Shock-Tube Control Panel

Sod's Problem Lax's Problem

• Eno of 1 2 3 4 order
• MUSCL First order Fully upwind Upwind biased scheme.

  Apply the recontruction/interpolation operator on

• conservative variables characteristic variables.

  Estimate fluxes at cell-interface with the Riemann Solver of

• Godunov Roe. HLLE.

For the MUSCL interpolation method you must also specify a limiter:

Minmod Van Albada Superbee

These are the variables that should be visualized:

density momentum energy pressure velocity sound speed mach number

Press this button to plot the result: .