Effect of laser shock processing on the mechanical properties and fatigue lives of the turbojet engine blades manufactured by LY2 aluminum alloy
- 19 July 2008
- journal article
- Published by Elsevier BV in Materials & Design (1980-2015)
- Vol. 30 (5), 1697-1703
- https://doi.org/10.1016/j.matdes.2008.07.017
Abstract
No abstract availableKeywords
This publication has 26 references indexed in Scilit:
- Geometrical effects on residual stresses in 7050-T7451 aluminum alloy rods subject to laser shock peeningJournal of the American Academy of Dermatology, 2007
- A Design Methodology to Take Credit for Residual Stresses in Fatigue Limited DesignsJournal of ASTM International, 2005
- The Effect of Fatigue on Residual Peening Stresses in Aerospace ComponentsMaterials Science Forum, 2005
- Effect of laser shock processing on fatigue crack growth and fracture toughness of 6061-T6 aluminum alloyMaterials Science and Engineering: A, 2004
- An approach for prediction of fatigue strength of shot peened componentsEngineering Fracture Mechanics, 2004
- Prediction of fatigue performance in gas turbine blades after foreign object damageInternational Journal of Fatigue, 2003
- Numerical prediction of plastic deformation and residual stresses induced by laser shock processingJournal of the American Academy of Dermatology, 2003
- Laser shock processing and its effects on microstructure and properties of metal alloys: a reviewInternational Journal of Fatigue, 2002
- Laser shock processing of 2024-T62 aluminum alloyMaterials Science and Engineering: A, 1998
- Compressive residual stress introduced by shot peeningJournal of the American Academy of Dermatology, 1998