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| 1 | // -*- mode: C++; tab-width: 4; indent-tabs-mode: nil; c-basic-offset: 4 -*- | ||
| 2 | // vi: set et ts=4 sw=4 sts=4: | ||
| 3 | // | ||
| 4 | // SPDX-FileCopyrightInfo: Copyright © DuMux Project contributors, see AUTHORS.md in root folder | ||
| 5 | // SPDX-License-Identifier: GPL-3.0-or-later | ||
| 6 | // | ||
| 7 | /*! | ||
| 8 | * \file | ||
| 9 | * \ingroup NavierStokesModel | ||
| 10 | * \copydoc Dumux::NavierStokesResidualImpl | ||
| 11 | */ | ||
| 12 | #ifndef DUMUX_NAVIERSTOKES_MOMENTUM_LOCAL_RESIDUAL_HH | ||
| 13 | #define DUMUX_NAVIERSTOKES_MOMENTUM_LOCAL_RESIDUAL_HH | ||
| 14 | |||
| 15 | #include <dumux/common/numeqvector.hh> | ||
| 16 | #include <dumux/common/properties.hh> | ||
| 17 | #include <dumux/discretization/extrusion.hh> | ||
| 18 | #include <dumux/discretization/method.hh> | ||
| 19 | #include <dumux/assembly/fclocalresidual.hh> | ||
| 20 | #include <dune/common/hybridutilities.hh> | ||
| 21 | |||
| 22 | namespace Dumux { | ||
| 23 | |||
| 24 | /*! | ||
| 25 | * \ingroup NavierStokesModel | ||
| 26 | * \brief Element-wise calculation of the Navier-Stokes residual for models using the staggered discretization | ||
| 27 | */ | ||
| 28 | template<class TypeTag> | ||
| 29 | class NavierStokesMomentumResidual | ||
| 30 | : public FaceCenteredLocalResidual<TypeTag> | ||
| 31 | { | ||
| 32 | using ParentType = FaceCenteredLocalResidual<TypeTag>; | ||
| 33 | friend class FaceCenteredLocalResidual<TypeTag>; | ||
| 34 | |||
| 35 | using GridVariables = GetPropType<TypeTag, Properties::GridVariables>; | ||
| 36 | |||
| 37 | using GridVolumeVariables = typename GridVariables::GridVolumeVariables; | ||
| 38 | using ElementVolumeVariables = typename GridVolumeVariables::LocalView; | ||
| 39 | using VolumeVariables = typename GridVolumeVariables::VolumeVariables; | ||
| 40 | |||
| 41 | using GridFluxVariablesCache = typename GridVariables::GridFluxVariablesCache; | ||
| 42 | using ElementFluxVariablesCache = typename GridFluxVariablesCache::LocalView; | ||
| 43 | |||
| 44 | using Scalar = GetPropType<TypeTag, Properties::Scalar>; | ||
| 45 | using Implementation = GetPropType<TypeTag, Properties::LocalResidual>; | ||
| 46 | using Problem = GetPropType<TypeTag, Properties::Problem>; | ||
| 47 | using GridGeometry = GetPropType<TypeTag, Properties::GridGeometry>; | ||
| 48 | using FVElementGeometry = typename GridGeometry::LocalView; | ||
| 49 | using SubControlVolume = typename FVElementGeometry::SubControlVolume; | ||
| 50 | using SubControlVolumeFace = typename FVElementGeometry::SubControlVolumeFace; | ||
| 51 | using GridView = typename GridGeometry::GridView; | ||
| 52 | using Element = typename GridView::template Codim<0>::Entity; | ||
| 53 | using ElementBoundaryTypes = GetPropType<TypeTag, Properties::ElementBoundaryTypes>; | ||
| 54 | using FluxVariables = GetPropType<TypeTag, Properties::FluxVariables>; | ||
| 55 | using Indices = typename GetPropType<TypeTag, Properties::ModelTraits>::Indices; | ||
| 56 | using NumEqVector = Dumux::NumEqVector<GetPropType<TypeTag, Properties::PrimaryVariables>>; | ||
| 57 | |||
| 58 | using Extrusion = Extrusion_t<GridGeometry>; | ||
| 59 | |||
| 60 | using ModelTraits = GetPropType<TypeTag, Properties::ModelTraits>; | ||
| 61 | |||
| 62 | static constexpr auto dim = GridView::dimension; | ||
| 63 | |||
| 64 | public: | ||
| 65 | //! Use the parent type's constructor | ||
| 66 |
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5211676 | using ParentType::ParentType; |
| 67 | |||
| 68 | /*! | ||
| 69 | * \brief Calculate the source term of the equation | ||
| 70 | * | ||
| 71 | * \param problem The problem to solve | ||
| 72 | * \param scv The sub-control volume over which we integrate the storage term | ||
| 73 | * \param volVars The volume variables associated with the scv | ||
| 74 | * \param isPreviousStorage Bool transferring the information if the storage term is computed at the current or previous time step | ||
| 75 | * \note has to be implemented by the model specific residual class | ||
| 76 | * | ||
| 77 | */ | ||
| 78 | 104823040 | NumEqVector computeStorage(const Problem& problem, | |
| 79 | const SubControlVolume& scv, | ||
| 80 | const VolumeVariables& volVars, | ||
| 81 | const bool isPreviousStorage = false) const | ||
| 82 | { | ||
| 83 | 209646080 | const auto& element = problem.gridGeometry().element(scv.elementIndex()); | |
| 84 |
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104823040 | return problem.density(element, scv, isPreviousStorage) * volVars.velocity(); |
| 85 | } | ||
| 86 | |||
| 87 | /*! | ||
| 88 | * \brief Calculate the source term of the equation | ||
| 89 | * | ||
| 90 | * \param problem The problem to solve | ||
| 91 | * \param element The DUNE Codim<0> entity for which the residual | ||
| 92 | * ought to be calculated | ||
| 93 | * \param fvGeometry The finite-volume geometry of the element | ||
| 94 | * \param elemVolVars The volume variables associated with the element stencil | ||
| 95 | * \param scv The sub-control volume over which we integrate the source term | ||
| 96 | * \note This is the default implementation for all models as sources are computed | ||
| 97 | * in the user interface of the problem | ||
| 98 | * | ||
| 99 | */ | ||
| 100 | 43559688 | NumEqVector computeSource(const Problem& problem, | |
| 101 | const Element& element, | ||
| 102 | const FVElementGeometry& fvGeometry, | ||
| 103 | const ElementVolumeVariables& elemVolVars, | ||
| 104 | const SubControlVolume& scv) const | ||
| 105 | { | ||
| 106 |
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43790472 | NumEqVector source = ParentType::computeSource(problem, element, fvGeometry, elemVolVars, scv); |
| 107 |
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130679064 | source += problem.gravity()[scv.dofAxis()] * problem.density(element, scv); |
| 108 | |||
| 109 | // Axisymmetric problems in 2D feature an extra source terms arising from the transformation to cylindrical coordinates. | ||
| 110 | // See Ferziger/Peric: Computational methods for fluid dynamics chapter 8. | ||
| 111 | // https://doi.org/10.1007/978-3-540-68228-8 (page 301) | ||
| 112 | if constexpr (dim == 2 && isRotationalExtrusion<Extrusion>) | ||
| 113 | { | ||
| 114 |
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2753520 | if (scv.dofAxis() == Extrusion::radialAxis) |
| 115 | { | ||
| 116 |
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4130280 | const auto r = scv.center()[scv.dofAxis()] - fvGeometry.gridGeometry().bBoxMin()[scv.dofAxis()]; |
| 117 | 1376760 | const auto& scvf = (*scvfs(fvGeometry, scv).begin()); // the frontal scvf belonging to the scv | |
| 118 | |||
| 119 | // Velocity term | ||
| 120 | 1376760 | source -= -2.0*problem.effectiveViscosity(element, fvGeometry, scvf) * elemVolVars[scv].velocity() / (r*r); | |
| 121 | |||
| 122 | // Pressure term (needed because we incorporate pressure in terms of a surface integral). | ||
| 123 | // grad(p) becomes div(pI) + (p/r)*n_r in cylindrical coordinates. The second term | ||
| 124 | // is new with respect to Cartesian coordinates and handled below as a source term. | ||
| 125 | 1376760 | source += problem.pressure(element, fvGeometry, scvf)/r; | |
| 126 | } | ||
| 127 | } | ||
| 128 | |||
| 129 | 43559688 | return source; | |
| 130 | } | ||
| 131 | |||
| 132 | /*! | ||
| 133 | * \brief Evaluates the mass flux over a face of a sub control volume. | ||
| 134 | * | ||
| 135 | * \param problem The problem | ||
| 136 | * \param element The element | ||
| 137 | * \param fvGeometry The finite volume geometry context | ||
| 138 | * \param elemVolVars The volume variables for all flux stencil elements | ||
| 139 | * \param scvf The sub control volume face to compute the flux on | ||
| 140 | * \param elemFluxVarsCache The cache related to flux computation | ||
| 141 | * \param elemBcTypes The element boundary condition types | ||
| 142 | */ | ||
| 143 | 279435948 | NumEqVector computeFlux(const Problem& problem, | |
| 144 | const Element& element, | ||
| 145 | const FVElementGeometry& fvGeometry, | ||
| 146 | const ElementVolumeVariables& elemVolVars, | ||
| 147 | const SubControlVolumeFace& scvf, | ||
| 148 | const ElementFluxVariablesCache& elemFluxVarsCache, | ||
| 149 | const ElementBoundaryTypes& elemBcTypes) const | ||
| 150 | { | ||
| 151 | 279435948 | FluxVariables fluxVars(problem, element, fvGeometry, scvf, elemVolVars, elemFluxVarsCache, elemBcTypes); | |
| 152 | |||
| 153 | 279435948 | NumEqVector flux(0.0); | |
| 154 | 279435948 | flux += fluxVars.advectiveMomentumFlux(); | |
| 155 | 279435948 | flux += fluxVars.diffusiveMomentumFlux(); | |
| 156 | 279435948 | flux += fluxVars.pressureContribution(); | |
| 157 | 279435948 | return flux; | |
| 158 | } | ||
| 159 | |||
| 160 | //! Evaluate flux residuals for one sub control volume face when the element features at least one Dirichlet boundary condition | ||
| 161 | //! Skip the flux calculation if the DOF of the associated sub control volume features an appropriate Dirichlet condition. | ||
| 162 | 17156648 | NumEqVector maybeHandleDirichletBoundary(const Problem& problem, | |
| 163 | const Element& element, | ||
| 164 | const FVElementGeometry& fvGeometry, | ||
| 165 | const ElementVolumeVariables& elemVolVars, | ||
| 166 | const ElementBoundaryTypes& elemBcTypes, | ||
| 167 | const ElementFluxVariablesCache& elemFluxVarsCache, | ||
| 168 | const SubControlVolumeFace& scvf) const | ||
| 169 | { | ||
| 170 |
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34313296 | if (const auto& scv = fvGeometry.scv(scvf.insideScvIdx()); scv.boundary()) |
| 171 | { | ||
| 172 | 5191452 | const auto& frontalScvfOnBoundary = fvGeometry.frontalScvfOnBoundary(scv); | |
| 173 | 5191452 | const auto& bcTypes = elemBcTypes[frontalScvfOnBoundary.localIndex()]; | |
| 174 |
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5191452 | if (bcTypes.isDirichlet(scv.dofAxis())) |
| 175 | 5081404 | return NumEqVector(0.0); // skip calculation as Dirichlet BC will be incorporated explicitly by assembler. | |
| 176 | } | ||
| 177 | |||
| 178 | // Default: The scv does not lie on a boundary with a Dirichlet condition for the velocity in normal direction. | ||
| 179 | // Check for a Neumann condition or calculate the flux as normal. | ||
| 180 |
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12075244 | if (elemBcTypes.hasNeumann()) |
| 181 | 667494 | return this->asImp().maybeHandleNeumannBoundary(problem, element, fvGeometry, elemVolVars, elemBcTypes, elemFluxVarsCache, scvf); | |
| 182 | else | ||
| 183 | 11407750 | return this->asImp().computeFlux(problem, element, fvGeometry, elemVolVars, scvf, elemFluxVarsCache, elemBcTypes); | |
| 184 | } | ||
| 185 | |||
| 186 | //! Evaluate flux residuals for one sub control volume face when the element features at least one Neumann boundary condition | ||
| 187 | //! This requires special care. | ||
| 188 | 3478292 | NumEqVector maybeHandleNeumannBoundary(const Problem& problem, | |
| 189 | const Element& element, | ||
| 190 | const FVElementGeometry& fvGeometry, | ||
| 191 | const ElementVolumeVariables& elemVolVars, | ||
| 192 | const ElementBoundaryTypes& elemBcTypes, | ||
| 193 | const ElementFluxVariablesCache& elemFluxVarsCache, | ||
| 194 | const SubControlVolumeFace& scvf) const | ||
| 195 | { | ||
| 196 | static_assert(FVElementGeometry::GridGeometry::discMethod == DiscretizationMethods::fcstaggered); // TODO overload this method for different discretizations | ||
| 197 | static_assert( | ||
| 198 | std::decay_t<decltype( | ||
| 199 | problem.neumann(element, fvGeometry, elemVolVars, elemFluxVarsCache, scvf) | ||
| 200 | )>::size() == ModelTraits::dim(), | ||
| 201 | "The momentum model expects problem.neumann to return a vector of size dim. " | ||
| 202 | "When in doubt you should be able to use 'using NumEqVector = typename ParentType::NumEqVector;'." | ||
| 203 | ); | ||
| 204 |
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3478292 | assert(elemBcTypes.hasNeumann()); |
| 205 | |||
| 206 |
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6956584 | const auto& scv = fvGeometry.scv(scvf.insideScvIdx()); |
| 207 | |||
| 208 |
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3478292 | if (scv.boundary()) |
| 209 | { | ||
| 210 | // This is the most simple case for a frontal scvf lying directly on the boundary. | ||
| 211 | // Just evaluate the Neumann flux for the normal velocity component. | ||
| 212 | // | ||
| 213 | // ---------------- * || frontal face of staggered half-control-volume | ||
| 214 | // | || # * | ||
| 215 | // | || # * D dof position (coincides with integration point where | ||
| 216 | // | || scv D * the Neumann flux is evaluated, here for x component) | ||
| 217 | // | || # * | ||
| 218 | // | || # * -- element boundaries | ||
| 219 | // ---------------- * | ||
| 220 | // y * domain boundary | ||
| 221 | // ^ | ||
| 222 | // | # current scvf over which Neumann flux is evaluated | ||
| 223 | // ----> x | ||
| 224 | // | ||
| 225 |
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819120 | if (scvf.boundary() && scvf.isFrontal()) |
| 226 | { | ||
| 227 | 186614 | const auto& bcTypes = elemBcTypes[scvf.localIndex()]; | |
| 228 |
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373228 | if (bcTypes.hasNeumann() && bcTypes.isNeumann(scv.dofAxis())) |
| 229 | { | ||
| 230 | 186614 | const auto neumannFluxes = problem.neumann(element, fvGeometry, elemVolVars, elemFluxVarsCache, scvf); | |
| 231 | 568466 | return neumannFluxes[scv.dofAxis()] * Extrusion::area(fvGeometry, scvf) * elemVolVars[scv].extrusionFactor(); | |
| 232 | } | ||
| 233 | } | ||
| 234 |
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632506 | else if (scvf.isLateral()) |
| 235 | { | ||
| 236 | // If a sub control volume lies on a boundary, Neumann fluxes also need to be considered for its lateral faces, | ||
| 237 | // even though those do not necessarily lie on a boundary (only their edges / integration points are touching the boundary). | ||
| 238 | // We cannot simply calculate momentum fluxes across the lateral boundary in this situation because we might not | ||
| 239 | // have enough information at the boundary to do so. | ||
| 240 | // We first need to find the scv's frontal face on the boundary to check if there actually is a Neumann BC. | ||
| 241 | // Afterwards, we use the actual (lateral) scvf to retrieve the Neumann flux at its integration point intersecting with the boundary. | ||
| 242 | // | ||
| 243 | // | ||
| 244 | // ---------######O * || frontal face of staggered half-control-volume | ||
| 245 | // | || : * | ||
| 246 | // | || : * D dof position | ||
| 247 | // | || scv D * | ||
| 248 | // | || : * -- element boundaries | ||
| 249 | // | || : * | ||
| 250 | // ---------------- * * domain boundary | ||
| 251 | // | ||
| 252 | // y # current scvf over which Neumann flux is evaluated | ||
| 253 | // ^ | ||
| 254 | // | : frontal scvf on boundary | ||
| 255 | // ----> x | ||
| 256 | // O integration point at which Neumann flux is evaluated (here for y component) | ||
| 257 | // | ||
| 258 | 445892 | const auto& frontalScvfOnBoundary = fvGeometry.frontalScvfOnBoundary(scv); | |
| 259 |
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445892 | assert(frontalScvfOnBoundary.isFrontal() && frontalScvfOnBoundary.boundary()); |
| 260 | 445892 | const auto& bcTypes = elemBcTypes[frontalScvfOnBoundary.localIndex()]; | |
| 261 |
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891784 | if (bcTypes.hasNeumann() && bcTypes.isNeumann(scvf.normalAxis())) |
| 262 | { | ||
| 263 | 442308 | const auto neumannFluxes = problem.neumann(element, fvGeometry, elemVolVars, elemFluxVarsCache, scvf); | |
| 264 | 1326924 | return neumannFluxes[scv.dofAxis()] * Extrusion::area(fvGeometry, scvf) * elemVolVars[scv].extrusionFactor(); | |
| 265 | } | ||
| 266 | } | ||
| 267 | } | ||
| 268 |
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2659172 | else if (scvf.boundary()) |
| 269 | { | ||
| 270 | // Here, the lateral face does lie on a boundary. Retrieve the Neumann flux component for | ||
| 271 | // the corresponding scvs' DOF orientation. | ||
| 272 | // | ||
| 273 | // | ||
| 274 | // ***************** | ||
| 275 | // ---------######O || frontal face of staggered half-control-volume | ||
| 276 | // | || : | ||
| 277 | // | || : D dof position | ||
| 278 | // | || scv D | ||
| 279 | // | || : -- element boundaries | ||
| 280 | // | || : | ||
| 281 | // ---------------- * domain boundary | ||
| 282 | // | ||
| 283 | // y # current scvf over which Neumann flux is evaluated | ||
| 284 | // ^ | ||
| 285 | // | : frontal scvf on boundary | ||
| 286 | // ----> x | ||
| 287 | // O integration point at which Neumann flux is evaluated (here for x component) | ||
| 288 | // | ||
| 289 |
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564220 | assert(scvf.isLateral()); |
| 290 | 564220 | const auto& bcTypes = elemBcTypes[scvf.localIndex()]; | |
| 291 |
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1128440 | if (bcTypes.hasNeumann() && bcTypes.isNeumann(scv.dofAxis())) |
| 292 | { | ||
| 293 | 499944 | const auto neumannFluxes = problem.neumann(element, fvGeometry, elemVolVars, elemFluxVarsCache, scvf); | |
| 294 | 1499832 | return neumannFluxes[scv.dofAxis()] * Extrusion::area(fvGeometry, scvf) * elemVolVars[scv].extrusionFactor(); | |
| 295 | } | ||
| 296 | } | ||
| 297 | |||
| 298 | // Default: Neither the scvf itself nor a lateral one considers a Neumann flux. We just calculate the flux as normal. | ||
| 299 | 2349426 | return this->asImp().computeFlux(problem, element, fvGeometry, elemVolVars, scvf, elemFluxVarsCache, elemBcTypes); | |
| 300 | } | ||
| 301 | |||
| 302 | //! Returns the implementation of the problem (i.e. static polymorphism) | ||
| 303 | Implementation &asImp_() | ||
| 304 | { return *static_cast<Implementation *>(this); } | ||
| 305 | |||
| 306 | //! \copydoc asImp_() | ||
| 307 | const Implementation &asImp_() const | ||
| 308 | { return *static_cast<const Implementation *>(this); } | ||
| 309 | }; | ||
| 310 | |||
| 311 | } // end namespace Dumux | ||
| 312 | |||
| 313 | #endif | ||
| 314 |