Corrosion Fatigue Crack Growth of 7475 T7351 Aluminum Alloy...

Procedia Engineering 2015 Vol. 101

Corrosion Fatigue Crack Growth of 7475 T7351 Aluminum Alloy under Flight Simulation Loading

Chemin, A., Spinelli, D., Filho, W. Bose, Ruchert, C.
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Volume:
101
Year:
2015
Language:
english
Journal:
Procedia Engineering
DOI:
10.1016/j.proeng.2015.02.012
File:
PDF, 1.66 MB
english, 2015
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