Effect of three-dimensional loading on macroscopic fretting aspects of an aero-engine blade–disc dovetail interface
Author:
Publisher
Elsevier BV
Subject
Surfaces, Coatings and Films,Surfaces and Interfaces,Mechanical Engineering,Mechanics of Materials
Reference36 articles.
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3. Contact stress distribution in a turbine disc dovetail type joint—a comparison of photo-elastic finite element results;Kenny;Strain,1991
4. A review of analytical aspect of fretting fatigue with extension to damage parameters and application to dovetail joints;Ciavarella;International Journal of Solids and Structure,2001
5. Modeling interfacial conditions in nominally flat contacts for application to fretting fatigue of turbine engine components;McVeigh;International Journal of Fatigue,1999
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