Crack initiation mechanisms during very high cycle fatigue of Ni-based single crystal superalloys at high temperature-Reference-Cited by-同舟云学术

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Crack initiation mechanisms during very high cycle fatigue of Ni-based single crystal superalloys at high temperature

Published:2020-04 Issue: Volume:188 Page:131-144
ISSN:1359-6454
Container-title:Acta Materialia
language:en
Short-container-title:Acta Materialia

Author:

Cervellon A.,Hémery S.,Kürnsteiner P.,Gault B.,Kontis P.,Cormier J.

Funder

Safran Helicopter Engines

Publisher

Elsevier BV

Subject

Metals and Alloys,Polymers and Plastics,Ceramics and Composites,Electronic, Optical and Magnetic Materials

Reference83 articles.

1. Evolution of Ni-based superalloys for single crystal gas turbine blade applications;Caron;Aerosp. Sci. Technol.,1999

2. Nickel-based superalloys for advanced turbine engines: chemistry, microstructure and properties;Pollock;J. Propuls. Power,2006

3. The Superalloys: Fundamentals and Applications;Reed,2008

4. Damage accumulation during creep deformation of a single crystal superalloy at 1150°C;Reed;Mater. Sci. Eng.: A,2007

5. Creep of CMSX-4 superalloy single crystals: effects of misorientation and temperature;Matan;Acta Mater.,1999

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5. Effects of standard heat treatment on micro-to nanostructure heterogeneities in a Rene 65 Ni-based superalloy billet;Materials Science and Engineering: A;2024-10

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