Fatigue cracks in a thermal barrier coating system on a superalloy in multiaxial thermomechanical testing

International Journal of Fatigue

Volumn 30, Issue 2, 2008, Pages 211-218

  Bartsch, Marion ^a   Baufeld, Bernd ^b   Dalkilic S ^c   Chernova, L ^a   Heinzelmann, Michael ^d  

^a GERMAN AEROSPACE CENTER DLR   (Germany)

^b UNIVERSITY OF LEUVEN   (Belgium)

^c ANADOLU UNIVERSITY   (Turkey)

^d BONN RHEIN SIEG UNIVERSITY OF APPLIED SCIENCES   (Germany)

Author keywords

Crack formation; Fatigue crack growth; Gas turbines; Stress analysis; Thermomechanical fatigue cycling

Indexed keywords

CRACK INITIATION; FATIGUE CRACK PROPAGATION; FATIGUE OF MATERIALS; FINITE ELEMENT METHOD; GAS TURBINES; NICKEL; STRESS ANALYSIS; THERMAL BARRIER COATINGS; THERMAL GRADIENTS; THERMOMECHANICAL TREATMENT;

LOCAL STRESS DISTRIBUTION; MULTIAXIAL STRESSES; THERMOMECHANICAL FATIGUE/CYCLING; THERMOMECHANICAL TESTING;

SUPERALLOYS;

EID: 35648981112     PISSN: 01421123     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.ijfatigue.2007.01.037     Document Type: Article

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