A mechanism governing oxidation-assisted low-cycle fatigue of superalloys

Acta Materialia

Volumn 57, Issue 10, 2009, Pages 2969-2983

  Evans, A G ^a   He, M Y ^a   Suzuki, A ^b   Gigliotti, M ^b   Hazel, B ^c   Pollock, T M ^d  

^a University of California   (United States)

^b GE GLOBAL RESEARCH   (United States)

^c GE AVIATION   (United States)

^d UNIVERSITY OF MICHIGAN   (United States)

Author keywords

Finite element; Low cycle fatigue; Superalloys; Thermally grown oxide

Indexed keywords

CRACK FRONTS; CRACK GROWTHS; CREEP STRENGTHS; EXPERIMENTAL MEASUREMENTS; FINITE ELEMENT; FINITE ELEMENT SIMULATIONS; GROWTH STRESS; IN PLANES; LOW-CYCLE FATIGUE; STRAIN CYCLES; THERMALLY GROWN OXIDE;

CRACKING (CHEMICAL); CRACKS; CREEP; FINITE ELEMENT METHOD; GROWTH (MATERIALS); OXIDATION; STRAIN RATE; THERMAL BARRIER COATINGS;

SUPERALLOYS;

EID: 65349124816     PISSN: 13596454     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.actamat.2009.02.047     Document Type: Article

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