Crack initiation in an aluminide coated single crystal during thermomechanical fatigue

ASTM Special Technical Publication

Volumn 1263, Issue , 1996, Pages 68-81

  Martínez Esnaola, José M ^a   Arana, María ^a   Bressers, Johan ^b   Timm, Jens ^b   Martín Meizoso, Antonio ^a   Bennett, Andy ^c   Affeldt, Ernst E ^d  

^a CEIT   (Spain)

^b JOINT RESEARCH CENTRE   (Italy)

^c ROLLS ROYCE PLC   (United Kingdom)

^d MTU AERO ENGINES GMBH   (Germany)

Author keywords

Aero engines; Coating; Crack initiation; Single crystal; Superalloy; Surface crack; Thermomechanical fatigue

Indexed keywords

ALUMINUM COMPOUNDS; COATINGS; CRACK INITIATION; FATIGUE OF MATERIALS; FRACTURE MECHANICS; LOADING; MECHANICAL PROPERTIES; NICKEL; SINGLE CRYSTALS; STRAIN; TEMPERATURE; THERMODYNAMIC PROPERTIES;

AERO ENGINES; ALUMINIDE COATINGS; CRACK DENSITY; DUCTILE BRITTLE TRANSITION TEMPERATURE; MULTIPLE THUMBNAIL CRACK ORIGINS; POINT INITIATION; STRESS TEMPERATURE COUPLING; SURFACE CRACK; THERMOMECHANICAL FATIGUE;

SUPERALLOYS;

EID: 0029699378     PISSN: 00660558     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1520/stp16447s     Document Type: Article

References (11)

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