Fig. 4.64 Pressure as a function of position at four different times showing one shock catching up
with the other shock. For the numerical procedure the following parameters apply; γ ¼ 1.4, κ ¼ 1.5,
Δx ¼ 0.4 and Δt ¼ 0.04 (see text)
Fig. 4.65 Pressure plotted as a function of position for the two shocks prior to and after the
overtaking process. For the numerical procedure the following parameters apply; γ ¼ 1.4, κ ¼ 1.5,
Δx ¼ 0.4 and Δt ¼ 0.04 (see text)
4.8 Numerical Examples of Plane Shocks
209
with the other shock. For the numerical procedure the following parameters apply; γ ¼ 1.4, κ ¼ 1.5,
Δx ¼ 0.4 and Δt ¼ 0.04 (see text)
Fig. 4.65 Pressure plotted as a function of position for the two shocks prior to and after the
overtaking process. For the numerical procedure the following parameters apply; γ ¼ 1.4, κ ¼ 1.5,
Δx ¼ 0.4 and Δt ¼ 0.04 (see text)
4.8 Numerical Examples of Plane Shocks
209