SILICON CARBIDE; STRAIN; STRENGTH OF MATERIALS; TITANIUM ALLOYS; VOLUME FRACTION; DEGRADATION; METALLIC MATRIX COMPOSITES;

RESIDUAL STRENGTH; TITANIUM MATRIX COMPOSITES (TMC); FIBER VOLUME FRACTION; RESIDUAL STRENGTH DEGRADATION;

METALLIC MATRIX COMPOSITES; TITANIUM ALLOYS;

EID: 0033078811     PISSN: 10735623     EISSN: None     Source Type: Journal    
DOI: 10.1007/s11661-999-0319-y     Document Type: Article

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