compressible.h

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Requires: conservation.h

Test cases (1): explosion

Compressible gas dynamics

The Euler system of conservation laws for a compressible gas can be written

$$ \partial_t\left(\begin{array}{c} \rho \\ E \\ w_x \\ w_y \\ \end{array}\right) + \nabla_x \cdot\left(\begin{array}{c} w_x \\ \frac{w_x}{\rho} ( E + p ) \\ \frac{w_x^2}{\rho} + p \\ \frac{w_y w_x}{\rho} \\ \end{array}\right) + \nabla_y \cdot\left(\begin{array}{c} w_y \\ \frac{w_y}{\rho} ( E + p ) \\ \frac{w_y w_x}{\rho} \\ \frac{w_y^2}{\rho} + p \\ \end{array}\right) = 0 $$

with $\rho$ the gas density, $E$ the total energy, $\mathbf{w}$ the gas momentum and $p$ the pressure given by the equation of state

$$ p = (\gamma - 1)(E - \rho\mathbf{u}^2/2) $$

with $\gamma$ the polytropic exponent. This system can be solved using the generic solver for systems of conservation laws.

#include "conservation.h" [api]

The conserved scalars are the gas density $\rho$ and the total energy $E$. The only conserved vector is the momentum $\mathbf{w}$. The constant $\gamma$ is represented by *gammao* here, with a default value of 1.4.

scalar rho[], E[];
vector w[];
scalar * scalars = {rho, E};
vector * vectors = {w};
double gammao = 1.4 ;

The system is entirely defined by the flux() function called by the generic solver for conservation laws. The parameter passed to the function is the array s which contains the state variables for each conserved field, in the order of their definition above (i.e. scalars then vectors).

void flux (const double * s, double * f, double * e)
{

We first recover each value ($\rho$, $E$, $w_x$ and $w_y$) and then compute the corresponding fluxes (f[0], f[1], f[2] and f[3]).

double rho = s[0], E = s[1], wn = s[2], w2 = 0.;
  for (int i = 2; i < 2 + dimension; i++)
    w2 += sq(s[i]);
  double un = wn/rho, p = (gammao - 1.)*(E - 0.5*w2/rho);

  f[0] = wn;
  f[1] = un*(E + p);
  f[2] = un*wn + p;
  for (int i = 3; i < 2 + dimension; i++)
    f[i] = un*s[i];

The minimum and maximum eigenvalues for the Euler system are the characteristic speeds $u \pm \sqrt(\gamma p / \rho)$.

double c = sqrt(gammao*p/rho);
  e[0] = un - c; // min
  e[1] = un + c; // max
}