Position (Arb.units)
Fig. 4.32 Pressure in the shock tube as a function of position at t ¼ 4 (Arb. units) is shown. 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)
Position (Arb.units)
Fig. 4.33 Density in the shock tube as a function of position at t ¼ 4 (Arb. units) is shown. 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)
178
4 Numerical Treatment of Plane Shocks
Fig. 4.32 Pressure in the shock tube as a function of position at t ¼ 4 (Arb. units) is shown. 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)
Position (Arb.units)
Fig. 4.33 Density in the shock tube as a function of position at t ¼ 4 (Arb. units) is shown. 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)
178
4 Numerical Treatment of Plane Shocks