Cumulative-damage modeling of fatigue crack growth in turbine engine materials
- 1 January 1985
- journal article
- Published by Elsevier in Engineering Fracture Mechanics
- Vol. 22 (4) , 713-730
- https://doi.org/10.1016/0013-7944(85)90134-1
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- Evaluation of cumulative damage models for fatigue crack growth in an aircraft engine alloyJournal of Propulsion and Power, 1985
- The effect of environment on the creep crack growth behavior several structural alloysMaterials Science and Engineering, 1980
- AN INVESTIGATION OF THE CREEP‐FATIGUE‐ENVIRONMENT INTERACTION IN A Ni‐BASE SUPERALLOYFatigue & Fracture of Engineering Materials & Structures, 1979