Fig. 4.22 Pressure as a function of the position of the fluid elements at the times indicated for
constant piston motion in a tube closed at the end. For the numerical procedure the following
parameters apply; γ ¼ 1.4, κ ¼ 1.5, Δx ¼ 0.4 and Δt ¼ 0.05 (see text)
Fig. 4.23 Density as a function of the position of the fluid elements at the times indicated for
constant piston motion in a tube closed at the end. For the numerical procedure the following
parameters apply; γ ¼ 1.4, κ ¼ 1.5, Δx ¼ 0.4 and Δt ¼ 0.05 (see text)
166
4 Numerical Treatment of Plane Shocks
constant piston motion in a tube closed at the end. For the numerical procedure the following
parameters apply; γ ¼ 1.4, κ ¼ 1.5, Δx ¼ 0.4 and Δt ¼ 0.05 (see text)
Fig. 4.23 Density as a function of the position of the fluid elements at the times indicated for
constant piston motion in a tube closed at the end. For the numerical procedure the following
parameters apply; γ ¼ 1.4, κ ¼ 1.5, Δx ¼ 0.4 and Δt ¼ 0.05 (see text)
166
4 Numerical Treatment of Plane Shocks