Correction to: Modelling of Mach reflections in internal axisymmetric steady supersonic flow

1 Correction to: Shock Waves https://doi.org/10.1007/s00193-021-01047-1

In this article, the legends for Figs. 4 and 5 were inadvertently omitted; the figures should have appeared as shown below.

Fig. 4

Top: CFD predictions of Mach disc radius for β_w = 150° and l_w = 1.0, with LSQ fits and Richardson extrapolation value. Bottom: percentage difference between y_tp and the Richardson extrapolation value, y_tp,e, for ranges of MRL_disc and MRL_field

Fig. 5

Effect of wedge length, l_w, on Mach disc radius, y_tp, (top) and incident shock angle at the triple point, β_tp, (bottom) for shock angles at the wedge leading edge, β_w = 148°, 150°, 152°, and 154°. Lines indicate results from the model, open symbols—CFD results, and solid symbols—model predictions at l_w,crit