naginterfaces.library.pde.dim1_​parab_​euler_​roe

naginterfaces.library.pde.dim1_parab_euler_roe(uleft, uright, gamma, comm)

dim1_parab_euler_roe calculates a numerical flux function using Roe’s Approximate Riemann Solver for the Euler equations in conservative form. It is designed primarily for use with the upwind discretization schemes dim1_parab_convdiff(), dim1_parab_convdiff_dae() or dim1_parab_convdiff_remesh(), but may also be applicable to other conservative upwind schemes requiring numerical flux functions.

For full information please refer to the NAG Library document for d03pu

https://support.nag.com/numeric/nl/nagdoc_30.1/flhtml/d03/d03puf.html

Parameters

uleftfloat, array-like, shape $\left(3\right)$

$uleft[\text{i}-1]$ must contain the left value of the component $U_{\text{i}}$, for $\text{i}=1,2,\dots ,3$. That is, $uleft\left[0\right]$ must contain the left value of $\rho$, $uleft\left[1\right]$ must contain the left value of $m$ and $uleft\left[2\right]$ must contain the left value of $e$.

urightfloat, array-like, shape $\left(3\right)$

$uright[\text{i}-1]$ must contain the right value of the component $U_{\text{i}}$, for $\text{i}=1,2,\dots ,3$. That is, $uright\left[0\right]$ must contain the right value of $\rho$, $uright\left[1\right]$ must contain the right value of $m$ and $uright\left[2\right]$ must contain the right value of $e$.

gammafloat

The ratio of specific heats, $\gamma$.

commdict, communication object

Communication structure.

On initial entry: need not be set.

Returns

fluxfloat, ndarray, shape $\left(3\right)$

$flux[\text{i}-1]$ contains the numerical flux component ${\hat{F}}_{\text{i}}$, for $\text{i}=1,2,\dots ,3$.

Raises

NagValueError

(errno $1$)

On entry, $gamma=⟨value⟩$.

Constraint: $gamma>0.0$.

(errno $2$)

Right pressure value $\text{pr}<0.0$: $\text{pr}=⟨value⟩$.

(errno $2$)

Left pressure value $\text{pl}<0.0$: $\text{pl}=⟨value⟩$.

(errno $2$)

On entry, $uright\left[0\right]=⟨value⟩$.

Constraint: $uright\left[0\right]\ge 0.0$.

(errno $2$)

On entry, $uleft\left[0\right]=⟨value⟩$.

Constraint: $uleft\left[0\right]\ge 0.0$.

Notes

dim1_parab_euler_roe calculates a numerical flux function at a single spatial point using Roe’s Approximate Riemann Solver (see Roe (1981)) for the Euler equations (for a perfect gas) in conservative form. You must supply the left and right solution values at the point where the numerical flux is required, i.e., the initial left and right states of the Riemann problem defined below.

In the functions dim1_parab_convdiff(), dim1_parab_convdiff_dae() and dim1_parab_convdiff_remesh(), the left and right solution values are derived automatically from the solution values at adjacent spatial points and supplied to the function argument $\text{numflx}$ from which you may call dim1_parab_euler_roe.

The Euler equations for a perfect gas in conservative form are:

$$\frac{\partial U}{\partial t}+\frac{\partial F}{\partial x}=0\text{,}$$

with

$$\begin{array}{c}U=\left[\begin{array}{c}\rho \\ m\\ e\end{array}\right]\text{and}F=\left[\begin{array}{c}m\\ \frac{m^2}{\rho }+(\gamma -1)(e-\frac{m^2}{2\rho })\\ \frac{me}{\rho }+\frac{m}{\rho }(\gamma -1)(e-\frac{m^2}{2\rho })\end{array}\right]\text{,}\end{array}$$

where $\rho$ is the density, $m$ is the momentum, $e$ is the specific total energy, and $\gamma$ is the (constant) ratio of specific heats. The pressure $p$ is given by

$$p=(\gamma -1)(e-\frac{\rho u^2}{2})\text{,}$$

where $u=m/\rho$ is the velocity.

The function calculates the Roe approximation to the numerical flux function $F(U_L,U_R)=F\left(U^{\ast }(U_L,U_R)\right)$, where $U=U_L$ and $U=U_R$ are the left and right solution values, and $U^{\ast }(U_L,U_R)$ is the intermediate state $\omega \left(0\right)$ arising from the similarity solution $U(y,t)=\omega \left(y/t\right)$ of the Riemann problem defined by

$$\frac{\partial U}{\partial t}+\frac{\partial F}{\partial y}=0\text{,}$$

with $U$ and $F$ as in (2), and initial piecewise constant values $U=U_L$ for $y<0$ and $U=U_R$ for $y>0$. The spatial domain is $-\infty <y<\infty$, where $y=0$ is the point at which the numerical flux is required. This implementation of Roe’s scheme for the Euler equations uses the so-called argument-vector method described in Roe (1981).

References

LeVeque, R J, 1990, Numerical Methods for Conservation Laws, Birkhäuser Verlag

Quirk, J J, 1994, A contribution to the great Riemann solver debate, Internat. J. Numer. Methods Fluids (18), 555–574

Roe, P L, 1981, Approximate Riemann solvers, parameter vectors, and difference schemes, J. Comput. Phys. (43), 357–372