OVERLOAD RETARDATION IN A STRUCTURAL STEEL
Author:
Publisher
Wiley
Subject
Mechanical Engineering,Mechanics of Materials,General Materials Science
Link
http://onlinelibrary.wiley.com/wol1/doi/10.1111/j.1460-2695.1987.tb00464.x/fullpdf
Reference15 articles.
1. Fatigue crack growth retardation after single-cycle peak overload in Ti-6Al-4V titanium alloy
2. Crack Propagation
3. Micromechanisms of fatigue crack growth retardation following overloads
4. 5. W. Elber (1971 ) Damage Tolerance in Aircraft Structures , ASTM STP 486, pp.230 -242 . American Society for Testing and Materials.
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