Commit e9f29167 by Douglas Serson

### Remove unused variables

parent 473e0a90
 ... ... @@ -198,6 +198,7 @@ Under this section it is possible to set the parameters of the simulation.

pInf = 101325

rhoInf = 1.225

TInf = pInf/(287.058*rhoInf)

Twall = pInf/(287.058*rhoInf)+15.0

uInf = 147.4

vInf = 0.0

wInf = 0.0

... ... @@ -218,6 +219,8 @@ to screen; \item \inltt{pInf} farfield pressure (i.e. $p_{\infty}$). Default value = 101325 $Pa$; \item \inltt{rhoInf} farfield density (i.e. $\rho_{\infty}$). Default value = 1.225 $Kg/m^{3}$; \item \inltt{TInf} farfield temperature (i.e. $T_{\infty}$). Default value = 288.15 $K$; \item \inltt{Twall} temperature at the wall when isothermal boundary conditions are employed (i.e. $T_{w}$). Default value = 300.15$K$; \item \inltt{uint} farfield $X$-component of the velocity (i.e. $u_{\infty}$). Default value = 0.1 $m/s$; \item \inltt{vInf} farfield $Y$-component of the velocity (i.e. $v_{\infty}$). Default value = 0.0 $m/s$; \item \inltt{wInf} farfield $Z$-component of the velocity (i.e. $w_{\infty}$). Default value = 0.0 $m/s$; ... ...
 ... ... @@ -122,9 +122,7 @@ namespace Nektar numericalFluxO1(m_spaceDim); Array > > derivativesO1(m_spaceDim); Array > fluxvector(m_spaceDim); for (j = 0; j < m_spaceDim; ++j) { numericalFluxO1[j] = Array >( ... ... @@ -227,8 +225,7 @@ namespace Nektar int nDim = fields[0]->GetCoordim(0); Array Vn (nTracePts, 0.0); Array fluxtemp(nTracePts, 0.0); // Get the normal velocity Vn for(i = 0; i < nDim; ++i) { ... ...
Markdown is supported
0% or .
You are about to add 0 people to the discussion. Proceed with caution.
Finish editing this message first!