Fatigue behavior of SCS-6/titanium/titanium aluminide hybrid laminated composite
Book
·
OSTI ID:490787
- Univ. of California, Los Angeles, CA (United States). Dept. of Materials Science and Engineering
The 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.
- Sponsoring Organization:
- Department of the Air Force, Washington, DC (United States)
- OSTI ID:
- 490787
- Report Number(s):
- CONF-960401--; ISBN 1-55899-337-1
- Country of Publication:
- United States
- Language:
- English
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