Fig. 4.7 Pressure as a function of position at t ¼ 10 is shown for the piston moving into the tube at
constant velocity. For the numerical procedure the following parameters apply; γ ¼ 1.4, κ ¼ 1.2,
Δx ¼ 0.1 and Δt ¼ 0.01 (see text)
Fig. 4.8 Density as a function of position at t ¼ 10 is shown for the piston moving into the tube at
constant velocity. For the numerical procedure the following parameters apply; γ ¼ 1.4, κ ¼ 1.2,
Δx ¼ 0.1 and Δt ¼ 0.01 (see text)
4.8 Numerical Examples of Plane Shocks
155
constant velocity. For the numerical procedure the following parameters apply; γ ¼ 1.4, κ ¼ 1.2,
Δx ¼ 0.1 and Δt ¼ 0.01 (see text)
Fig. 4.8 Density as a function of position at t ¼ 10 is shown for the piston moving into the tube at
constant velocity. For the numerical procedure the following parameters apply; γ ¼ 1.4, κ ¼ 1.2,
Δx ¼ 0.1 and Δt ¼ 0.01 (see text)
4.8 Numerical Examples of Plane Shocks
155