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Thermal Expansion and Mechanical Behavior of Graphite-Fiber-Reinforced Tantalum-Carbide Composites

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Thermal Expansion 6
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Abstract

Thermal expansion measurements, on a variety of graphite-fiber-reinforced tantalum-carbide composites fabricated at temperatures above 3, 000°C, imply that little bonding exists between fibers and matrix at room temperature. The results of flexure tests tend to confirm this hypothesis. Heating to above 1, 600°C appears to provide significant mechanical interactions between fibers and matrix, presumably caused by differential thermal expansions and interface friction, which lead to highly anisotropic thermal strains at higher temperatures despite isotropic thermal expansion at lower temperatures. One implication is that the thermal expansion behavior of these composites will be similar, in terms of volumetric thermal strain, to that of the carbide matrix, as long as the carbide is the continuous phase of the composite. It was only in those composites which showed evidence of a damaged and/or discontinuous matrix phase that significantly lower volumetric thermal expansions were observed.

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References

  1. J. O. Gibson. Low- Linear Thermal- Exp ans ion NbC- Graphite Composite Studies. Phase II Report under Contract SNPC-67 for NASA, McDonnell Douglas Astronautics Company Report MDC G1692, May 1970.

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  3. G. W. Hollenberg and R. L. Crane. Effect of Graphite Fiber Additions on the Grain Growth and Strength of Hot-pressed Silicon Carbide. Paper 9-C-74, 76th annual meeting of the American Ceramic Society, May 1974.

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© 1978 Purdue Research Foundation

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Jortner, J. (1978). Thermal Expansion and Mechanical Behavior of Graphite-Fiber-Reinforced Tantalum-Carbide Composites. In: Peggs, I.D. (eds) Thermal Expansion 6. Springer, Boston, MA. https://doi.org/10.1007/978-1-4615-9086-6_22

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  • DOI: https://doi.org/10.1007/978-1-4615-9086-6_22

  • Publisher Name: Springer, Boston, MA

  • Print ISBN: 978-1-4615-9088-0

  • Online ISBN: 978-1-4615-9086-6

  • eBook Packages: Springer Book Archive

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