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{ 2D_EULERIAN_SHOCK.PDE
Comparison with shock tube problem of G.A. Sod
See 1D_EULERIAN_SHOCK.PDE for a 1D model of the same problem.
Ref: G.A. Sod, "A Survey of Several Finite Difference Methods for Systems of
Nonlinear Hyperbolic Conservation Laws", J. Comp. Phys. 27, 1-31 (1978)
See also Kershaw, Prasad and Shaw, "3D Unstructured ALE Hydrodynamics with the
Upwind Discontinuous Finite Element Method", UCRL-JC-122104, Sept 1995.
}
TITLE "Sod's Shock Tube Problem - 2D Eulerian"
SELECT
ngrid = 100 { increase the grid density }
regrid = off { disable the adaptive mesh refinement }
errlim = 1e-4 { lower the error limit }
VARIABLES
rho(1)
u(1)
P(1)
DEFINITIONS
len = 1
wid = 0.02
gamma = 1.4
eps = 0.001 {=4*(1/63)^2}
INITIAL VALUES
rho = 1.0 - 0.875*uramp(x-0.49, x-0.51)
u = 0
P = 1.0 - 0.9*uramp(x-0.49, x-0.51)
EQUATIONS
rho: dt(rho)+u*dx(rho) = eps*div(grad(rho)) - rho*dx(u)
u: dt(u)+u*dx(u) = eps*div(grad(u)) - dx(P)/rho
P: dt(P)+u*dx(P) = eps*div(grad(P)) - gamma*P*dx(u)
BOUNDARIES
REGION 1
START(0,0)
Line to (len,0)
Value(u)=0 line to (len,wid)
Natural(u)=0 line to (0,wid) to close
TIME 0 TO 0.375
MONITORS
for cycle=5
elevation(rho) from(0,wid/2) to (len,wid/2)
elevation(u) from(0,wid/2) to (len,wid/2)
elevation(P) from(0,wid/2) to (len,wid/2)
history(rho) at (0.5,wid/2)
history(u) at (0.48,wid/2) (0.49,wid/2) (0.5,wid/2) (0.51,wid/2) (0.52,wid/2)
history(p) at (0.48,wid/2) (0.49,wid/2) (0.5,wid/2) (0.51,wid/2) (0.52,wid/2)
history(deltat)
PLOTS
for t=0.143, 0.375
elevation(rho) from(0,wid/2) to (len,wid/2)
elevation(u) from(0,wid/2) to (len,wid/2)
elevation(P) from(0,wid/2) to (len,wid/2)
history(rho) at (0.48,wid/2) (0.49,wid/2) (0.5,wid/2) (0.51,wid/2) (0.52,wid/2)
history(u) at (0.48,wid/2) (0.49,wid/2) (0.5,wid/2) (0.51,wid/2) (0.52,wid/2)
history(p) at (0.48,wid/2) (0.49,wid/2) (0.5,wid/2) (0.51,wid/2) (0.52,wid/2)
END