Fatigue Crack Delay and Arrest Due to Single Peak Tensile Overloads
- 1 March 1974
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 12 (3), 330-335
- https://doi.org/10.2514/3.49229
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- The Significance of Fatigue Crack ClosurePublished by ASTM International ,1971
- The Effect of Load Interaction and Sequence on the Fatigue Behavior of Notched CouponsPublished by ASTM International ,1971
- Stress-Intensity Factors for the Tension of an Eccentrically Cracked StripJournal of Applied Mechanics, 1966
- FATIGUE CRACK PROPAGATION IN LIGHT ALLOY SHEET MATERIAL AND STRUCTURESPublished by Elsevier BV ,1962
- Published by Springer Science and Business Media LLC ,1956