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Developments in Ceramic Materials Research

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Model<strong>in</strong>g of Thermal Transport <strong>in</strong> <strong>Ceramic</strong>s Matrix Composites 189<br />

The thermal properties determ<strong>in</strong>ed us<strong>in</strong>g one model is <strong>in</strong>cluded <strong>in</strong> subsequent models. It<br />

is <strong>in</strong> this way that the synergy between different classes of porosity is assessed. Figure 15<br />

shows the flow chart for thermal transport modell<strong>in</strong>g of this DLR-XT CMC material us<strong>in</strong>g<br />

sub-models shown <strong>in</strong> Figure 14 and <strong>in</strong>corporat<strong>in</strong>g porosity type D, shown <strong>in</strong> Figure 9.<br />

3.4.1. Thermal Properties<br />

Thermal conductivity is one of the driv<strong>in</strong>g forces <strong>in</strong> design<strong>in</strong>g materials for thermal<br />

applications. In a material, heat flow is proportional to the temperature gradient with the<br />

constant of proportionality be<strong>in</strong>g the thermal conductivity. Its general form is<br />

q = − k<br />

i<br />

ij<br />

d T<br />

d x<br />

j<br />

where qi is the heat flux and kij is the thermal conductivity. This is a second-order tensor<br />

and <strong>in</strong> most cases a symmetric one. Another important parameter for controll<strong>in</strong>g thermal<br />

transport is thermal diffusivity α . It is def<strong>in</strong>ed as the ratio of a material’s capacity to conduct<br />

heat versus its capacity to store it. It is related to thermal conductivity k , specific heat C p<br />

and density ρ as:<br />

k = α ρ C<br />

(10)<br />

p<br />

Relevant thermal properties of CMC constituents, shown <strong>in</strong> Table 3, along with air for<br />

the pores or cracks are employed for the thermal transport models.<br />

Table 3. Standard thermal property values of constituent materials<br />

Material k (W m -1 K -1 ) ρ (kg m -3 ) C p (x10 -6 )(J kg -1 K -1 )<br />

Carbon Fibre Transverse 4 1928 921<br />

Carbon Fibre Longitud<strong>in</strong>al 40 1928 921<br />

Carbon Matrix 10 1800 717<br />

SiC Matrix 70 3200 1422<br />

Air 0.001 1 1<br />

F<strong>in</strong>ite-element methods for determ<strong>in</strong><strong>in</strong>g the thermal transport properties of solids are<br />

based on the two thermal analyses; Steady State and Transient. The steady state thermal<br />

(9)

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