Prediction of corrosion fatigue crack growth rate in alloys. Part I: General corrosion fatigue model for aero-space aluminum alloys

Author:

Kovalov DanyilORCID,Fekete Balázs,Engelhardt George R.,Macdonald Digby D.ORCID

Funder

US Air Force Academy

Corrosion Policy

Oversight office via Scientific Simulation Systems of Dayton, OH

Publisher

Elsevier BV

Subject

General Materials Science,General Chemical Engineering,General Chemistry

Reference33 articles.

1. Crack propagation behavior of some airframe materials;Donaldson,1961

2. On conversion coating treatments to replace chromating for Al alloys: recent developments and possible future directions;Kulinich;Russ. J. Non_Ferrous Metals,2012

3. Modeling the crack propagation rate for corrosion fatigue at High frequency of applied stress;Engelhardt;Corros. Sci.,2010

4. A theoretical evaluation of the influence of mechanical variables on the concentration of oxygen in a corrosion fatigue crack;Turnbull;Corros. Sci.,1982

5. Review of the electrochemical conditions in cracks with particular reference to corrosion fatigue of structural steels in Sea Water;Turnbull;Corros. Rev.,1982

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