Effect of crystal orientation on fatigue failure of single crystal nickel base turbine blade superalloys

Proceedings of the ASME Turbo Expo

Volumn 4, Issue , 2000, Pages

  Arakere, Nagaraj K ^a   Swanson, Gregory ^b  

^a UNIVERSITY OF FLORIDA   (United States)

^b NASA MARSHALL SPACE FLIGHT CENTER   (United States)

Author keywords

Crystal orientation; Fatigue; Single crystal nickel superalloy; Turbine blade

Indexed keywords

ENGINES; FATIGUE OF MATERIALS; FIGHTER AIRCRAFT; GAS TURBINES; NICKEL; NICKEL ALLOYS; OUTAGES; PROPULSION; ROCKET ENGINES; ROCKETS; SINGLE CRYSTALS; SPACECRAFT PROPULSION; SUPERALLOYS; TURBINE COMPONENTS; TURBINE PUMPS; TURBOMACHINE BLADES;

FATIGUE FAILURE CRITERION; NICKEL SUPERALLOY; ROCKET ENGINE TURBOPUMPS; SINGLE CRYSTAL TURBINE BLADES; SINGLE-CRYSTAL MATERIALS; SPACE PROPULSION SYSTEM; THERMO MECHANICAL FATIGUES (TMF); TURBINE BLADE;

CRYSTAL ORIENTATION;

EID: 84955302799     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/1.1413767     Document Type: Conference Paper

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