Comparative Study of Corrosion-Fatigue in Aircraft Materials
- 1 February 2001
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 39 (2), 325-330
- https://doi.org/10.2514/2.1308
Abstract
No abstract availableThis publication has 11 references indexed in Scilit:
- Probabilistic Approach to Predicting Fatigue Lives of Corroded 2024-T3AIAA Journal, 1999
- Technical note High‐cycle fatigue crack initiation and propagation behaviour of high‐strength sprin steel wiresFatigue & Fracture of Engineering Materials & Structures, 1999
- Probabilities of occurrence and detection of damage in airframe materialsFatigue & Fracture of Engineering Materials & Structures, 1999
- Effect of pitting corrosion on fatigue crack initiation and fatigue lifeEngineering Fracture Mechanics, 1999
- A transmission electron microscopy study of constituent-particle-induced corrosion in 7075-T6 and 2024-T3 aluminum alloysMetallurgical and Materials Transactions A, 1998
- A probability model for the growth of corrosion pits in aluminum alloys induced by constituent particlesEngineering Fracture Mechanics, 1998
- Probability approach for prediction of corrosion and corrosion fatigue lifeAIAA Journal, 1994
- A Theory of Fatigue Crack Initiation in SolidsJournal of Applied Mechanics, 1990
- Micropitting in Rolling and Sliding Contact Under Mixed LubricationJournal of Tribology, 1989
- Prediction of Fatigue Crack Initiation Life Based on Pit GrowthCorrosion, 1989