Evaluation of cumulative damage models for fatigue crack growth in an aircraft engine alloy
- 1 March 1985
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Propulsion and Power
- Vol. 1 (2) , 131-136
- https://doi.org/10.2514/3.22770
Abstract
No abstract availableThis publication has 0 references indexed in Scilit: