Corrosion Fatigue Crack Growth of 7475 T7351 Aluminum Alloy under Flight Simulation Loading
| Autor: | Cassius Olívio Figueiredo Terra Ruchert, A.E.A. Chemin, W.W. Bose Filho, Dirceu Spinelli |
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| Rok vydání: | 2015 |
| Předmět: |
inorganic chemicals
Materials science Alloy Metallurgy flight load fungi Oxide technology industry and agriculture chemistry.chemical_element Fracture mechanics General Medicine engineering.material equipment and supplies Flight simulator complex mixtures Corrosion Fatigue crack propagation chemistry.chemical_compound chemistry Corrosion fatigue Aluminium engineering aluminum alloy Engineering(all) |
| Zdroj: | Procedia Engineering. 101:85-92 |
| ISSN: | 1877-7058 |
| DOI: | 10.1016/j.proeng.2015.02.012 |
| Popis: | Corrosion crack propagation experiments were carried out on specimens of 7475 T7351 aluminum alloy. Variable amplitude tests were performed with flight-simulated spectrum Twist ( Transport Aircraft Wing Structures ) and Falstaff ( Fighter Aircraft Loading Standard for Fatigue) exposed to air and saline environment. The results showed that fatigue crack propagation life of specimens tested on saline environment were longer than specimens tested on air environment. The fatigue surfaces of specimens tested on saline environment examined in the SEM showed oxide and Na crystals in the wake of crack, which can promote retardation of crack propagation. |
| Databáze: | OpenAIRE |
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