17YJunction.C

Go to the documentation of this file.

/*---------------------------------------------------------------------------*\
     ██╗████████╗██╗  ██╗ █████╗  ██████╗ █████╗       ███████╗██╗   ██╗
     ██║╚══██╔══╝██║  ██║██╔══██╗██╔════╝██╔══██╗      ██╔════╝██║   ██║
     ██║   ██║   ███████║███████║██║     ███████║█████╗█████╗  ██║   ██║
     ██║   ██║   ██╔══██║██╔══██║██║     ██╔══██║╚════╝██╔══╝  ╚██╗ ██╔╝
     ██║   ██║   ██║  ██║██║  ██║╚██████╗██║  ██║      ██║      ╚████╔╝
     ╚═╝   ╚═╝   ╚═╝  ╚═╝╚═╝  ╚═╝ ╚═════╝╚═╝  ╚═╝      ╚═╝       ╚═══╝
 
 * In real Time Highly Advanced Computational Applications for Finite Volumes
 * Copyright (C) 2021 by the ITHACA-FV authors
-------------------------------------------------------------------------------
License
    This file is part of ITHACA-FV
    ITHACA-FV is free software: you can redistribute it and/or modify
    it under the terms of the GNU Lesser General Public License as published by
    the Free Software Foundation, either version 3 of the License, or
    (at your option) any later version.
    ITHACA-FV is distributed in the hope that it will be useful,
    but WITHOUT ANY WARRANTY; without even the implied warranty of
    MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
    GNU Lesser General Public License for more details.
    You should have received a copy of the GNU Lesser General Public License
    along with ITHACA-FV. If not, see <http://www.gnu.org/licenses/>.
Description
    Example of an unsteady NS Reduction Problem with time-dependent boundary
    conditions.
SourceFiles
    17YJunction.C
\*---------------------------------------------------------------------------*/
#include "unsteadyNS.H"
#include "ITHACAPOD.H"
#include "ReducedUnsteadyNS.H"
#include "ITHACAstream.H"
#include <chrono>
#include <math.h>
#include <iomanip>
 
class tutorial17: public unsteadyNS
{
    public:
        explicit tutorial17(int argc, char* argv[])
            :
            unsteadyNS(argc, argv),
            U(_U()),
            p(_p())
        {}
 
        // Fields To Perform
        volVectorField& U;
        volScalarField& p;
 
        void offlineSolve()
        {
            List<scalar> mu_now(1);
            volVectorField U0 = U;
            volScalarField P0 = p;
 
            if (offline)
            {
                ITHACAstream::read_fields(Ufield, U, "./ITHACAoutput/Offline/");
                ITHACAstream::read_fields(Pfield, p, "./ITHACAoutput/Offline/");
            }
            else
            {
                U = U0;
                p = P0;
                mu_now[0] = mu(0, 0);
                truthSolve(mu_now);
            }
        }
 
        // Method to compute the lifting functions for this tutorial
        void liftSolve(Eigen::MatrixXd BCs)
        {
            for (label k = 0; k < inletPatch.rows(); k++)
            {
                Time& runTime = _runTime();
                surfaceScalarField& phi = _phi();
                fvMesh& mesh = _mesh();
                volScalarField p = _p();
                volVectorField U = _U();
                IOMRFZoneList& MRF = _MRF();
                label BCind = inletPatch(k, 0);
                volVectorField Ulift("Ulift" + name(k), U);
                instantList Times = runTime.times();
                runTime.setTime(Times[1], 1);
                pisoControl potentialFlow(mesh, "potentialFlow");
                Info << "Solving a lifting Problem" << endl;
                Vector<double> v1(0, 0, 0);
                v1[0] = BCs(0, k);
                v1[1] = BCs(1, k);
                Vector<double> v0(0, 0, 0);
 
                for (label j = 0; j < U.boundaryField().size(); j++)
                {
                    if (j == BCind)
                    {
                        assignBC(Ulift, j, v1);
                    }
                    else if (U.boundaryField()[BCind].type() == "fixedValue")
                    {
                        assignBC(Ulift, j, v0);
                    }
                    else
                    {
                    }
 
                    assignIF(Ulift, v0);
                    phi = linearInterpolate(Ulift) & mesh.Sf();
                }
 
                Info << "Constructing velocity potential field Phi\n" << endl;
                volScalarField Phi
                (
                    IOobject
                    (
                        "Phi",
                        runTime.timeName(),
                        mesh,
                        IOobject::READ_IF_PRESENT,
                        IOobject::NO_WRITE
                    ),
                    mesh,
                    dimensionedScalar("Phi", dimLength * dimVelocity, 0),
                    p.boundaryField().types()
                );
                label PhiRefCell = 0;
                scalar PhiRefValue = 0;
                setRefCell
                (
                    Phi,
                    potentialFlow.dict(),
                    PhiRefCell,
                    PhiRefValue
                );
                mesh.setFluxRequired(Phi.name());
                runTime.functionObjects().start();
                MRF.makeRelative(phi);
                adjustPhi(phi, Ulift, p);
 
                while (potentialFlow.correctNonOrthogonal())
                {
                    fvScalarMatrix PhiEqn
                    (
                        fvm::laplacian(dimensionedScalar("1", dimless, 1), Phi)
                        ==
                        fvc::div(phi)
                    );
                    PhiEqn.setReference(PhiRefCell, PhiRefValue);
                    PhiEqn.solve();
 
                    if (potentialFlow.finalNonOrthogonalIter())
                    {
                        phi -= PhiEqn.flux();
                    }
                }
 
                MRF.makeAbsolute(phi);
                Info << "Continuity error = "
                     << mag(fvc::div(phi))().weightedAverage(mesh.V()).value()
                     << endl;
                Ulift = fvc::reconstruct(phi);
                Ulift.correctBoundaryConditions();
                Info << "Interpolated velocity error = "
                     << (sqrt(sum(sqr((fvc::interpolate(U) & mesh.Sf()) - phi)))
                         / sum(mesh.magSf())).value()
                     << endl;
                Ulift.write();
                volVectorField Uzero
                (
                    IOobject
                    (
                        "Uzero",
                        U.time().timeName(),
                        U.mesh(),
                        IOobject::NO_READ,
                        IOobject::AUTO_WRITE
                    ),
                    U.mesh(),
                    dimensionedVector("zero", U.dimensions(), vector::zero)
                );
                volVectorField Uliftx("Uliftx" + name(k), Uzero);
                Uliftx.replace(0, Ulift.component(0));
                Uliftx.write();
                liftfield.append((Uliftx).clone());
                volVectorField Ulifty("Ulifty" + name(k), Uzero);
                Ulifty.replace(1, Ulift.component(1));
                Ulifty.write();
                liftfield.append((Ulifty).clone());
            }
        }
 
};
 
/*---------------------------------------------------------------------------*\
                               Starting the MAIN
\*---------------------------------------------------------------------------*/
int main(int argc, char* argv[])
{
    // Construct the tutorial17 object
    tutorial17 example(argc, argv);
    // the offline samples for the boundary conditions
    word par_offline_BC("./timeBCoff");
    // Convert boundary values x-direction and y-direction to x,y,z
    Eigen::MatrixXd timeBCoff2D = ITHACAstream::readMatrix(par_offline_BC);
    Eigen::MatrixXd timeBCoff3D = Eigen::MatrixXd::Zero(6, timeBCoff2D.cols());
    timeBCoff3D.row(0) = timeBCoff2D.row(0);
    timeBCoff3D.row(1) = timeBCoff2D.row(1);
    timeBCoff3D.row(3) = timeBCoff2D.row(2);
    timeBCoff3D.row(4) = timeBCoff2D.row(3);
    example.timeBCoff = timeBCoff3D;
    Eigen::MatrixXd par_on_BC;
    word par_online_BC("./timeBCon");
    par_on_BC = ITHACAstream::readMatrix(par_online_BC);
    // Read parameters from ITHACAdict file
    ITHACAparameters* para = ITHACAparameters::getInstance(example._mesh(),
                             example._runTime());
    int NmodesUout = para->ITHACAdict->lookupOrDefault<int>("NmodesUout", 15);
    int NmodesPout = para->ITHACAdict->lookupOrDefault<int>("NmodesPout", 15);
    int NmodesSUPout = para->ITHACAdict->lookupOrDefault<int>("NmodesSUPout", 15);
    int NmodesUproj = para->ITHACAdict->lookupOrDefault<int>("NmodesUproj", 10);
    int NmodesPproj = para->ITHACAdict->lookupOrDefault<int>("NmodesPproj", 10);
    int NmodesSUPproj = para->ITHACAdict->lookupOrDefault<int>("NmodesSUPproj", 10);
    int NmodesOut = para->ITHACAdict->lookupOrDefault<int>("NmodesOut", 20);
    example.Pnumber = 1;
    example.Tnumber = 1;
    example.setParameters();
    // Set the parameter ranges
    example.mu_range(0, 0) = 0.01;
    example.mu_range(0, 1) = 0.01;
    // Generate equispaced samples inside the parameter range
    example.genEquiPar();
    // Set the inlet boundaries where we have non homogeneous boundary conditions
    example.inletIndex.resize(4, 2); // rows: total number of patches
    example.inletIndex(0, 0) = 1;  // Patch inlet 1
    example.inletIndex(0, 1) = 0;  // Patch inlet 1: x-direction
    example.inletIndex(1, 0) = 1;  // Patch inlet 1: y-direction
    example.inletIndex(1, 1) = 1;  // Patch inlet 2
    example.inletIndex(2, 0) = 2;  // Patch inlet 2: x-direction
    example.inletIndex(2, 1) = 0;  // Patch inlet 2: y-direction
    example.inletIndex(3, 0) = 2;  // Patch inlet 2: x-direction
    example.inletIndex(3, 1) = 1;  // Patch inlet 2: y-direction
    example.inletPatch.resize(2, 1);
    example.inletPatch(0, 0) = example.inletIndex(0, 0);  // Patch inlet 1
    example.inletPatch(1, 0) = example.inletIndex(2, 0);  // Patch inlet 2
    // Time parameters
    example.startTime = 0;
    example.finalTime = 12;
    example.timeStep = 0.0005;
    example.writeEvery = 0.03;
    // Perform The Offline Solve;
    example.offlineSolve();
 
    // Perform POD
    if (example.bcMethod == "lift")
    {
        // Search the lift function
        Eigen::MatrixXd BCs;
        BCs.resize(2, 2);
        BCs(0, 0) = 1;  // Patch inlet 1
        BCs(1, 0) = -1;  // Patch inlet 2
        BCs(0, 1) = 1;  // Patch inlet 1
        BCs(1, 1) = 1;  // Patch inlet 2
        example.liftSolve(BCs);
        // Normalize the lifting function
        ITHACAutilities::normalizeFields(example.liftfield);
        // Create homogeneous basis functions for velocity
        example.computeLift(example.Ufield, example.liftfield, example.Uomfield);
        // Perform a POD decomposition for velocity and pressure
        ITHACAPOD::getModes(example.Uomfield, example.Umodes, example._U().name(),
                            example.podex, 0, 0,
                            NmodesUout);
        ITHACAPOD::getModes(example.Pfield, example.Pmodes, example._p().name(),
                            example.podex, 0, 0,
                            NmodesPout);
    }
    else if (example.bcMethod == "penalty")
    {
        // Perform a POD decomposition for velocity and pressure
        ITHACAPOD::getModes(example.Ufield, example.Umodes, example._U().name(),
                            example.podex, 0, 0,
                            NmodesUout);
        ITHACAPOD::getModes(example.Pfield, example.Pmodes, example._p().name(),
                            example.podex, 0, 0,
                            NmodesPout);
    }
 
    // Reduced Matrices
    example.projectPPE("./Matrices", NmodesUproj, NmodesPproj, NmodesSUPproj);
    reducedUnsteadyNS reduced(example);
    // Set values of the online phase
    reduced.nu = 0.01;
    reduced.tstart = 0;
    reduced.finalTime = 18;
    reduced.dt = 0.0005;
    reduced.storeEvery = 0.0005;
    reduced.exportEvery = 0.03;
    // Set values velocity boundary conditions of the online phase
    Eigen::MatrixXd vel_now = par_on_BC;
 
    if (example.bcMethod == "penalty")
    {
        // Set values of the iterative penalty method
        reduced.maxIterPenalty = 100;
        reduced.tolerancePenalty = 1e-5;
        reduced.timeStepPenalty = 5;
        // Set initial quess for penalty factors
        reduced.tauIter = Eigen::MatrixXd::Zero(4, 1);
        reduced.tauIter <<  1e-6, 1e-6, 1e-6, 1e-6;
        // Solve for the penalty factors with the iterative solver
        reduced.tauU = reduced.penalty_PPE(vel_now, reduced.tauIter);
    }
 
    // Set the online temperature BC and solve reduced model
    reduced.solveOnline_PPE(vel_now);
    reduced.reconstruct(false, "./ITHACAoutput/Reconstruction/");
    exit(0);
}