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Figure 4.

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Steady-state flow fields as a function of the longitudinal length x/L for the geometric () and thermal throat (- - -) choking cases obtained from the CFD solver. The steady Mach number ( M ¯ $ \bar{{\text{ M}}} $, (a)); the static pressure ( p ¯ $ \bar{p} $, (b)) and the static temperature ( T ¯ $ \bar{T} $, (c)) are displayed. Quantities are measured on the symmetry axis of the computational domain.

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