Crack progression during sustained-peak low-cycle fatigue in single-crystal Ni-base superalloy rené N5

Metallurgical and Materials Transactions A: Physical Metallurgy and Materials Science

Volumn 41, Issue 4, 2010, Pages 947-956

  Suzuki, A ^a   Gigliotti, M F X ^a   Hazel, B T ^b   Konitzer, D G ^b   Pollock, T M ^c,d  

^a GE GLOBAL RESEARCH   (United States)

^b GE AVIATION   (United States)

^c UNIVERSITY OF MICHIGAN   (United States)

^d University of California   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ALUMINIDES; COATING SURFACE; COATING SYSTEM; CONTROLLED TESTS; CRACK DEPTHS; CRACK LENGTH; CRACK PENETRATION; CRYSTALLOGRAPHIC PLANE; CYCLIC EXPOSURES; INTER-DIFFUSION; LONGITUDINAL SECTION; LOW CYCLE FATIGUES; NI-BASE SUPERALLOYS; RESIDUAL TENSIONS; STRESS AXIS; SUBSTRATE ALLOYS; TEST SPECIMENS; TOTAL STRAIN; VAPOR PHASE;

COATINGS; SUPERALLOYS; UNLOADING;

CRACKS;

EID: 77952369114     PISSN: 10735623     EISSN: None     Source Type: Journal    
DOI: 10.1007/s11661-009-0169-7     Document Type: Conference Paper

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