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A Comparison Study of Wear and Fretting Fatigue Behavior Between Cr-alloyed Layer and Cr-Ti Solid-solution Layer
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Fig. 11. Morphologies of the fretting contact zones a, c, e and fretting fatigue fracture surfaces b, d, f of the Ti6Al4V base material a, b, the sample with Cr-alloyed layer c, d and the sample with Cr-Ti solid-solution layer e, f |
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