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A model for fatigue crack propagation
Authors:Stephen D. Antolovich   A. Saxena  Govind R. Chanani
Affiliation:

Department of Materials Science and Metallurgical Engineering, University of Cincinnati, Cincinnati, OH 45221, U.S.A.

Aircraft Division, Northrop Corp., Hawthorne, CA 90250, U.S.A.

Abstract:A model for fatigue crack propagation is presented which incorporates low cycle fatigue, mechanical properties and a microstructurally-associated process zone. Comparison of the model to published date for 4340 (hard and soft), a series of TRIP steels, Ti-6A1-4V, 2024-T6 and 300 grade maraging steel shows good agreement.
Keywords:
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