A numerical method is developed for calculating the radiating axisymmetric flowfield accounting for nonequilibrium thermochemistry. Solutions of the flow with radiation are obtained in a fully coupled manner using a fully implicit time-marching method through a full block-matrix inversion. The method is used in calculating the radiation from the blunt-body shock layer in both air and carbon-containing airflows. The calculated results are compared with the experimental data obtained in a ballistic range at flight speeds of up to 13.4 km/s
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Sakai et al. (2001) studied this question.
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