Comparison of SCC Thresholds and Environmentally Assisted Cracking in 7050-T7451 Aluminum Plate

Author:

Arnold Eric M.,Schubbe Joel J.,Moran Patrick J.,Bayles Robert A.

Publisher

Springer Science and Business Media LLC

Subject

Mechanical Engineering,Mechanics of Materials,General Materials Science

Reference12 articles.

1. J. Schubbe, Evaluation of fatigue life and crack growth rates in 7050-T7451 aluminum plate for T-L and L-S oriented failure under truncated spectra loading, Eng. Fail. Anal., 2009, 16, p 340–349

2. J. Schubbe, Fatigue Crack Propagation in 7050-T7451 Plate Alloy, Eng. Fract. Mech., 2009, 76, p 1037–1048. doi: 10.1016/j.engfracmech.2009.01.006

3. R. Braun, Environmentally Assisted Cracking of Aluminum Alloys, Mat.-wiss. u. Werkstofftech., 2007, 38(9), doi: 10.1002/mawe.200700204

4. N. Holroyd, Environment-Induced Cracking of High-Strength Aluminum Alloys, Proceedings of the First International Conference on Environment-Induced Cracking of Metals, R.P. Gangloff, M.B. Ives, Ed., 1988, NACE-10, National Association of Corrosion Engineers, Houston TX, 1990, p 311–345

5. D. Sprowls, Fundamental Aspects of Stress Corrosion Cracking, R.W. Staehle, Ed., National Association of Corrosion Engineers, Houston, 1969, p 466

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