Application of Low Plasticity Burnishing to Improve Damage Tolerance of a Ti-6Al-4V First Stage Fan Blades
- 7 April 2003
- conference paper
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 1 reference indexed in Scilit:
- A Test Procedure for Determining the Influence of Stress Ratio on Fatigue Crack GrowthJournal of Testing and Evaluation, 1974