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Fatigue Initiation Sites

  • Russell Wanhill
  • Simon Barter
Chapter
Part of the SpringerBriefs in Applied Sciences and Technology book series (BRIEFSAPPLSCIENCES)

Abstract

Figure 3.1 illustrates schematically the reported fatigue crack initiation sites for the three main microstructural categories of near-α and α–β alloys (Wells and Sullivan 1969; Stubbington and Bowen 1974; Eylon and Pierce 1976; Eylon and Hall 1977; Postans and Jeal 1977; Ruppen et al. 1979; Bania et al. 1982; Bolingbroke and King 1986; Wojcik et al. 1988; Dowson et al. 1992; Evans and Bache 1994; Demulsant and Mendez 1995; Lütjering et al. 1996; Wagner 1997; Hines and Lütjering 1999).

Keywords

Fatigue Crack Titanium Nitride High Purity Material Titanium Sponge Progression Marking 
These keywords were added by machine and not by the authors. This process is experimental and the keywords may be updated as the learning algorithm improves.

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Copyright information

© The Author(s) 2012

Authors and Affiliations

  1. 1.Aerospace Vehicles DivisionNational Aerospace Laboratory NLREmmeloordThe Netherlands
  2. 2.Air Vehicle DivisionDSTO Defence Science and Technology OrganisationMelbourneAustralia

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