Fatigue Behavior of Scs-6/Titanium/Titan1ium Aluminide Hybrid Laminated Composite
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AbstractThe fatigue behavior of the SCS-6 silicon carbide fiber-reinforced Ti-6Al-4V/Ti-25Al- 10Nb hybrid laminated composite was investigated at room temperature. The accumulation of fatigue damage in the form of matrix cracking was measured as a function of loading cycles and applied stress levels. The residual stiffness and residual tensile strength of the post-fatigued specimens were determined. The comparison of the crack growth behavior of the hybrid composite with both the SCS-6/Ti-6-4 and SCS-6/Ti-25-10 composites will also be discussed.
1986 ◽
pp. 561-570
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2009 ◽
Vol 50
(7)
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pp. 1785-1791
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1985 ◽
Vol 27
(3)
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pp. 250-262
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1984 ◽
Vol 106
(1)
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pp. 25-37
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