Influence of applied stress ratio on fatigue crack growth in 6063-T6 aluminium alloy
- 1 January 1985
- journal article
- Published by Elsevier in International Journal of Pressure Vessels and Piping
- Vol. 20 (1) , 65-76
- https://doi.org/10.1016/0308-0161(85)90035-3
Abstract
No abstract availableKeywords
This publication has 5 references indexed in Scilit:
- Some formulas for the crack opening stress levelPublished by Elsevier ,2003
- Crack closure in 2219-T851 aluminum alloyEngineering Fracture Mechanics, 1977
- A study of fatigue crack closure using electric potential and compliance techniquesEngineering Fracture Mechanics, 1977
- Observations of crack closureInternational Journal of Fracture, 1972
- Fatigue crack closure at positive stressesEngineering Fracture Mechanics, 1972