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Journal ArticleDOI

Thermal expansion at elevated temperatures III. A hemispherical laminar composite of pyrolytic graphite, silicon carbide and its constituents between 300 and 800 K

A F Pojur, +2 more
- 01 Jul 1972 - 
- Vol. 5, Iss: 7, pp 1321-1329
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TLDR
In this article, the results of measurements of the linear coefficients of thermal expansion of hollow hemispherical specimens of pyrolytic graphite, silicon carbide and triplet composite specimens of these components over the approximate temperature range 300 to 800 K are reported.
Abstract
Attention is drawn to attempts which have been made to calculate thermal and elastic properties of particle-, fibre- and laminar-reinforced composite materials from corresponding properties of their constituents. The results of measurements of the linear coefficients of thermal expansion of small (similar 0?5 mm) hollow hemispherical specimens of pyrolytic graphite, silicon carbide and triplet hemispherical composite specimens of these components over the approximate temperature range 300 to 800 K are then reported. In conclusion it is shown how dilatation in composite structures such as these is amenable to the application of classical elasticity theory, and how agreement between the results of such calculations and observation provides evidence for the absence of layer separation resulting from constrained expansion.

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Citations
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Journal ArticleDOI

Handbook of SiC properties for fuel performance modeling

TL;DR: In this paper, a compilation of non-irradiated and irradiated properties of SiC are provided and reviewed and analyzed in terms of application to TRISO fuels, specifically in the high-temperature irradiation regime.
Journal ArticleDOI

Properties of silicon carbide for nuclear fuel particle coatings

R. J. Price
- 01 Sep 1977 - 
TL;DR: The properties of pyrolytic silicon carbide (SiC) that are important to its use in nuclear fuel particle coatings are reviewed in this paper, where the structure of material deposited under different conditions varies.
Journal ArticleDOI

Thermal expansion at elevated temperatures IV. Carbon-fibre composites

TL;DR: In this paper, the linear thermal expansion coefficient of a unidirectional carbon-fibre-reinforced plastic (CFRP) is reported in the approximate temperature range 80-400 K.
References
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Journal ArticleDOI

The Influence of Stacking Sequence on Laminate Strength

TL;DR: In this article, an approach is presented to predict the detailed stacking sequence of specific layer orientations which leads to optimum protection against delamination under uniaxial static and fatigue loadings.
Journal ArticleDOI

Thermal Expansion of Various Ceramic Materials to 1500°C

TL;DR: In this article, thermal expansion data from room temperature to 1500°C were given for a number of ceramic materials with telemicroscopes on bars or rods 7 in. long.
Journal ArticleDOI

Elastic properties of isotropic graphite

TL;DR: Young's modulus and the shear modulus for bulk isotropic graphites of various porosities were reported for the first time in this article, where they were shown to be 255 and 97 kilobars, respectively.
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A mathematical model for calculating stresses in a pyrocarbon- and silicon carbide-coated fuel particle.

TL;DR: In this article, the analysis employed by previous authors in calculating the stresses developed during service in a pyrolytic carbon coating on a spherical fuel particle has been extended to consider composite carbide-carbon coatings.
Journal ArticleDOI

Thermal expansivities and preferred orientation of pyrolytic carbons

TL;DR: The relation between preferred orientation and thermal expansion coefficient was investigated for a wide variety of pyrolytic carbons, including materials used for free-standing bodies as well as those used for coating nuclear fuel particles as discussed by the authors.
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