thermochemical ablation of carbon/carbon composites with non-linear thermal conductivity
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ID: 176505
2014
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Abstract
Carbon/carbon composites have been typically used to protect a rocket nozzle
from high temperature oxidizing gas. Based on the Fourier’s law of heat
conduction and the oxidizing ablation mechanism, the ablation model with
non-linear thermal conductivity for a rocket nozzle is established in order
to simulate the one-dimensional thermochemical ablation rate on the surface
and the temperature distributions by using a written computer code. As the
presented results indicate, the thermochemical ablation rate of a solid
rocket nozzle calculated by using actual thermal conductivity, which is a
function of temperature, is higher than that by a constant thermal
conductivity, so the effect of thermal conductivity on the ablation rate of a
solid rocket nozzle made of carbon/carbon composites cannot be neglected.
| Reference Key |
wei-jie2014thermalthermochemical
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|---|---|
| Authors | ;Li Wei-Jie;Huang Hai-Ming;Hu Yu-Meng |
| Journal | Nature |
| Year | 2014 |
| DOI |
10.2298/TSCI1405625L
|
| URL | |
| Keywords | Keywords not found |
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