Effect of combined cycle fatigue on Ti62
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L.Mendia; F.J. Estensoro; C. Mary; F. Vogel
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Article
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2011
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Elsevier
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English
โ 268 KB
Gas turbine blades are subjected to very high levels of stress and temperature during each engine operating cycle. Superimposed upon this quasy-steady state condition, blades also endure vibrational stresses induced by local perturbations. When characterizing advanced manufacturing candidate materia