Abstract
In this study, the microstructural formation and static/dynamic compression behaviour of the recycled Ni-Al/Nb2Al/ZrO2 matrix-hybrid composites reinforced with Nb and ZrO2 will be studied. It is intended to be an alternative to traditional alloys/composites used in the aeronautical industry. These composites are generally produced by using combined sintering + forging processes. The static and dynamic properties will be evaluated in detail, considering the relevant scanning electron microscopy (SEM) microstructures, including the distribution of reinforcement elements.
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Acknowledgements
All the mechanical tests have been conducted on the Zwick mechanical test device installed at the laboratory of ISAE-SUPMECA-Paris, France; we acknowledge their technical help. We acknowledge the French Aeronautical Society, Airbus-Helicopters and Dr. G. Zambelis for his support for this project. The authors acknowledge Prof. I. Miskioglu from Michigan Technical University, MI-USA, for the nanoindentation tests for the wear behaviour of the composite studied in this project.
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Kaftancıoglu, U., Zambelis, G., Gatamorta, F., Miskioglu, I., Bayraktar, E. (2023). Development of Ni-Al/Nb2Al/ZrO2-Based Composites for Aircraft Engine Applications Produced by a Combined Method: Sintering + Forging. In: Chalivendra, V., Gardea, F. (eds) Mechanics of Composite, Hybrid & Multi-functional Materials, Volume 5. SEM 2022. Conference Proceedings of the Society for Experimental Mechanics Series. Springer, Cham. https://doi.org/10.1007/978-3-031-17445-2_7
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