Acknowledgements

The research reported herein was performed as a part of the research program "Modeling corrosion growth on aircraft structure" for NCI Information Systems, Fairborn, OH, under contract NCI USAF 9138-003 with Mr. Garth Cooke as the program manager. The support of NCI Information Systems in conducting this research is gratefully acknowledged. The authors also would like to thank the University of Utah for use of facilities and encouragement.


Review of Pitting Corrosion Fatigue Models, D.W. Hoeppner, V. Chandrasekaran, and A.M.H. Taylor, University of Utah and FASIDE International Inc.