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592 | // *****************************************************************************
/*!
\file src/PDE/Integrate/Boundary.cpp
\copyright 2012-2015 J. Bakosi,
2016-2018 Los Alamos National Security, LLC.,
2019-2021 Triad National Security, LLC.
All rights reserved. See the LICENSE file for details.
\brief Functions for computing physical boundary surface integrals of a
system of PDEs in DG methods
\details This file contains functionality for computing physical boundary
surface integrals of a system of PDEs used in discontinuous Galerkin
methods for various orders of numerical representation.
*/
// *****************************************************************************
#include <array>
#include "Basis.hpp"
#include "Boundary.hpp"
#include "Vector.hpp"
#include "Quadrature.hpp"
#include "MultiMatTerms.hpp"
#include "MultiMat/MultiMatIndexing.hpp"
#include "Reconstruction.hpp"
#include "Inciter/InputDeck/InputDeck.hpp"
namespace inciter {
extern ctr::InputDeck g_inputdeck;
}
namespace tk {
void
bndSurfInt( const bool pref,
std::size_t nmat,
const std::vector< inciter::EOS >& mat_blk,
const std::size_t ndof,
const std::size_t rdof,
const std::vector< std::size_t >& bcconfig,
const inciter::FaceData& fd,
const Fields& geoFace,
const Fields& geoElem,
const std::vector< std::size_t >& inpoel,
const UnsMesh::Coords& coord,
real t,
const RiemannFluxFn& flux,
const VelFn& vel,
const StateFn& state,
const Fields& U,
const Fields& P,
const std::vector< std::size_t >& ndofel,
Fields& R,
std::vector< std::vector< tk::real > >& riemannDeriv,
int intsharp )
// *****************************************************************************
//! Compute boundary surface flux integrals for a given boundary type for DG
//! \details This function computes contributions from surface integrals along
//! all faces for a particular boundary condition type, configured by the state
//! function
//! \param[in] pref Indicator for p-adaptive algorithm
//! \param[in] nmat Number of materials in this PDE system
//! \param[in] mat_blk EOS material block
//! \param[in] ndof Maximum number of degrees of freedom
//! \param[in] rdof Maximum number of reconstructed degrees of freedom
//! \param[in] bcconfig BC configuration vector for multiple side sets
//! \param[in] fd Face connectivity and boundary conditions object
//! \param[in] geoFace Face geometry array
//! \param[in] geoElem Element geometry array
//! \param[in] inpoel Element-node connectivity
//! \param[in] coord Array of nodal coordinates
//! \param[in] t Physical time
//! \param[in] flux Riemann flux function to use
//! \param[in] vel Function to use to query prescribed velocity (if any)
//! \param[in] state Function to evaluate the left and right solution state at
//! boundaries
//! \param[in] U Solution vector at recent time step
//! \param[in] P Vector of primitives at recent time step
//! \param[in] ndofel Vector of local number of degrees of freedom
//! \param[in,out] R Right-hand side vector computed
//! \param[in,out] riemannDeriv Derivatives of partial-pressures and velocities
//! computed from the Riemann solver for use in the non-conservative terms.
//! These derivatives are used only for multi-material hydro and unused for
//! single-material compflow and linear transport.
//! \param[in] intsharp Interface compression tag, an optional argument, with
//! default 0, so that it is unused for single-material and transport.
// *****************************************************************************
{
const auto& bface = fd.Bface();
const auto& esuf = fd.Esuf();
const auto& inpofa = fd.Inpofa();
const auto& cx = coord[0];
const auto& cy = coord[1];
const auto& cz = coord[2];
auto ncomp = U.nprop()/rdof;<--- Variable 'ncomp' is assigned a value that is never used.
auto nprim = P.nprop()/rdof;<--- Variable 'nprim' is assigned a value that is never used.
//Assert( (nmat==1 ? riemannDeriv.empty() : true), "Non-empty Riemann "
// "derivative vector for single material compflow" );
for (const auto& s : bcconfig) { // for all bc sidesets
auto bc = bface.find(static_cast<int>(s));// faces for side set
if (bc != end(bface))
{
for (const auto& f : bc->second)
{
Assert( esuf[2*f+1] == -1, "outside boundary element not -1" );
std::size_t el = static_cast< std::size_t >(esuf[2*f]);
auto ng = tk::NGfa(ndofel[el]);
// arrays for quadrature points
std::array< std::vector< real >, 2 > coordgp;
std::vector< real > wgp;
coordgp[0].resize( ng );
coordgp[1].resize( ng );
wgp.resize( ng );
// get quadrature point weights and coordinates for triangle
GaussQuadratureTri( ng, coordgp, wgp );
// Extract the left element coordinates
std::array< std::array< tk::real, 3>, 4 > coordel_l {{
{{ cx[ inpoel[4*el ] ], cy[ inpoel[4*el ] ], cz[ inpoel[4*el ] ] }},
{{ cx[ inpoel[4*el+1] ], cy[ inpoel[4*el+1] ], cz[ inpoel[4*el+1] ] }},
{{ cx[ inpoel[4*el+2] ], cy[ inpoel[4*el+2] ], cz[ inpoel[4*el+2] ] }},
{{ cx[ inpoel[4*el+3] ], cy[ inpoel[4*el+3] ], cz[ inpoel[4*el+3] ] }} }};
// Compute the determinant of Jacobian matrix
auto detT_l =
Jacobian( coordel_l[0], coordel_l[1], coordel_l[2], coordel_l[3] );
// Extract the face coordinates
std::array< std::array< tk::real, 3>, 3 > coordfa {{
{{ cx[ inpofa[3*f ] ], cy[ inpofa[3*f ] ], cz[ inpofa[3*f ] ] }},
{{ cx[ inpofa[3*f+1] ], cy[ inpofa[3*f+1] ], cz[ inpofa[3*f+1] ] }},
{{ cx[ inpofa[3*f+2] ], cy[ inpofa[3*f+2] ], cz[ inpofa[3*f+2] ] }} }};
std::array< real, 3 >
fn{{ geoFace(f,1), geoFace(f,2), geoFace(f,3) }};
// Gaussian quadrature
for (std::size_t igp=0; igp<ng; ++igp)
{
// Compute the coordinates of quadrature point at physical domain
auto gp = eval_gp( igp, coordfa, coordgp );
// If an rDG method is set up (P0P1), then, currently we compute the P1
// basis functions and solutions by default. This implies that P0P1 is
// unsupported in the p-adaptive DG (PDG). This is a workaround until
// we have rdofel, which is needed to distinguish between ndofs and
// rdofs per element for pDG.
std::size_t dof_el;
if (rdof > ndof)
{
dof_el = rdof;
}
else
{
dof_el = ndofel[el];
}
// For multi-material p-adaptive simulation, when dofel = 1, p0p1 is applied and ndof
// for solution evaluation should be 4
if(ncomp > 5 && dof_el == 1 && pref)
dof_el = 4;
std::array< tk::real, 3> ref_gp_l{
Jacobian( coordel_l[0], gp, coordel_l[2], coordel_l[3] ) / detT_l,
Jacobian( coordel_l[0], coordel_l[1], gp, coordel_l[3] ) / detT_l,
Jacobian( coordel_l[0], coordel_l[1], coordel_l[2], gp ) / detT_l };
//Compute the basis functions for the left element
auto B_l = eval_basis( dof_el, ref_gp_l[0], ref_gp_l[1], ref_gp_l[2] );
auto wt = wgp[igp] * geoFace(f,0);<--- Variable 'wt' is assigned a value that is never used.
// Compute the state variables at the left element
auto ugp = evalPolynomialSol(mat_blk, intsharp, ncomp, nprim,
rdof, nmat, el, dof_el, inpoel, coord, geoElem, ref_gp_l, B_l, U, P);
Assert( ugp.size() == ncomp+nprim, "Incorrect size for "
"appended boundary state vector" );
auto var = state( ncomp, mat_blk, ugp, gp[0], gp[1], gp[2], t, fn );
// Compute the numerical flux
auto fl = flux(mat_blk, fn, var, vel(ncomp, gp[0], gp[1], gp[2], t));
// Code below commented until details about the form of these terms in
// the \alpha_k g_k equations are sorted out.
// // Add RHS inverse deformation terms if necessary
// if (haveSolid)
// solidTermsSurfInt( nmat, ndof, rdof, fn, el, er, solidx, geoElem, U,
// coordel_l, coordel_r, igp, coordgp, dt, fl );
// Add the surface integration term to the rhs
update_rhs_bc( ncomp, nmat, ndof, ndofel[el], wt, fn, el, fl,
B_l, R, riemannDeriv );
}
}
}
}
}
void
update_rhs_bc ( ncomp_t ncomp,
std::size_t nmat,
const std::size_t ndof,
const std::size_t ndof_l,
const tk::real wt,
const std::array< tk::real, 3 >& fn,
const std::size_t el,
const std::vector< tk::real >& fl,
const std::vector< tk::real >& B_l,
Fields& R,<--- Parameter 'R' can be declared with const
std::vector< std::vector< tk::real > >& riemannDeriv )
// *****************************************************************************
// Update the rhs by adding the boundary surface integration term
//! \param[in] ncomp Number of scalar components in this PDE system
//! \param[in] nmat Number of materials in this PDE system
//! \param[in] ndof Maximum number of degrees of freedom
//! \param[in] ndof_l Number of degrees of freedom for the left element
//! \param[in] wt Weight of gauss quadrature point
//! \param[in] fn Face/Surface normal
//! \param[in] el Left element index
//! \param[in] fl Surface flux
//! \param[in] B_l Basis function for the left element
//! \param[in,out] R Right-hand side vector computed
//! \param[in,out] riemannDeriv Derivatives of partial-pressures and velocities
//! computed from the Riemann solver for use in the non-conservative terms.
//! These derivatives are used only for multi-material hydro and unused for
//! single-material compflow and linear transport.
// *****************************************************************************
{
// following line commented until rdofel is made available.
//Assert( B_l.size() == ndof_l, "Size mismatch" );
using inciter::newSolidsAccFn;
const auto& solidx =
inciter::g_inputdeck.get< tag::matidxmap, tag::solidx >();
for (ncomp_t c=0; c<ncomp; ++c)
{
auto mark = c*ndof;
R(el, mark) -= wt * fl[c];
if(ndof_l > 1) //DG(P1)
{
R(el, mark+1) -= wt * fl[c] * B_l[1];
R(el, mark+2) -= wt * fl[c] * B_l[2];
R(el, mark+3) -= wt * fl[c] * B_l[3];
}
if(ndof_l > 4) //DG(P2)
{
R(el, mark+4) -= wt * fl[c] * B_l[4];
R(el, mark+5) -= wt * fl[c] * B_l[5];
R(el, mark+6) -= wt * fl[c] * B_l[6];
R(el, mark+7) -= wt * fl[c] * B_l[7];
R(el, mark+8) -= wt * fl[c] * B_l[8];
R(el, mark+9) -= wt * fl[c] * B_l[9];
}
}
// Prep for non-conservative terms in multimat
if (fl.size() > ncomp)
{
// Gradients of partial pressures
for (std::size_t k=0; k<nmat; ++k)
{
for (std::size_t idir=0; idir<3; ++idir)
riemannDeriv[3*k+idir][el] += wt * fl[ncomp+k] * fn[idir];
}
// Divergence of velocity multiples basis fucntion( d(uB) / dx )
for(std::size_t idof = 0; idof < ndof_l; idof++)
riemannDeriv[3*nmat+idof][el] += wt * fl[ncomp+nmat] * B_l[idof];
// Divergence of asigma: d(asig_ij)/dx_j
for (std::size_t k=0; k<nmat; ++k)
if (solidx[k] > 0)
{
std::size_t mark = ncomp+nmat+1+3*(solidx[k]-1);
for (std::size_t i=0; i<3; ++i)
riemannDeriv[3*nmat+ndof+3*(solidx[k]-1)+i][el] -=
wt * fl[mark+i];
}
}
}
void
bndSurfIntFV(
std::size_t nmat,
const std::vector< inciter::EOS >& mat_blk,
const std::size_t rdof,
const std::vector< std::size_t >& bcconfig,
const inciter::FaceData& fd,
const Fields& geoFace,
const Fields& geoElem,
const std::vector< std::size_t >& inpoel,
const UnsMesh::Coords& coord,
real t,
const RiemannFluxFn& flux,
const VelFn& vel,
const StateFn& state,
const Fields& U,
const Fields& P,
const std::vector< int >& srcFlag,
Fields& R,
int intsharp )
// *****************************************************************************
//! Compute boundary surface flux integrals for a given boundary type for FV
//! \details This function computes contributions from surface integrals along
//! all faces for a particular boundary condition type, configured by the state
//! function
//! \param[in] nmat Number of materials in this PDE system
//! \param[in] mat_blk EOS material block
//! \param[in] rdof Maximum number of reconstructed degrees of freedom
//! \param[in] bcconfig BC configuration vector for multiple side sets
//! \param[in] fd Face connectivity and boundary conditions object
//! \param[in] geoFace Face geometry array
//! \param[in] geoElem Element geometry array
//! \param[in] inpoel Element-node connectivity
//! \param[in] coord Array of nodal coordinates
//! \param[in] t Physical time
//! \param[in] flux Riemann flux function to use
//! \param[in] vel Function to use to query prescribed velocity (if any)
//! \param[in] state Function to evaluate the left and right solution state at
//! boundaries
//! \param[in] U Solution vector at recent time step
//! \param[in] P Vector of primitives at recent time step
//! \param[in] srcFlag Whether the energy source was added
//! \param[in,out] R Right-hand side vector computed
//! \param[in] intsharp Interface compression tag, an optional argument, with
//! default 0, so that it is unused for single-material and transport.
// *****************************************************************************
{
const auto& bface = fd.Bface();
const auto& esuf = fd.Esuf();
const auto& cx = coord[0];
const auto& cy = coord[1];
const auto& cz = coord[2];
auto ncomp = U.nprop()/rdof;<--- Variable 'ncomp' is assigned a value that is never used.
auto nprim = P.nprop()/rdof;<--- Variable 'nprim' is assigned a value that is never used.
for (const auto& s : bcconfig) { // for all bc sidesets
auto bc = bface.find(static_cast<int>(s));// faces for side set
if (bc != end(bface))
{
for (const auto& f : bc->second)
{
Assert( esuf[2*f+1] == -1, "outside boundary element not -1" );
std::size_t el = static_cast< std::size_t >(esuf[2*f]);
// Extract the left element coordinates
std::array< std::array< tk::real, 3>, 4 > coordel_l {{
{{ cx[ inpoel[4*el ] ], cy[ inpoel[4*el ] ], cz[ inpoel[4*el ] ] }},
{{ cx[ inpoel[4*el+1] ], cy[ inpoel[4*el+1] ], cz[ inpoel[4*el+1] ] }},
{{ cx[ inpoel[4*el+2] ], cy[ inpoel[4*el+2] ], cz[ inpoel[4*el+2] ] }},
{{ cx[ inpoel[4*el+3] ], cy[ inpoel[4*el+3] ], cz[ inpoel[4*el+3] ] }} }};
// Compute the determinant of Jacobian matrix
auto detT_l =
Jacobian( coordel_l[0], coordel_l[1], coordel_l[2], coordel_l[3] );
// face normal
std::array< real, 3 >
fn{{ geoFace(f,1), geoFace(f,2), geoFace(f,3) }};
// face centroid
std::array< real, 3 >
gp{{ geoFace(f,4), geoFace(f,5), geoFace(f,6) }};
std::array< tk::real, 3> ref_gp_l{
Jacobian( coordel_l[0], gp, coordel_l[2], coordel_l[3] ) / detT_l,
Jacobian( coordel_l[0], coordel_l[1], gp, coordel_l[3] ) / detT_l,
Jacobian( coordel_l[0], coordel_l[1], coordel_l[2], gp ) / detT_l };
//Compute the basis functions for the left element
auto B_l = eval_basis( rdof, ref_gp_l[0], ref_gp_l[1], ref_gp_l[2] );
// Compute the state variables at the left element
auto ugp = evalFVSol(mat_blk, intsharp, ncomp, nprim,
rdof, nmat, el, inpoel, coord, geoElem, ref_gp_l, B_l, U, P,
srcFlag[el]);
Assert( ugp.size() == ncomp+nprim, "Incorrect size for "
"appended boundary state vector" );
auto var = state( ncomp, mat_blk, ugp, gp[0], gp[1], gp[2], t, fn );
// Compute the numerical flux
auto fl = flux( mat_blk, fn, var, vel(ncomp, gp[0], gp[1], gp[2], t) );
// compute non-conservative terms
std::vector< tk::real > var_riemann(nmat+1, 0.0);
for (std::size_t k=0; k<nmat+1; ++k) var_riemann[k] = fl[ncomp+k];
auto ncf_l = nonConservativeIntFV(nmat, rdof, el, fn, U, P, var_riemann);
// Add the surface integration term to the rhs
for (ncomp_t c=0; c<ncomp; ++c)
{
R(el, c) -= geoFace(f,0) * (fl[c] - ncf_l[c]);
}
}
}
}
}
void
bndSurfIntViscousFV(
std::size_t nmat,
const std::vector< inciter::EOS >& mat_blk,
const std::size_t rdof,
const std::vector< std::size_t >& bcconfig,
const inciter::FaceData& fd,
const Fields& geoFace,
const Fields& geoElem,
const std::vector< std::size_t >& inpoel,
const UnsMesh::Coords& coord,
real t,
const StateFn& state,
const StateFn& gradFn,
const Fields& U,
const Fields& P,
const std::vector< int >& srcFlag,
Fields& R,
int intsharp )
// *****************************************************************************
//! Compute boundary surface flux integrals for a given boundary type for FV
//! \details This function computes contributions from surface integrals along
//! all faces for a particular boundary condition type, configured by the state
//! function
//! \param[in] nmat Number of materials in this PDE system
//! \param[in] mat_blk EOS material block
//! \param[in] rdof Maximum number of reconstructed degrees of freedom
//! \param[in] bcconfig BC configuration vector for multiple side sets
//! \param[in] fd Face connectivity and boundary conditions object
//! \param[in] geoFace Face geometry array
//! \param[in] geoElem Element geometry array
//! \param[in] inpoel Element-node connectivity
//! \param[in] coord Array of nodal coordinates
//! \param[in] t Physical time
//! \param[in] state Function to evaluate the left and right solution state at
//! boundaries
//! \param[in] gradFn Function to evaluate the left and right solution gradients
//! at boundaries
//! \param[in] U Solution vector at recent time step
//! \param[in] P Vector of primitives at recent time step
//! \param[in] srcFlag Whether the energy source was added
//! \param[in,out] R Right-hand side vector computed
//! \param[in] intsharp Interface compression tag, an optional argument, with
//! default 0, so that it is unused for single-material and transport.
// *****************************************************************************
{
using inciter::velocityDofIdx;
const auto& bface = fd.Bface();
const auto& esuf = fd.Esuf();
const auto& cx = coord[0];
const auto& cy = coord[1];
const auto& cz = coord[2];
auto ncomp = U.nprop()/rdof;<--- Variable 'ncomp' is assigned a value that is never used.
auto nprim = P.nprop()/rdof;<--- Variable 'nprim' is assigned a value that is never used.
for (const auto& s : bcconfig) { // for all bc sidesets
auto bc = bface.find(static_cast<int>(s));// faces for side set
if (bc != end(bface))
{
for (const auto& f : bc->second)
{
Assert( esuf[2*f+1] == -1, "outside boundary element not -1" );
std::size_t el = static_cast< std::size_t >(esuf[2*f]);
// Extract the left element coordinates
std::array< std::array< tk::real, 3>, 4 > coordel_l {{
{{ cx[ inpoel[4*el ] ], cy[ inpoel[4*el ] ], cz[ inpoel[4*el ] ] }},
{{ cx[ inpoel[4*el+1] ], cy[ inpoel[4*el+1] ], cz[ inpoel[4*el+1] ] }},
{{ cx[ inpoel[4*el+2] ], cy[ inpoel[4*el+2] ], cz[ inpoel[4*el+2] ] }},
{{ cx[ inpoel[4*el+3] ], cy[ inpoel[4*el+3] ], cz[ inpoel[4*el+3] ] }} }};
// Compute the determinant of Jacobian matrix
auto detT_l =
Jacobian( coordel_l[0], coordel_l[1], coordel_l[2], coordel_l[3] );
// face normal
std::array< real, 3 >
fn{{ geoFace(f,1), geoFace(f,2), geoFace(f,3) }};
// face centroid
std::array< real, 3 >
gp{{ geoFace(f,4), geoFace(f,5), geoFace(f,6) }};
std::array< tk::real, 3> ref_gp_l{
Jacobian( coordel_l[0], gp, coordel_l[2], coordel_l[3] ) / detT_l,
Jacobian( coordel_l[0], coordel_l[1], gp, coordel_l[3] ) / detT_l,
Jacobian( coordel_l[0], coordel_l[1], coordel_l[2], gp ) / detT_l };
//Compute the basis functions for the left element
auto B_l = eval_basis( rdof, ref_gp_l[0], ref_gp_l[1], ref_gp_l[2] );
// Compute the state variables at the left element
auto ugp = evalFVSol(mat_blk, intsharp, ncomp, nprim,
rdof, nmat, el, inpoel, coord, geoElem, ref_gp_l, B_l, U, P,
srcFlag[el]);
Assert( ugp.size() == ncomp+nprim, "Incorrect size for "
"appended boundary state vector" );
auto var = state( ncomp, mat_blk, ugp, gp[0], gp[1], gp[2], t, fn );<--- Variable 'var' is assigned a value that is never used.
// cell averaged state for computing the diffusive flux
std::vector< tk::real > Bcc(rdof, 0.0);
Bcc[0] = 1.0;
auto ucc = evalFVSol(mat_blk, 0, ncomp, nprim, rdof,
nmat, el, inpoel, coord, geoElem, {{0.25, 0.25, 0.25}}, Bcc, U, P,
srcFlag[el]);
Assert( ucc.size() == ncomp+nprim, "Incorrect size for "
"appended cell-averaged state vector" );
// Cell centroids- [0]: left cell, [1]: ghost cell
// The ghost-cell is a 'reflection' of the boundary cell about the
// boundary-face. i.e. the vector pointing from the internal-cell
// centroid to the ghost-cell centroid is normal to the face (aligned
// with the face-normal), and has length 2*d. d is the distance between
// the internal-cell centroid and the boundary-face. Based on this
// information, the centroid of the ghost-cell can be computed using
// vector algebra.
std::array< std::array< tk::real, 3 >, 2 > centroids;
centroids[0] = {{geoElem(el,1), geoElem(el,2), geoElem(el,3)}};
tk::real d = std::abs( tk::dot(fn,centroids[0]) + tk::dot(fn,gp) ) /
std::sqrt(tk::dot(fn,fn));
for (std::size_t i=0; i<3; ++i)
centroids[1][i] = centroids[0][i] + 2.0*d*fn[i];
// Get BC for cell-averaged state
auto varcc = state( ncomp, mat_blk, ucc,
centroids[1][0], centroids[1][1], centroids[1][2], t, fn );
// Numerical viscous flux
// ---------------------------------------------------------------------
// 1. Get spatial gradient from Dubiner dofs
auto jacInv_l = tk::inverseJacobian( coordel_l[0], coordel_l[1],
coordel_l[2], coordel_l[3] );
auto dBdx_l = tk::eval_dBdx_p1( rdof, jacInv_l );
std::vector< real > dudx_l(9,0.0);
for (std::size_t i=0; i<3; ++i)
for (std::size_t j=0; j<3; ++j)
dudx_l[3*i+j] =
dBdx_l[j][1] * P(el, velocityDofIdx(nmat,i,rdof,1))
+ dBdx_l[j][2] * P(el, velocityDofIdx(nmat,i,rdof,2))
+ dBdx_l[j][3] * P(el, velocityDofIdx(nmat,i,rdof,3));
// 2. Average du_i/dx_j
auto grad = gradFn( 3, mat_blk, dudx_l, gp[0], gp[2], gp[2], t, fn );
std::array< std::array< tk::real, 3 >, 3 > dudx;
for (std::size_t i=0; i<3; ++i)
for (std::size_t j=0; j<3; ++j)
dudx[i][j] = 0.5 * (grad[0][3*i+j] + grad[1][3*i+j]);
// 3. Compute flux
auto fl = modifiedGradientViscousFlux(nmat, ncomp, fn, centroids, var,
varcc, dudx);
// Add the surface integration term to the rhs
for (ncomp_t c=0; c<ncomp; ++c)
{
R(el, c) += geoFace(f,0) * fl[c];
}
}
}
}
}
} // tk::
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