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The Australian National University
Research School of Astronomy and Astrophysics
Fyris Alpha Simulation Code

2D Double Mach Reflection Shock Wedge Test

This is an example of complex boundary conditions, and the emergence of a complex self-similar structure in the multiple shocks that form from a simple initial geometry. A horizontal Mach 10 shocked flow impinges on a ramp, or wedge, at an angle of 30 degrees up from the horizontal.

In the simulation the shock is setup as an oblique shock, and the wedge is set as a partially reflecting horizontal lower boundary. The horizontal axis is 4.0 units long, and is a free outflow for the first $1/6$ units, then reflecting for the rest of the boundary. The upper boundary is updated with the time-dependent oblique shock location. The left and boundary is constant with the post oblique shock values, and the right boundary is free.

The remaining problem parameters are:

  • Adiabatic index: gamma = 1.4.
  • Grid Domain: 0.0 < x < 4.0, 0.0 < y < 2.0
  • Shock: Mach 10, v_s = 10.0,
  • Angle: 30 degrees.
  • Pre--shock Conditions: P = 1.0$, d = 1.4, v = 0.0.
  • Post--shock Conditions: P = 116.5, d = 8, v = 8.25. v_x = 7.14471, v_y = -4.125
  • Time Limit: t = 0.25.

As the shock moves, it impinges on the reflecting part of the lower boundary and a complex shock reflection structure forms. The simulation was run for a range of resolutions, from h = 50 to h = 800.

The overall appearance, in the density variable, is shown in the lower panel of figure \ref{f:machwedge}. Key features include:

  • A, the leading edge of the wedge.
  • B -- C -- D, a remnant artifact from the initial shock location.
  • E -- F -- G. A slipping contact line, E ,that leads around to a forward moving stem structure, F , with a vortex head, G.
  • S The oblique shock travelling in the direction of the arrow.

The upper panels show the leading structure as a function of increasing resolution, showing the essential features even at the lowest resolution, while the saturated Kelvin-Helmholtz instabilities occur in the slip layers, E -- F -- G, at sufficiently high resolutions.

Mach Wedge density. Upper Panels show a unit area centered on x - 3.0, $y = 0.5, at t = 0.25. Numbers indicate the linear resolution of the unit square in cells. The lower panel shows the entire 0.0 < x < 4.0, 0.0 < y < 2.0 domain of the simulation at t = 0.25 for the h = 400 resolution simulation. The standard color scale is used for 5 < d < 19