foam-extend4.1-coherent-io/applications/solvers/engine/sonicTurbDyMEngineFoam/pEqn.H

{
    rho = thermo.rho();

    rUA = 1.0/UEqn.A();
    U = rUA*UEqn.H();

    if (nOuterCorr != 1)
    {
        p.storePrevIter();
    }

    if (transonic)
    {
        surfaceScalarField phid =
            fvc::interpolate(thermo.psi())*
            ((fvc::interpolate(U) & mesh.Sf()) - fvc::meshPhi(rho, U));

        for (int nonOrth=0; nonOrth<=nNonOrthCorr; nonOrth++)
        {
            fvScalarMatrix pEqn
            (
                fvm::ddt(psi, p)
              + fvm::div(phid, p, "div(phid,p)")
              - fvm::laplacian(rho*rUA, p)
            );

            pEqn.solve();

            if (nonOrth == nNonOrthCorr)
            {
                phi == pEqn.flux();
            }
        }
    }
    else
    {
        phi = fvc::interpolate(rho)*
            ((fvc::interpolate(U) & mesh.Sf()) - fvc::meshPhi(rho, U));

        for (int nonOrth=0; nonOrth<=nNonOrthCorr; nonOrth++)
        {
            fvScalarMatrix pEqn
            (
                fvm::ddt(psi, p)
              + fvc::div(phi)
              - fvm::laplacian(rho*rUA, p)
            );

            pEqn.solve();

            if (nonOrth == nNonOrthCorr)
            {
                phi += pEqn.flux();
            }
        }
    }

    // Explicitly relax pressure except for last corrector
    if (oCorr != nOuterCorr - 1)
    {
        p.relax();
    }

#   include "rhoEqn.H"
#   include "compressibleContinuityErrs.H"

    U -= rUA*fvc::grad(p);
    U.correctBoundaryConditions();

    DpDt = fvc::DDt(surfaceScalarField("phiU", phi/fvc::interpolate(rho)), p);
    dpdt = fvc::ddt(p);
}