20421 Corrosion Fatigue of Al 5083-H131 Sensitized at 70, 100, and 175C and Relation to Microstructure and Degree of Sensitization

Wednesday, August 3, 2011: 2:00 PM
Ronald L. Holtz*, Peter S. Pao, Robert A. Bayles, Thomas M. Longazel, and Ramasis Goswami
Naval Research Laboratory
Corrosion fatigue thresholds of Al 5083-H131 at high load ratio do not degrade until the ASTM G67 mass loss exceeds approximately 30 mg/cm2, regardless of aging temperature.  For mass loss greater than 30 mg/cm2, the rate of degradation of the corrosion fatigue threshold with mass loss is independent of aging temperature. The critical mass loss for corrosion fatigue threshold degradation, 30 mg/cm2, is associated with the occurrence of a semi-continuous type of grain boundary coverage by β Al3Mg2. Once the grain boundary is fully covered with β, typically in the ASTM G67 mass loss range of 40 to 50 mg/cm2, the threshold has already degraded substantially. Some of the practical implications of these findings are that the existence of a critical degree of sensitization for corrosion-fatigue degradation can serve as a structural risk management criterion, and the aging temperature independence of this critical degree of sensitization suggests an accelerated aging method for quality control for manufacture and procurement of Al-Mg alloys.