High cycle fatigue in aircraft gas turbines—an industry perspective
- 6 April 1996
- journal article
- Published by Springer Nature in International Journal of Fracture
- Vol. 80 (2-3) , 147-163
- https://doi.org/10.1007/bf00012667
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- An assessment of the role of near-threshold crack growth in high-cycle-fatigue life prediction of aerospace titanium alloys under turbine engine spectraInternational Journal of Fracture, 1996
- On the use of the Goodman diagram for high cycle fatigue designInternational Journal of Fracture, 1996
- Damage Tolerance Based Life Prediction in Gas Turbine Engine Blades Under Vibratory High Cycle FatiguePublished by ASME International ,1995
- Life prediction in high temperature environments: Overview of a current gas turbine engine approachMaterials Science and Engineering: A, 1988