High-Cycle Fatigue and Time-Dependent Failure in Metallic Alloys for Propulsion Systems
Abstract
The objective of the AFOSR-Multidisciplinary Research Initiative on High-Cycle Fatigue has been to characterize and performed physically-based modeling of the limiting damage states at the onset of high-cycle fatigue failure in blade and disk components in gas-turbine aircraft engines. The intent has been to facilitate mechanistic understanding as a basis for improved life prediction of such engine components. Efforts were focused on defining: (1) the fatigue thresholds for high-cycle fatigue, specifically involving small crack and mixed-mode effects, and (2) the influence of foreign object damage (FOD) on such thresholds and on the subsequent life, and the role of fretting and fretting fatigue, in a Ti-6Al-4V blade alloy and a polycrystalline Ni-base disk alloy.
Document Details
- Document Type
- Technical Report
- Publication Date
- May 01, 2002
- Accession Number
- ADA405144
Entities
People
- J. W. Hutchinson
- Robert O. Ritchie
- S. Suresh
- W. W. Milligan
Organizations
- University of California, Berkeley