Effect of Residual Stresses on Fatigue Crack Growth Rates in Weldments of Aluminum Alloy 5456 Plate
- 1 January 1982
- book chapter
- Published by ASTM International
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- Experimental results on fatigue crack closure for two aluminum alloysEngineering Fracture Mechanics, 1979
- Fracture Toughness and Fatigue Properties of 5083-0 Plate and 5183 Welds for Liquefied Natural Gas ApplicationsPublished by ASTM International ,1975
- The Significance of Fatigue Crack ClosurePublished by ASTM International ,1971