// This is a user-supplied routine that sets the the boundary conditions
//
void SetBndValues_Unst(const mesh& Mesh, dTensor3* q, dTensor3* aux)
{
int meqn = q->getsize(2);
int kmax = q->getsize(3);
int maux = aux->getsize(2);
int NumElems = Mesh.get_NumElems();
int NumPhysElems = Mesh.get_NumPhysElems();
int NumGhostElems = Mesh.get_NumGhostElems();
int NumNodes = Mesh.get_NumNodes();
int NumPhysNodes = Mesh.get_NumPhysNodes();
int NumEdges = Mesh.get_NumEdges();
// ----------------------------------------
// Loop over each ghost cell element and
// place the correct information into
// these elements
// ----------------------------------------
for (int i=1; i<=NumGhostElems; i++)
{
int j = Mesh.get_ghost_link(i);
for (int m=1; m<=meqn; m++)
for (int k=1; k<=kmax; k++)
{
q->set(i+NumPhysElems,m,k, 0.0 );
}
}
}
// This is a user-supplied routine that sets the the boundary conditions
//
// The default routine for the 4D Vlasov code is to apply zero boundary
// conditions in configuration space. This routine is identical to the one
// found in the unst branch of the 2D DoGPack code, and *should* be setting
// periodic boundary conditions.
//
void SetBndValues_Unst(const mesh& Mesh, dTensor3* q, dTensor3* aux)
{
// problem information (If this were to be pulled from DogParams, these
// numbers would NOT be correct! The reason is that each quadrature point
// was actually saved as a separate "equation")
const int meqn = q->getsize(2);
const int kmax = q->getsize(3);
const int maux = aux->getsize(2);
// Mesh information
const int NumElems = Mesh.get_NumElems();
const int NumPhysElems = Mesh.get_NumPhysElems();
const int NumGhostElems = Mesh.get_NumGhostElems();
const int NumNodes = Mesh.get_NumNodes();
const int NumPhysNodes = Mesh.get_NumPhysNodes();
const int NumEdges = Mesh.get_NumEdges();
// ----------------------------------------
// Loop over each ghost cell element and
// place the correct information into
// these elements
// ----------------------------------------
for (int i=1; i<=NumGhostElems; i++)
{
int j = Mesh.get_ghost_link(i);
for (int m=1; m<=meqn; m++)
for (int k=1; k<=kmax; k++)
{
q->set(i+NumPhysElems, m, k, q->get(j, m, k) );
}
}
}
//
// Output basic mesh information to screen
//
void ScreenOutput(const mesh& Mesh)
{
// Compute mesh quality parameters
double totalarea = Mesh.get_area_prim(1);
double maxarea = Mesh.get_area_prim(1);
double minarea = Mesh.get_area_prim(1);
for (int i=2; i<=Mesh.get_NumPhysElems(); i++)
{
double tmp = Mesh.get_area_prim(i);
totalarea = totalarea + tmp;
if (tmp < minarea)
{ minarea = tmp; }
if (tmp > maxarea)
{ maxarea = tmp; }
}
double minAngle = 180.0;
for (int i=1; i<=Mesh.get_NumPhysElems(); i++)
{
const int i1 = Mesh.get_tnode(i,1);
const int i2 = Mesh.get_tnode(i,2);
const int i3 = Mesh.get_tnode(i,3);
point v12, v23, v31;
v12.x = Mesh.get_node(i2,1) - Mesh.get_node(i1,1);
v12.y = Mesh.get_node(i2,2) - Mesh.get_node(i1,2);
v23.x = Mesh.get_node(i3,1) - Mesh.get_node(i2,1);
v23.y = Mesh.get_node(i3,2) - Mesh.get_node(i2,2);
v31.x = Mesh.get_node(i1,1) - Mesh.get_node(i3,1);
v31.y = Mesh.get_node(i1,2) - Mesh.get_node(i3,2);
double angle1 = acos((v12.x*-v31.x+v12.y*-v31.y)
/(sqrt(v12.x*v12.x+v12.y*v12.y)*sqrt(v31.x*v31.x+v31.y*v31.y)));
double angle2 = acos((v23.x*-v12.x+v23.y*-v12.y)
/(sqrt(v23.x*v23.x+v23.y*v23.y)*sqrt(v12.x*v12.x+v12.y*v12.y)));
double angle3 = acos((v31.x*-v23.x+v31.y*-v23.y)
/(sqrt(v31.x*v31.x+v31.y*v31.y)*sqrt(v23.x*v23.x+v23.y*v23.y)));
if ((angle1*180/pi) < minAngle)
{ minAngle = angle1*180/pi; }
if ((angle2*180/pi) < minAngle)
{ minAngle = angle2*180/pi; }
if ((angle3*180/pi) < minAngle)
{ minAngle = angle3*180/pi; }
}
// Output summary of results to screen
printf("\n");
printf(" SUMMARY OF RESULTS:\n");
printf(" -------------------\n");
printf(" Number of Elements: %8i\n",Mesh.get_NumElems());
printf(" Number of Physical Elements: %8i\n",Mesh.get_NumPhysElems());
printf(" Number of Ghost Elements: %8i\n",Mesh.get_NumGhostElems());
printf(" Number of Nodes: %8i\n",Mesh.get_NumNodes());
printf(" Number of Physical Nodes: %8i\n",Mesh.get_NumPhysNodes());
printf(" Number of Boundary Nodes: %8i\n",Mesh.get_NumBndNodes());
printf(" Number of Edges: %8i\n",Mesh.get_NumEdges());
printf(" Number of Boundary Edges: %8i\n",Mesh.get_NumBndEdges());
printf("\n");
printf(" Total Area Covered: %24.16e\n",totalarea);
printf(" Area Ratio: small/large: %24.16e\n",minarea/maxarea);
printf(" Angle Ratio: minAngle/60: %24.16e\n",minAngle/60.0);
printf("\n");
}
void ComputeError(const int space_order,
const mesh& Mesh,
const dTensor1& phi,
const dTensor2& E1,
const dTensor2& E2,
void (*PhiFunc)(const dTensor2& xpts,dTensor2& phi_ex),
void (*EfieldFunc)(const dTensor2& xpts,dTensor2& Efield_ex))
{
// Potential
const int NumPhysNodes = phi.getsize();//Mesh.get_NumPhysNodes();
dTensor2 xpts(NumPhysNodes,2);
dTensor2 phi_ex(NumPhysNodes,1);
double phi_err;
double phi_rel;
switch(space_order)
{
case 2:
for (int i=1; i<=NumPhysNodes; i++)
{
xpts.set(i,1, Mesh.get_node(i,1) );
xpts.set(i,2, Mesh.get_node(i,2) );
}
PhiFunc(xpts,phi_ex);
phi_err = 0.0;
phi_rel = 0.0;
for (int i=1; i<=NumPhysNodes; i++)
{
phi_rel = phi_rel + pow(phi_ex.get(i,1),2);
phi_err = phi_err + pow(phi_ex.get(i,1)-phi.get(i),2);
}
phi_err = sqrt(phi_err/phi_rel);
break;
case 3:
for (int i=1; i<=NumPhysNodes; i++)
{
xpts.set(i,1, Mesh.get_sub_node(i,1) );
xpts.set(i,2, Mesh.get_sub_node(i,2) );
}
PhiFunc(xpts,phi_ex);
phi_err = 0.0;
phi_rel = 0.0;
for (int i=1; i<=NumPhysNodes; i++)
{
phi_rel = phi_rel + pow(phi_ex.get(i,1),2);
phi_err = phi_err + pow(phi_ex.get(i,1)-phi.get(i),2);
}
phi_err = sqrt(phi_err/phi_rel);
break;
}
// Electric field components
void L2Project_Unst(const int istart,
const int iend,
const int QuadOrder,
const int BasisOrder_fout,
const mesh& Mesh,
dTensor3* fout,
void (*Func)(const dTensor2&,dTensor2&));
const int NumElems = Mesh.get_NumElems();
const int NumPhysElems = Mesh.get_NumPhysElems();
const int kmax = E1.getsize(2);
dTensor3 Efield_ex(NumElems,2,kmax);
L2Project_Unst(1,NumElems,space_order,space_order,
Mesh,&Efield_ex,EfieldFunc);
double E1_err = 0.0;
double E1_rel = 0.0;
double E2_err = 0.0;
double E2_rel = 0.0;
for (int i=1; i<=NumPhysElems; i++)
{
double Area = Mesh.get_area_prim(i);
double tmp1 = 0.0;
double tmp2 = 0.0;
double tmp1_rel = 0.0;
double tmp2_rel = 0.0;
for (int k=1; k<=kmax; k++)
{
tmp1 = tmp1 + pow((E1.get(i,k)-Efield_ex.get(i,1,k)),2);
tmp2 = tmp2 + pow((E2.get(i,k)-Efield_ex.get(i,2,k)),2);
tmp1_rel = tmp1_rel + pow((Efield_ex.get(i,1,k)),2);
tmp2_rel = tmp2_rel + pow((Efield_ex.get(i,2,k)),2);
}
E1_err = E1_err + Area*tmp1;
E2_err = E2_err + Area*tmp2;
E1_rel = E1_rel + Area*tmp1_rel;
E2_rel = E2_rel + Area*tmp2_rel;
}
E1_err = sqrt(E1_err/E1_rel);
E2_err = sqrt(E2_err/E2_rel);
// Summary
printf(" |----------------------------\n");
printf(" | Errors:\n");
printf(" |----------------------------\n");
printf(" | phi_err = %e\n",phi_err);
printf(" | E1_err = %e\n",E1_err);
printf(" | E2_err = %e\n",E2_err);
printf(" |----------------------------\n");
printf("\n");
}
// All-purpose routine for computing the L2-projection
// of various functions onto the gradient of the Legendre basis
// (Unstructured grid version)
//
void L2ProjectGrad_Unst(
const dTensor2* vel_vec,
const int istart,
const int iend,
const int QuadOrder,
const int BasisOrder_qin,
const int BasisOrder_auxin,
const int BasisOrder_fout,
const mesh& Mesh,
const dTensor3* qin,
const dTensor3* auxin,
dTensor3* fout,
void (*Func)(const dTensor2* vel_vec,
const dTensor2&,const dTensor2&,
const dTensor2&,dTensor3&))
{
// starting and ending indeces
const int NumElems = Mesh.get_NumElems();
assert_ge(istart,1);
assert_le(iend,NumElems);
// qin variable
assert_eq(NumElems,qin->getsize(1));
const int meqn = qin->getsize(2);
const int kmax_qin = qin->getsize(3);
assert_eq(kmax_qin,(BasisOrder_qin*(BasisOrder_qin+1))/2);
// auxin variable
assert_eq(NumElems,auxin->getsize(1));
const int maux = auxin->getsize(2);
const int kmax_auxin = auxin->getsize(3);
assert_eq(kmax_auxin,(BasisOrder_auxin*(BasisOrder_auxin+1))/2);
// fout variables
assert_eq(NumElems,fout->getsize(1));
const int mcomps_out = fout->getsize(2);
const int kmax_fout = fout->getsize(3);
assert_eq(kmax_fout,(BasisOrder_fout*(BasisOrder_fout+1))/2);
// number of quadrature points
assert_ge(QuadOrder,1);
assert_le(QuadOrder,5);
int mpoints;
switch ( QuadOrder )
{
case 1:
mpoints = 0;
break;
case 2:
mpoints = 1;
break;
case 3:
mpoints = 6;
break;
case 4:
mpoints = 7;
break;
case 5:
mpoints = 16;
break;
}
// trivial case
if ( QuadOrder==1 )
{
for (int i=istart; i<=iend; i++)
for (int m=1; m<=mcomps_out; m++)
for (int k=1; k<=kmax_fout; k++)
{ fout->set(i,m,k, 0.0 ); }
}
else
{
const int kmax = iMax(iMax(kmax_qin,kmax_auxin),kmax_fout);
dTensor2 spts(mpoints,2);
dTensor1 wgts(mpoints);
dTensor2 xpts(mpoints,2);
dTensor2 qvals(mpoints,meqn);
dTensor2 auxvals(mpoints,maux);
dTensor3 fvals(mpoints,mcomps_out,2);
dTensor2 mu(mpoints,kmax); // monomial basis (non-orthogonal)
dTensor2 phi(mpoints,kmax); // Legendre basis (orthogonal)
dTensor2 mu_xi(mpoints,kmax_fout); // xi-derivative of monomial basis (non-orthogonal)
dTensor2 mu_eta(mpoints,kmax_fout); // eta-derivative of monomial basis (non-orthogonal)
dTensor2 phi_xi(mpoints,kmax_fout); // xi-derivative of Legendre basis (orthogonal)
dTensor2 phi_eta(mpoints,kmax_fout); // eta-derivative of Legendre basis (orthogonal)
dTensor2 phi_x(mpoints,kmax_fout); // x-derivative of Legendre basis (orthogonal)
dTensor2 phi_y(mpoints,kmax_fout); // y-derivative of Legendre basis (orthogonal)
switch ( QuadOrder )
{
case 2:
spts.set(1,1, 0.0 );
spts.set(1,2, 0.0 );
wgts.set(1, 0.5 );
break;
case 3:
spts.set(1,1, 0.112615157582632 );
spts.set(1,2, 0.112615157582632 );
spts.set(2,1, -0.225230315165263 );
spts.set(2,2, 0.112615157582632 );
spts.set(3,1, 0.112615157582632 );
spts.set(3,2, -0.225230315165263 );
spts.set(4,1, -0.241757119823562 );
spts.set(4,2, -0.241757119823562 );
spts.set(5,1, 0.483514239647126 );
spts.set(5,2, -0.241757119823562 );
spts.set(6,1, -0.241757119823562 );
spts.set(6,2, 0.483514239647126 );
wgts.set(1, 0.1116907948390055 );
wgts.set(2, 0.1116907948390055 );
wgts.set(3, 0.1116907948390055 );
wgts.set(4, 0.0549758718276610 );
wgts.set(5, 0.0549758718276610 );
wgts.set(6, 0.0549758718276610 );
break;
case 4:
spts.set(1,1, 0.000000000000000 );
spts.set(1,2, 0.000000000000000 );
spts.set(2,1, 0.136808730771782 );
spts.set(2,2, 0.136808730771782 );
spts.set(3,1, -0.273617461543563 );
spts.set(3,2, 0.136808730771782 );
spts.set(4,1, 0.136808730771782 );
spts.set(4,2, -0.273617461543563 );
spts.set(5,1, -0.232046826009877 );
spts.set(5,2, -0.232046826009877 );
spts.set(6,1, 0.464093652019754 );
spts.set(6,2, -0.232046826009877 );
spts.set(7,1, -0.232046826009877 );
spts.set(7,2, 0.464093652019754 );
wgts.set(1, 0.1125000000000000 );
wgts.set(2, 0.0661970763942530 );
wgts.set(3, 0.0661970763942530 );
wgts.set(4, 0.0661970763942530 );
wgts.set(5, 0.0629695902724135 );
wgts.set(6, 0.0629695902724135 );
wgts.set(7, 0.0629695902724135 );
break;
case 5:
spts.set(1,1, 0.000000000000000 );
spts.set(1,2, 0.000000000000000 );
spts.set(2,1, 0.125959254959390 );
spts.set(2,2, 0.125959254959390 );
spts.set(3,1, -0.251918509918779 );
spts.set(3,2, 0.125959254959390 );
spts.set(4,1, 0.125959254959390 );
spts.set(4,2, -0.251918509918779 );
spts.set(5,1, -0.162764025581573 );
spts.set(5,2, -0.162764025581573 );
spts.set(6,1, 0.325528051163147 );
spts.set(6,2, -0.162764025581573 );
spts.set(7,1, -0.162764025581573 );
spts.set(7,2, 0.325528051163147 );
spts.set(8,1, -0.282786105016302 );
spts.set(8,2, -0.282786105016302 );
spts.set(9,1, 0.565572210032605 );
spts.set(9,2, -0.282786105016302 );
spts.set(10,1, -0.282786105016302 );
spts.set(10,2, 0.565572210032605 );
spts.set(11,1, -0.324938555923375 );
spts.set(11,2, -0.070220503698695 );
spts.set(12,1, -0.324938555923375 );
spts.set(12,2, 0.395159059622071 );
spts.set(13,1, -0.070220503698695 );
spts.set(13,2, -0.324938555923375 );
spts.set(14,1, -0.070220503698695 );
spts.set(14,2, 0.395159059622071 );
spts.set(15,1, 0.395159059622071 );
spts.set(15,2, -0.324938555923375 );
spts.set(16,1, 0.395159059622071 );
spts.set(16,2, -0.070220503698695 );
wgts.set(1, 0.0721578038388935 );
wgts.set(2, 0.0475458171336425 );
wgts.set(3, 0.0475458171336425 );
wgts.set(4, 0.0475458171336425 );
wgts.set(5, 0.0516086852673590 );
wgts.set(6, 0.0516086852673590 );
wgts.set(7, 0.0516086852673590 );
wgts.set(8, 0.0162292488115990 );
wgts.set(9, 0.0162292488115990 );
wgts.set(10, 0.0162292488115990 );
wgts.set(11, 0.0136151570872175 );
wgts.set(12, 0.0136151570872175 );
wgts.set(13, 0.0136151570872175 );
wgts.set(14, 0.0136151570872175 );
wgts.set(15, 0.0136151570872175 );
wgts.set(16, 0.0136151570872175 );
break;
}
// Loop over each quadrature point and construct monomial polys
for (int m=1; m<=mpoints; m++)
{
// coordinates
const double xi = spts.get(m,1);
const double xi2 = xi*xi;
const double xi3 = xi2*xi;
const double xi4 = xi3*xi;
const double eta = spts.get(m,2);
const double eta2 = eta*eta;
const double eta3 = eta2*eta;
const double eta4 = eta3*eta;
// monomial basis functions at each gaussian quadrature point
switch( kmax )
{
case 15: // fifth order
mu.set(m, 15, eta4 );
mu.set(m, 14, xi4 );
mu.set(m, 13, xi2*eta2 );
mu.set(m, 12, eta3*xi );
mu.set(m, 11, xi3*eta );
case 10: // fourth order
mu.set(m, 10, eta3 );
mu.set(m, 9, xi3 );
mu.set(m, 8, xi*eta2 );
mu.set(m, 7, eta*xi2 );
case 6: // third order
mu.set(m, 6, eta2 );
mu.set(m, 5, xi2 );
mu.set(m, 4, xi*eta );
case 3: // second order
mu.set(m, 3, eta );
mu.set(m, 2, xi );
case 1: // first order
mu.set(m, 1, 1.0 );
break;
}
// Loop over each quadrature point and construct Legendre polys
for (int i=1; i<=kmax; i++)
{
double tmp = 0.0;
for (int j=1; j<=i; j++)
{ tmp = tmp + Mmat[i-1][j-1]*mu.get(m,j); }
phi.set(m,i, tmp );
}
// Gradient of monomial basis functions at each gaussian quadrature point
switch( kmax_fout )
{
case 15: // fifth order
mu_xi.set( m,15, 0.0 );
mu_xi.set( m,14, 4.0*xi3 );
mu_xi.set( m,13, 2.0*xi*eta2 );
mu_xi.set( m,12, eta3 );
mu_xi.set( m,11, 3.0*xi2*eta );
mu_eta.set( m,15, 4.0*eta3 );
mu_eta.set( m,14, 0.0 );
mu_eta.set( m,13, 2.0*xi2*eta );
mu_eta.set( m,12, 3.0*eta2*xi );
mu_eta.set( m,11, xi3 );
case 10: // fourth order
mu_xi.set( m,10, 0.0 );
mu_xi.set( m,9, 3.0*xi2 );
mu_xi.set( m,8, eta2 );
mu_xi.set( m,7, 2.0*eta*xi );
mu_eta.set( m,10, 3.0*eta2 );
mu_eta.set( m,9, 0.0 );
mu_eta.set( m,8, 2.0*eta*xi );
mu_eta.set( m,7, xi2 );
case 6: // third order
mu_xi.set( m,6, 0.0 );
mu_xi.set( m,5, 2.0*xi );
mu_xi.set( m,4, eta );
mu_eta.set( m,6, 2.0*eta );
mu_eta.set( m,5, 0.0 );
mu_eta.set( m,4, xi );
case 3: // second order
mu_xi.set( m,3, 0.0 );
mu_xi.set( m,2, 1.0 );
mu_eta.set( m,3, 1.0 );
mu_eta.set( m,2, 0.0 );
case 1: // first order
mu_xi.set( m,1, 0.0 );
mu_eta.set( m,1, 0.0 );
break;
}
// Loop over each quadrature point and construct Legendre polys
for (int i=1; i<=kmax_fout; i++)
{
double tmp1 = 0.0;
double tmp2 = 0.0;
for (int j=1; j<=i; j++)
{
tmp1 = tmp1 + Mmat[i-1][j-1]*mu_xi.get(m,j);
tmp2 = tmp2 + Mmat[i-1][j-1]*mu_eta.get(m,j);
}
phi_xi.set(m,i, tmp1 );
phi_eta.set(m,i, tmp2 );
}
}
// -------------------------------------------------------------
// Loop over every grid cell indexed by user supplied parameters
// described by istart...iend
// -------------------------------------------------------------
#pragma omp parallel for
for (int i=istart; i<=iend; i++)
{
// Find center of current cell
const int i1 = Mesh.get_tnode(i,1);
const int i2 = Mesh.get_tnode(i,2);
const int i3 = Mesh.get_tnode(i,3);
const double x1 = Mesh.get_node(i1,1);
const double y1 = Mesh.get_node(i1,2);
const double x2 = Mesh.get_node(i2,1);
const double y2 = Mesh.get_node(i2,2);
const double x3 = Mesh.get_node(i3,1);
const double y3 = Mesh.get_node(i3,2);
const double xc = (x1+x2+x3)/3.0;
const double yc = (y1+y2+y3)/3.0;
// Compute q, aux and fvals at each Gaussian Quadrature point
// for this current cell indexed by (i,j)
// Save results into dTensor2 qvals, auxvals and fvals.
for (int m=1; m<=mpoints; m++)
{
// convert phi_xi and phi_eta derivatives
// to phi_x and phi_y derivatives through Jacobian
for (int k=1; k<=kmax_fout; k++)
{
phi_x.set(m,k, Mesh.get_jmat(i,1,1)*phi_xi.get(m,k)
+ Mesh.get_jmat(i,1,2)*phi_eta.get(m,k) );
phi_y.set(m,k, Mesh.get_jmat(i,2,1)*phi_xi.get(m,k)
+ Mesh.get_jmat(i,2,2)*phi_eta.get(m,k) );
}
// point on the unit triangle
const double s = spts.get(m,1);
const double t = spts.get(m,2);
// point on the physical triangle
xpts.set(m,1, xc + (x2-x1)*s + (x3-x1)*t );
xpts.set(m,2, yc + (y2-y1)*s + (y3-y1)*t );
// Solution values (q) at each grid point
for (int me=1; me<=meqn; me++)
{
qvals.set(m,me, 0.0 );
for (int k=1; k<=kmax_qin; k++)
{
qvals.set(m,me, qvals.get(m,me)
+ phi.get(m,k) * qin->get(i,me,k) );
}
}
// Auxiliary values (aux) at each grid point
for (int ma=1; ma<=maux; ma++)
{
auxvals.set(m,ma, 0.0 );
for (int k=1; k<=kmax_auxin; k++)
{
auxvals.set(m,ma, auxvals.get(m,ma)
+ phi.get(m,k) * auxin->get(i,ma,k) );
}
}
}
// Call user-supplied function to set fvals
Func(vel_vec, xpts, qvals, auxvals, fvals);
// Evaluate integral on current cell (project onto Legendre basis)
// using Gaussian Quadrature for the integration
for (int m1=1; m1<=mcomps_out; m1++)
for (int m2=1; m2<=kmax_fout; m2++)
{
double tmp = 0.0;
for (int k=1; k<=mpoints; k++)
{
tmp = tmp + wgts.get(k)*
( fvals.get(k,m1,1)*phi_x.get(k,m2) +
fvals.get(k,m1,2)*phi_y.get(k,m2) );
}
fout->set(i, m1, m2, 2.0*tmp );
}
}
}
}
// Right-hand side for hyperbolic PDE in divergence form
//
// q_t = -( f(q,x,y,t)_x + g(q,x,y,t)_y ) + Psi(q,x,y,t)
//
void LaxWendroff_Unst(double dt,
const mesh& Mesh, const edge_data_Unst& EdgeData,
dTensor3& aux, // SetBndValues modifies ghost cells
dTensor3& q, // SetBndValues modifies ghost cells
dTensor3& Lstar, dTensor1& smax)
{
const int NumElems = Mesh.get_NumElems();
const int NumPhysElems = Mesh.get_NumPhysElems();
const int NumEdges = Mesh.get_NumEdges();
const int meqn = q.getsize(2);
const int kmax = q.getsize(3);
const int maux = aux.getsize(2);
const int space_order = dogParams.get_space_order();
dTensor3 EdgeFluxIntegral(NumElems,meqn,kmax);
dTensor3 ElemFluxIntegral(NumElems,meqn,kmax);
dTensor3 Psi(NumElems,meqn,kmax);
// ---------------------------------------------------------
// Boundary Conditions
SetBndValues_Unst(Mesh, &q, &aux);
// ---------------------------------------------------------
// --------------------------------------------------------------------- //
// Part 0: Compute the Lax-Wendroff "flux" function:
//
// Here, we include the extra information about time derivatives.
// --------------------------------------------------------------------- //
dTensor3 F(NumElems, meqn, kmax ); F.setall(0.);
dTensor3 G(NumElems, meqn, kmax ); G.setall(0.);
L2ProjectLxW_Unst( dogParams.get_time_order(), 1.0, 0.5*dt, dt*dt/6.0, 1, NumElems,
space_order, space_order, space_order, space_order, Mesh,
&q, &aux, &F, &G, &FluxFunc, &DFluxFunc, &D2FluxFunc );
// ---------------------------------------------------------
// Part I: compute source term
// ---------------------------------------------------------
if ( dogParams.get_source_term()>0 )
{
// eprintf("error: have not implemented source term for LxW solver.");
printf("Source term has not been implemented for LxW solver. Terminating program.");
exit(1);
}
Lstar.setall(0.);
// ---------------------------------------------------------
// ---------------------------------------------------------
// Part II: compute flux integral on element edges
// ---------------------------------------------------------
// Loop over all interior edges
EdgeFluxIntegral.setall(0.);
ElemFluxIntegral.setall(0.);
#pragma omp parallel for
// Loop over all interior edges
for (int i=1; i<=NumEdges; i++)
{
// Edge coordinates
double x1 = Mesh.get_edge(i,1);
double y1 = Mesh.get_edge(i,2);
double x2 = Mesh.get_edge(i,3);
double y2 = Mesh.get_edge(i,4);
// Elements on either side of edge
int ileft = Mesh.get_eelem(i,1);
int iright = Mesh.get_eelem(i,2);
double Areal = Mesh.get_area_prim(ileft);
double Arear = Mesh.get_area_prim(iright);
// Scaled normal to edge
dTensor1 nhat(2);
nhat.set(1, (y2-y1) );
nhat.set(2, (x1-x2) );
// Variables to store flux integrals along edge
dTensor2 Fr_tmp(meqn,dogParams.get_space_order());
dTensor2 Fl_tmp(meqn,dogParams.get_space_order());
// Loop over number of quadrature points along each edge
for (int ell=1; ell<=dogParams.get_space_order(); ell++)
{
dTensor1 Ql(meqn), Qr(meqn);
dTensor1 ffl(meqn), ffr(meqn); // << -- NEW PART -- >>
dTensor1 Auxl(maux), Auxr(maux);
// Riemann data - q
for (int m=1; m<=meqn; m++)
{
Ql.set(m, 0.0 );
Qr.set(m, 0.0 );
// << -- NEW PART, ffl and ffr -- >> //
ffl.set(m, 0.0 );
ffr.set(m, 0.0 );
for (int k=1; k<=kmax; k++)
{
Ql.set(m, Ql.get(m) + EdgeData.phi_left->get(i,ell,k)
*q.get(ileft, m,k) );
Qr.set(m, Qr.get(m) + EdgeData.phi_right->get(i,ell,k)
*q.get(iright,m,k) );
// << -- NEW PART, ffl and ffr -- >> //
// Is this the correct way to use the normal vector?
ffl.set(m, ffl.get(m) + EdgeData.phi_left->get (i, ell, k) * (
nhat.get(1)*F.get( ileft, m, k) + nhat.get(2)*G.get( ileft, m, k) ) );
ffr.set(m, ffr.get(m) + EdgeData.phi_right->get(i, ell, k) * (
nhat.get(1)*F.get(iright, m, k) + nhat.get(2)*G.get(iright, m, k) ) );
}
}
// Riemann data - aux
for (int m=1; m<=maux; m++)
{
Auxl.set(m, 0.0 );
Auxr.set(m, 0.0 );
for (int k=1; k<=kmax; k++)
{
Auxl.set(m, Auxl.get(m) + EdgeData.phi_left->get(i,ell,k) * aux.get(ileft, m,k) );
Auxr.set(m, Auxr.get(m) + EdgeData.phi_right->get(i,ell,k) * aux.get(iright,m,k) );
}
}
// Solve Riemann problem
dTensor1 xedge(2);
double s = EdgeData.xpts1d->get(ell);
xedge.set(1, x1 + 0.5*(s+1.0)*(x2-x1) );
xedge.set(2, y1 + 0.5*(s+1.0)*(y2-y1) );
// Solve the Riemann problem for this edge
dTensor1 Fl(meqn), Fr(meqn);
// Use the time-averaged fluxes to define left and right values for
// the Riemann solver.
const double smax_edge = RiemannSolveLxW(
nhat, xedge, Ql, Qr, Auxl, Auxr, ffl, ffr, Fl, Fr);
smax.set(i, Max(smax_edge,smax.get(i)) );
// Construct fluxes
for (int m=1; m<=meqn; m++)
{
Fr_tmp.set(m,ell, Fr.get(m) );
Fl_tmp.set(m,ell, Fl.get(m) );
}
}
// Add edge integral to line integral around the full element
for (int m=1; m<=meqn; m++)
for (int k=1; k<=kmax; k++)
{
double Fl_sum = 0.0;
double Fr_sum = 0.0;
for (int ell=1; ell<=dogParams.get_space_order(); ell++)
{
Fl_sum = Fl_sum + 0.5*EdgeData.wgts1d->get(ell)
*EdgeData.phi_left->get(i,ell,k) *Fl_tmp.get(m,ell);
Fr_sum = Fr_sum + 0.5*EdgeData.wgts1d->get(ell)
*EdgeData.phi_right->get(i,ell,k)*Fr_tmp.get(m,ell);
}
EdgeFluxIntegral.set(ileft, m,k, EdgeFluxIntegral.get(ileft, m,k) + Fl_sum/Areal );
EdgeFluxIntegral.set(iright,m,k, EdgeFluxIntegral.get(iright,m,k) - Fr_sum/Arear );
}
}
// ---------------------------------------------------------
// ---------------------------------------------------------
// Part III: compute intra-element contributions
// ---------------------------------------------------------
if( dogParams.get_space_order() > 1 )
{
L2ProjectGradAddLegendre_Unst(1, NumPhysElems, space_order,
Mesh, &F, &G, &ElemFluxIntegral );
}
// ---------------------------------------------------------
// ---------------------------------------------------------
// Part IV: construct Lstar
// ---------------------------------------------------------
if (dogParams.get_source_term()==0) // Without Source Term
{
#pragma omp parallel for
for (int i=1; i<=NumPhysElems; i++)
for (int m=1; m<=meqn; m++)
for (int k=1; k<=kmax; k++)
{
double tmp = ElemFluxIntegral.get(i,m,k) - EdgeFluxIntegral.get(i,m,k);
Lstar.set(i,m,k, tmp );
}
}
else // With Source Term
{
#pragma omp parallel for
for (int i=1; i<=NumPhysElems; i++)
for (int m=1; m<=meqn; m++)
for (int k=1; k<=kmax; k++)
{
// double tmp = ElemFluxIntegral.get(i,m,k)
// - EdgeFluxIntegral.get(i,m,k)
// + Psi.get(i,m,k);
// Lstar.set(i,m,k, tmp );
printf("Source term has not been implemented for LxW solver. Terminating program.");
exit(1);
}
}
// ---------------------------------------------------------
// ---------------------------------------------------------
// Part V: add extra contributions to Lstar
// ---------------------------------------------------------
// Call LstarExtra
LstarExtra_Unst(Mesh, &q, &aux, &Lstar);
// ---------------------------------------------------------
// ---------------------------------------------------------
// Part VI: artificial viscosity limiter
// ---------------------------------------------------------
// if (dogParams.get_space_order()>1 &&
// dogParams.using_viscosity_limiter())
// { ArtificialViscosity(&aux,&q,&Lstar); }
// ---------------------------------------------------------
}
// This file should be identical to DogSolveRK_Unst, with the exception that all
// output printing statements are silenced.
//
// Advance the solution qold to qnew over time interval tstart to tend.
//
// All local information is allocated within this function. The only part
// that gets shared are time values passed through dogStateUnst2. This class
// should be modified to accept the state variable, q and aux in place of only
// containing time information as is currently the case. (-DS)
double DogSolveRK_Unst_Quiet(
const dTensor2* vel_vec,
const mesh& Mesh, const edge_data_Unst& EdgeData,
dTensor3& aux, dTensor3& qold, dTensor3& qnew,
const double tstart, const double tend, DogStateUnst2& dogStateUnst2)
{
const int mx = qnew.getsize(1);
const int meqn = qnew.getsize(2);
const int kmax = qnew.getsize(3);
const int maux = aux.getsize(2);
const double* cflv = dogParams.get_cflv();
const int nv = dogParams.get_nv();
RKinfo rk;
SetRKinfo(dogParams.get_time_order(),rk);
// define local variables
int n_step = 0;
double t = tstart;
double dt = dogStateUnst2.get_initial_dt();
const double CFL_max = cflv[1];
const double CFL_target = cflv[2];
double cfl = 0.0;
double dtmin = dt;
double dtmax = dt;
const int NumElems = Mesh.get_NumElems(); // Number of total elements in mesh
const int NumNodes = Mesh.get_NumNodes(); // Number of nodes in mesh
const int NumEdges = Mesh.get_NumEdges(); // Number of edges in mesh
dTensor3 qstar(NumElems,meqn,kmax);
dTensor3 q1(NumElems,meqn,kmax);
dTensor3 q2(NumElems,meqn,kmax);
dTensor3 auxstar(NumElems,maux,kmax);
dTensor3 Lstar(NumElems,meqn,kmax);
dTensor3 Lold(NumElems,meqn,kmax);
dTensor3 auxold(NumElems,maux,kmax);
dTensor1 smax(NumEdges);
void L2Project_Unst(
const dTensor2* vel_vec,
const int istart, const int iend,
const int QuadOrder, const int BasisOrder_qin, const int BasisOrder_auxin, const
int BasisOrder_fout, const mesh& Mesh, const dTensor3* qin, const dTensor3*
auxin, dTensor3* fout, void (*Func)(const dTensor2* vel_vec, const
dTensor2&,const dTensor2&, const dTensor2&,dTensor2&));
// JUNK here:
void AuxFuncWrapper(
const dTensor2* vel_vec,
const dTensor2& xpts,
const dTensor2& NOT_USED_1,
const dTensor2& NOT_USED_2,
dTensor2& auxvals);
const int space_order = dogParams.get_space_order();
if( maux > 0 )
{
printf("WARNING: maux = %d should be zero for Vlasov routines.", maux);
printf(" Modify parameters.ini to remove this warning\n" );
L2Project_Unst(vel_vec,1,NumElems,
space_order,space_order,space_order,space_order,
Mesh,&qnew,&aux,&aux,&AuxFuncWrapper);
}
// Set initialize qstar and auxstar values
qstar.copyfrom(qold);
auxstar.copyfrom(aux);
// Runge-Kutta time stepping
while (t<tend)
{
// initialize time step
int m_accept = 0;
n_step = n_step + 1;
// check if max number of time steps exceeded
if( n_step > nv )
{
eprintf(" Error in DogSolveRK_Unst.cpp: "
" Exceeded allowed # of time steps \n"
" n_step = %d\n"
" nv = %d\n\n",
n_step, nv);
}
// copy qnew into qold
qold.copyfrom(qnew);
auxold.copyfrom(aux);
// keep trying until we get a dt that does not violate CFL condition
while (m_accept==0)
{
// set current time
double told = t;
if (told+dt > tend)
{ dt = tend - told; }
t = told + dt;
// TODO - this needs to be performed at the 'local' level
dogStateUnst2.set_time ( told );
dogStateUnst2.set_dt ( dt );
// Set initial maximum wave speed to zero
smax.setall(0.);
// Take a full time step of size dt
switch ( dogParams.get_time_order() )
{
case 1: // First order in time (1-stage)
// -----------------------------------------------
// Stage #1 (the only one in this case)
rk.mstage = 1;
BeforeStep_Unst(dt,Mesh,aux,qnew);
ConstructL_Unst(told, vel_vec,Mesh,EdgeData,aux,qnew,Lstar,smax);
UpdateSoln_Unst(rk.alpha1->get(rk.mstage),rk.alpha2->get(rk.mstage),
rk.beta->get(rk.mstage),dt,Mesh,aux, qnew, Lstar, qnew);
AfterStep_Unst(dt,Mesh,aux,qnew);
// -----------------------------------------------
break;
case 2: // Second order in time (2-stages)
// -----------------------------------------------
// Stage #1
rk.mstage = 1;
dogStateUnst2.set_time(told);
BeforeStep_Unst(dt,Mesh,aux,qnew);
ConstructL_Unst(told,vel_vec,Mesh,EdgeData,aux,qnew,Lstar,smax);
UpdateSoln_Unst(
rk.alpha1->get(rk.mstage),rk.alpha2->get(rk.mstage),
rk.beta->get(rk.mstage), dt, Mesh, aux, qnew, Lstar, qstar);
AfterStep_Unst(dt, Mesh, auxstar, qstar);
// ------------------------------------------------
// Stage #2
rk.mstage = 2;
dogStateUnst2.set_time(told+dt);
BeforeStep_Unst(dt, Mesh, auxstar, qstar);
ConstructL_Unst(told+1.0*dt, vel_vec, Mesh, EdgeData, aux, qstar, Lstar, smax);
UpdateSoln_Unst(rk.alpha1->get(rk.mstage), rk.alpha2->get(rk.mstage),
rk.beta->get(rk.mstage), dt, Mesh, auxstar, qstar, Lstar, qnew);
AfterStep_Unst(dt, Mesh, aux, qnew);
// ------------------------------------------------
break;
case 3: // Third order in time (3-stages)
// qnew = alpha1 * qstar + alpha2 * qnew + beta * dt * L( qstar )
// alpha1 = 1.0
// alpha2 = 0.0
// beta = 1.0
// ------------------------------------------------
// Stage #1
rk.mstage = 1;
dogStateUnst2.set_time(told);
BeforeStep_Unst(dt,Mesh,aux,qnew);
ConstructL_Unst(told, vel_vec,Mesh,EdgeData,aux,qnew,Lstar,smax);
Lold.copyfrom(Lstar);
UpdateSoln_Unst(rk.alpha1->get(rk.mstage),rk.alpha2->get(rk.mstage),
rk.beta->get(rk.mstage),dt,Mesh,aux,qnew,Lstar,qstar);
AfterStep_Unst(dt,Mesh,aux,qstar);
// -------------------------------------------------
// alpha1 = 0.75
// alpha2 = 0.25
// beta = 0.25
// Stage #2
rk.mstage = 2;
dogStateUnst2.set_time(told+0.5*dt);
BeforeStep_Unst(dt,Mesh,aux,qstar);
ConstructL_Unst(told+dt, vel_vec,Mesh,EdgeData,aux,qstar,Lstar,smax);
UpdateSoln_Unst(rk.alpha1->get(rk.mstage),rk.alpha2->get(rk.mstage),
rk.beta->get(rk.mstage),dt,Mesh,aux,qnew,Lstar,qstar);
AfterStep_Unst(dt,Mesh,aux,qstar);
// --------------------------------------------------
// alpha1 = 2/3
// alpha2 = 1/3
// beta = 2/3
// Stage #3
rk.mstage = 3;
dogStateUnst2.set_time(told+dt);
BeforeStep_Unst(dt,Mesh,auxstar,qstar);
ConstructL_Unst(told+0.5*dt,vel_vec,Mesh,EdgeData,auxstar,qstar,Lstar,smax);
UpdateSoln_Unst(rk.alpha1->get(rk.mstage),rk.alpha2->get(rk.mstage),
rk.beta->get(rk.mstage),dt,Mesh,aux,qstar,Lstar,qnew);
AfterStep_Unst(dt,Mesh,aux,qnew);
// --------------------------------------------------
break;
default: unsupported_value_error(dogParams.get_time_order());
}
// compute cfl number
cfl = GetCFL_Unst(dt,Mesh,aux,smax);
// output time step information
// if (dogParams.get_verbosity()>0)
// {
// printf(" In DogSolveRK_Quiet: DogSolve2D ... Step %5d"
// " CFL =%6.3f"
// " dt =%11.3e"
// " t =%11.3e\n",
// n_step, cfl, dt, t);
// }
// choose new time step
if (cfl>0.0)
{
dt = Min(dogParams.get_max_dt(), dt*CFL_target/cfl);
dtmin = Min(dt,dtmin);
dtmax = Max(dt,dtmax);
}
else
{
dt = dogParams.get_max_dt();
}
// see whether to accept or reject this step
if (cfl<=CFL_max)
// accept
{
m_accept = 1;
dogStateUnst2.set_time(t);
// do any extra work
// AfterFullTimeStep_Unst(dogStateUnst2.get_dt(),Mesh,
// auxold,qold,Lold,aux,qnew);
}
else
//reject
{
t = told;
dogStateUnst2.set_time(told);
// if( dogParams.get_verbosity() > 0 )
// {
// printf("DogSolve2D rejecting step..."
// "CFL number too large\n");
// }
// copy qold into qnew
qnew.copyfrom(qold);
aux.copyfrom(auxold);
// after reject function
// AfterReject_Unst(Mesh,dt,aux,qnew);
}
}
}
// printf(" Finished! t = %2.3e and nsteps = %d\n", t, n_step );
// set initial time step for next call to DogSolveRK
dogStateUnst2.set_initial_dt(dt);
void DeleteRKInfo(RKinfo& rk);
DeleteRKInfo(rk);
return cfl;
}
// This routine simply glues together many of the routines that are already
// written in the Poisson solver library
//
// phi( 1:SubNumPhysNodes ) is a scalar quantity.
//
// E1 ( 1:NumElems, 1:kmax2d ) is a vector quantity.
// E2 ( 1:NumElems, 1:kmax2d ) is a vector quantity.
//
// See also: ConvertEfieldOntoDGbasis
void ComputeElectricField( const double t, const mesh& Mesh, const dTensorBC5& q,
dTensor2& E1, dTensor2& E2)
{
//
const int mx = q.getsize(1); assert_eq(mx,dogParamsCart2.get_mx());
const int my = q.getsize(2); assert_eq(my,dogParamsCart2.get_my());
const int NumElems = q.getsize(3);
const int meqn = q.getsize(4);
const int kmax = q.getsize(5);
const int space_order = dogParams.get_space_order();
// unstructured parameters:
const int kmax2d = E2.getsize(2);
const int NumBndNodes = Mesh.get_NumBndNodes();
const int NumPhysNodes = Mesh.get_NumPhysNodes();
// Quick error check
if( !Mesh.get_is_submesh() )
{
printf("ERROR: mesh needs to have subfactor set to %d\n", space_order);
printf("Go to Unstructured mesh and remesh the problem\n");
exit(-1);
}
const int SubFactor = Mesh.get_SubFactor();
assert_eq( NumElems, Mesh.get_NumElems() );
// -- Step 1: Compute rho -- //
dTensor3 rho(NumElems, 1, kmax2d );
void ComputeDensity( const mesh& Mesh, const dTensorBC5& q, dTensor3& rho );
ComputeDensity( Mesh, q, rho );
// -- Step 2: Figure out how large phi needs to be
int SubNumPhysNodes = 0;
int SubNumBndNodes = 0;
switch( dogParams.get_space_order() )
{
case 1:
SubNumPhysNodes = NumPhysNodes;
SubNumBndNodes = NumBndNodes;
break;
case 2:
SubNumPhysNodes = Mesh.get_SubNumPhysNodes();
SubNumBndNodes = Mesh.get_SubNumBndNodes();
if(SubFactor!=2)
{
printf("\n");
printf(" Error: for space_order = %i, need SubFactor = %i\n",space_order,2);
printf(" SubFactor = %i\n",SubFactor);
printf("\n");
exit(1);
}
break;
case 3:
SubNumPhysNodes = Mesh.get_SubNumPhysNodes();
SubNumBndNodes = Mesh.get_SubNumBndNodes();
if(SubFactor!=3)
{
printf("\n");
printf(" Error: for space_order = %i, need SubFactor = %i\n",space_order,3);
printf(" SubFactor = %i\n",SubFactor);
printf("\n");
exit(1);
}
break;
default:
printf("\n");
printf(" ERROR in RunDogpack_unst.cpp: space_order value not supported.\n");
printf(" space_order = %i\n",space_order);
printf("\n");
exit(1);
}
// local storage:
dTensor1 rhs(SubNumPhysNodes);
dTensor1 phi(SubNumPhysNodes);
// Get Cholesky factorization matrix R
//
// TODO - this should be saved earlier in the code rather than reading
// from file every time we with to run a Poisson solve!
//
SparseCholesky R(SubNumPhysNodes);
string outputdir = dogParams.get_outputdir();
R.init(outputdir);
R.read(outputdir);
// Create right-hand side vector
void Rhs2D_unst(const int space_order,
const mesh& Mesh, const dTensor3& rhs_dg,
dTensor1& rhs);
Rhs2D_unst(space_order, Mesh, rho, rhs);
// Call Poisson solver
void PoissonSolver2D_unst(const int space_order,
const mesh& Mesh,
const SparseCholesky& R,
const dTensor1& rhs,
dTensor1& phi,
dTensor2& E1,
dTensor2& E2);
PoissonSolver2D_unst(space_order, Mesh, R, rhs, phi, E1, E2);
// Compare errors with the exact Electric field:
//
void L2Project_Unst(
const double time,
const dTensor2* vel_vec,
const int istart,
const int iend,
const int QuadOrder,
const int BasisOrder_qin,
const int BasisOrder_auxin,
const int BasisOrder_fout,
const mesh& Mesh,
const dTensor3* qin,
const dTensor3* auxin,
dTensor3* fout,
void (*Func)(const double t, const dTensor2* vel_vec, const dTensor2&,const dTensor2&,
const dTensor2&,dTensor2&));
const int sorder = dogParams.get_space_order();
dTensor3 qtmp (NumElems, 2, kmax2d ); qtmp.setall(0.);
dTensor3 auxtmp (NumElems, 0, kmax2d );
dTensor3 ExactE (NumElems, 2, kmax2d );
L2Project_Unst( t, NULL, 1, NumElems,
sorder, sorder, sorder, sorder, Mesh,
&qtmp, &auxtmp, &ExactE,
&ExactElectricField );
// Compute errors on these two:
//
double err = 0.;
for( int n=1; n <= NumElems; n++ )
for( int k=1; k <= kmax2d; k++ )
{
err += Mesh.get_area_prim(n)*pow( ExactE.get(n,1,k) - E1.get(n,k), 2 );
err += Mesh.get_area_prim(n)*pow( ExactE.get(n,2,k) - E2.get(n,k), 2 );
}
printf("error = %2.15e\n", err );
}
// This is the positivity preserving limiter proposed in
// "Maximum-Principle-Satisfying and Positivity-Preserving
// High Order Discontinuous Galerkin Schemes
// for Conservation Laws on Triangular Meshes", Zhang, Xia and Shu
// J. Sci. Comput. (2012).
//
// THIS METHOD ASSUMES THAT EVERY COMPONENT OF CONSERVED VARIABLES SHOULD STAY
// POSITIVE.
//
// In order to implement this for a different scheme, one should rewrite, or
// redefine what components should remain positiive. This will require
// reworking the control flow logic for how time step lengths are chosen.
void ApplyPosLimiter_Unst(const mesh& Mesh, const dTensor3& aux, dTensor3& q)
{
const int NumElems = Mesh.get_NumElems();
const int NumPhysElems = Mesh.get_NumPhysElems();
const int NumEdges = Mesh.get_NumEdges();
const int meqn = q.getsize(2);
const int kmax = q.getsize(3);
const int maux = aux.getsize(2);
const int space_order = dogParams.get_space_order();
// Do nothing in the case of piecewise constants
if( space_order == 1 )
{ return; }
// ------------------------------------------------ //
// number of points where we want to check solution //
// ------------------------------------------------ //
const int space_order_sq = space_order*space_order;
const int mpts_vec[] = {0, 3*space_order_sq, 18, 3*space_order_sq, 3*space_order_sq }; // TODO - FILL IN 2ND-ORDER CASE
const int mpoints = mpts_vec[space_order-1];
// ---------------------------------------------------------- //
// sample basis at all points where we want to check solution //
// ---------------------------------------------------------- //
dTensor2 spts(mpoints, 2);
void SetPositivePoints_Unst(const int& space_order, dTensor2& spts);
SetPositivePoints_Unst(space_order, spts);
void SamplePhiAtPositivePoints_Unst(const int& space_order,
const dTensor2& spts, dTensor2& phi);
dTensor2 phi(mpoints, kmax);
SamplePhiAtPositivePoints_Unst(space_order, spts, phi);
// -------------------------------------------------------------- //
// q_limited = Q1 + \theta ( q(xi,eta) - Q1 ) //
// where theta = min(1, |Q1| / |Q1-m|; m = min_{i} q(xi_i, eta_i) //
// -------------------------------------------------------------- //
#pragma omp parallel for
for(int i=1; i <= NumPhysElems; i++)
for(int me=1; me <= meqn; me++)
{
double m = 0.0;
for(int mp=1; mp <= mpoints; mp++)
{
// evaluate q at spts(mp) //
double qnow = 0.0;
for( int k=1; k <= kmax; k++ )
{
qnow += q.get(i,me,k) * phi.get(mp,k);
}
m = Min(m, qnow);
}
double theta = 0.0;
double Q1 = q.get(i,me,1); assert_ge( Q1, -1e-13 );
if( fabs( Q1 - m ) < 1.0e-14 ){ theta = 1.0; }
else{ theta = Min( 1.0, fabs( Q1 / (Q1 - m) ) ); }
// limit q //
for( int k=2; k <= kmax; k++ )
{
q.set(i,me,k, q.get(i,me,k) * theta );
}
}
}
// Modified version of the all purpose routine L2Project specifically written
// for projecting the "time-averaged" flux function onto the basis function.
//
// This routine also returns the coefficients of the Lax Wendroff Flux
// Function when expanded with legendre basis functions, and therefore the
// basis expansions produced by this routine can be used for all of the
// Riemann solves.
//
// ---------------------------------------------------------------------
// Inputs should have the following sizes:
// TODO - document the inputs here
// ---------------------------------------------------------------------
void L2ProjectLxW_Unst( const int mterms,
const double alpha, const double beta_dt, const double charlie_dt,
const int istart, const int iend, // Start-stop indices
const int QuadOrder,
const int BasisOrder_qin,
const int BasisOrder_auxin,
const int BasisOrder_fout,
const mesh& Mesh,
const dTensor3* qin, const dTensor3* auxin, // state vector
dTensor3* F, dTensor3* G, // time-averaged Flux function
void FluxFunc (const dTensor2& xpts,
const dTensor2& Q, const dTensor2& Aux, dTensor3& flux),
void DFluxFunc (const dTensor2& xpts,
const dTensor2& Q, const dTensor2& aux, dTensor4& Dflux),
void D2FluxFunc (const dTensor2& xpts,
const dTensor2& Q, const dTensor2& aux, dTensor5& D2flux) )
{
if( fabs( alpha ) < 1e-14 && fabs( beta_dt ) < 1e-14 && fabs( charlie_dt ) < 1e-14 )
{
F->setall(0.);
G->setall(0.);
return;
}
// starting and ending indices
const int NumElems = Mesh.get_NumElems();
assert_ge(istart,1);
assert_le(iend,NumElems);
// qin variable
assert_eq(NumElems,qin->getsize(1));
const int meqn = qin->getsize(2);
const int kmax_qin = qin->getsize(3);
assert_eq(kmax_qin,(BasisOrder_qin*(BasisOrder_qin+1))/2);
// auxin variable
assert_eq(NumElems,auxin->getsize(1));
const int maux = auxin->getsize(2);
const int kmax_auxin = auxin->getsize(3);
assert_eq(kmax_auxin,(BasisOrder_auxin*(BasisOrder_auxin+1))/2);
// fout variables
assert_eq(NumElems, F->getsize(1));
const int mcomps_out = F->getsize(2);
const int kmax_fout = F->getsize(3);
assert_eq(kmax_fout, (BasisOrder_fout*(BasisOrder_fout+1))/2 );
// number of quadrature points
assert_ge(QuadOrder, 1);
assert_le(QuadOrder, 5);
// Number of quadrature points
int mpoints;
switch( QuadOrder )
{
case 1:
mpoints = 1;
break;
case 2:
mpoints = 3;
break;
case 3:
mpoints = 6;
break;
case 4:
mpoints = 12;
break;
case 5:
mpoints = 16;
break;
}
const int kmax = iMax(iMax(kmax_qin, kmax_auxin), kmax_fout);
dTensor2 phi(mpoints, kmax); // Legendre basis (orthogonal)
dTensor2 spts(mpoints, 2); // List of quadrature points
dTensor1 wgts(mpoints); // List of quadrature weights
setQuadPoints_Unst( QuadOrder, wgts, spts );
// ---------------------------------------------------------------------- //
// Evaluate the basis functions at each point
SetLegendreAtPoints_Unst(spts, phi);
// ---------------------------------------------------------------------- //
// ---------------------------------------------------------------------- //
// First-order derivatives
dTensor2 phi_xi (mpoints, kmax );
dTensor2 phi_eta(mpoints, kmax );
SetLegendreGrad_Unst( spts, phi_xi, phi_eta );
// ---------------------------------------------------------------------- //
// ---------------------------------------------------------------------- //
// Second-order derivatives
dTensor2 phi_xi2 (mpoints, kmax );
dTensor2 phi_xieta(mpoints, kmax );
dTensor2 phi_eta2 (mpoints, kmax );
LegendreDiff2_Unst(spts, &phi_xi2, &phi_xieta, &phi_eta2 );
// ---------------------------------------------------------------------- //
// ------------------------------------------------------------- //
// Loop over every grid cell indexed by user supplied parameters //
// described by istart...iend, jstart...jend //
// ------------------------------------------------------------- //
#pragma omp parallel for
for (int i=istart; i<=iend; i++)
{
// These need to be defined locally. Each mesh element carries its
// own change of basis matrix, so these need to be recomputed for
// each element. The canonical derivatives, phi_xi, and phi_eta can
// be computed and shared for each element.
// First-order derivatives
dTensor2 phi_x(mpoints, kmax_fout); // x-derivative of Legendre basis (orthogonal)
dTensor2 phi_y(mpoints, kmax_fout); // y-derivative of Legendre basis (orthogonal)
// Second-order derivatives
dTensor2 phi_xx(mpoints, kmax_fout); // xx-derivative of Legendre basis (orthogonal)
dTensor2 phi_xy(mpoints, kmax_fout); // xy-derivative of Legendre basis (orthogonal)
dTensor2 phi_yy(mpoints, kmax_fout); // yy-derivative of Legendre basis (orthogonal)
//find center of current cell
const int i1 = Mesh.get_tnode(i,1);
const int i2 = Mesh.get_tnode(i,2);
const int i3 = Mesh.get_tnode(i,3);
// Corners:
const double x1 = Mesh.get_node(i1,1);
const double y1 = Mesh.get_node(i1,2);
const double x2 = Mesh.get_node(i2,1);
const double y2 = Mesh.get_node(i2,2);
const double x3 = Mesh.get_node(i3,1);
const double y3 = Mesh.get_node(i3,2);
// Center of current cell:
const double xc = (x1+x2+x3)/3.0;
const double yc = (y1+y2+y3)/3.0;
// Variables that need to be written to, and therefore are
// created for each thread
dTensor2 xpts (mpoints, 2);
dTensor2 qvals (mpoints, meqn);
dTensor2 auxvals(mpoints, maux);
// local storage for Flux function its Jacobian, and the Hessian:
dTensor3 fvals(mpoints, meqn, 2); // flux function (vector)
dTensor4 A(mpoints, meqn, meqn, 2); // Jacobian of flux
dTensor5 H(mpoints, meqn, meqn, meqn, 2); // Hessian of flux
// Compute q, aux and fvals at each Gaussian Quadrature point
// for this current cell indexed by (i,j)
// Save results into dTensor2 qvals, auxvals and fvals.
for (int m=1; m<= mpoints; m++)
{
// convert phi_xi and phi_eta derivatives
// to phi_x and phi_y derivatives through Jacobian
//
// Note that:
//
// pd_x = J11 pd_xi + J12 pd_eta and
// pd_y = J21 pd_xi + J22 pd_eta.
//
// Squaring these operators yields the second derivatives.
for (int k=1; k<=kmax_fout; k++)
{
phi_x.set(m,k, Mesh.get_jmat(i,1,1)*phi_xi.get(m,k)
+ Mesh.get_jmat(i,1,2)*phi_eta.get(m,k) );
phi_y.set(m,k, Mesh.get_jmat(i,2,1)*phi_xi.get(m,k)
+ Mesh.get_jmat(i,2,2)*phi_eta.get(m,k) );
phi_xx.set(m,k, Mesh.get_jmat(i,1,1)*Mesh.get_jmat(i,1,1)*phi_xi2.get(m,k)
+ Mesh.get_jmat(i,1,1)*Mesh.get_jmat(i,1,2)*phi_xieta.get(m,k)
+ Mesh.get_jmat(i,1,2)*Mesh.get_jmat(i,1,2)*phi_eta2.get(m,k)
);
phi_xy.set(m,k, Mesh.get_jmat(i,1,1)*Mesh.get_jmat(i,2,1)*phi_xi2.get(m,k)
+(Mesh.get_jmat(i,1,2)*Mesh.get_jmat(i,2,1)
+ Mesh.get_jmat(i,1,1)*Mesh.get_jmat(i,2,2))*phi_xieta.get(m,k)
+ Mesh.get_jmat(i,1,2)*Mesh.get_jmat(i,2,2)*phi_eta2.get(m,k)
);
phi_yy.set(m,k, Mesh.get_jmat(i,2,1)*Mesh.get_jmat(i,2,1)*phi_xi2.get(m,k)
+ Mesh.get_jmat(i,2,1)*Mesh.get_jmat(i,2,2)*phi_xieta.get(m,k)
+ Mesh.get_jmat(i,2,2)*Mesh.get_jmat(i,2,2)*phi_eta2.get(m,k)
);
}
// point on the unit triangle
const double s = spts.get(m,1);
const double t = spts.get(m,2);
// point on the physical triangle
xpts.set(m,1, xc + (x2-x1)*s + (x3-x1)*t );
xpts.set(m,2, yc + (y2-y1)*s + (y3-y1)*t );
// Solution values (q) at each grid point
for (int me=1; me<=meqn; me++)
{
qvals.set(m,me, 0.0 );
for (int k=1; k<=kmax_qin; k++)
{
qvals.set(m,me, qvals.get(m,me)
+ phi.get(m,k) * qin->get(i,me,k) );
}
}
// Auxiliary values (aux) at each grid point
for (int ma=1; ma<=maux; ma++)
{
auxvals.set(m,ma, 0.0 );
for (int k=1; k<=kmax_auxin; k++)
{
auxvals.set(m,ma, auxvals.get(m,ma)
+ phi.get(m,k) * auxin->get(i,ma,k) );
}
}
}
// ----------------------------------------------------------------- //
//
// Part I:
//
// Project the flux function onto the basis
// functions. This is the term of order O( 1 ) in the
// "time-averaged" Taylor expansion of f and g.
//
// ----------------------------------------------------------------- //
// Call user-supplied function to set fvals
FluxFunc(xpts, qvals, auxvals, fvals);
// Evaluate integral on current cell (project onto Legendre basis)
// using Gaussian Quadrature for the integration
//
// TODO - do we want to optimize this by looking into using transposes,
// as has been done in the 2d/cart code? (5/14/2014) -DS
for (int me=1; me<=mcomps_out; me++)
for (int k=1; k<=kmax; k++)
{
double tmp1 = 0.0;
double tmp2 = 0.0;
for (int mp=1; mp <= mpoints; mp++)
{
tmp1 += wgts.get(mp)*fvals.get(mp, me, 1)*phi.get(mp, k);
tmp2 += wgts.get(mp)*fvals.get(mp, me, 2)*phi.get(mp, k);
}
F->set(i, me, k, 2.0*tmp1 );
G->set(i, me, k, 2.0*tmp2 );
}
// ----------------------------------------------------------------- //
//
// Part II:
//
// Project the derivative of the flux function onto the basis
// functions. This is the term of order O( \dt ) in the
// "time-averaged" Taylor expansion of f and g.
//
// ----------------------------------------------------------------- //
// ----------------------------------------------------------------- //
// Compute pointwise values for fx+gy:
//
// We can't multiply fvals of f, and g,
// by alpha, otherwise we compute the wrong derivative here!
//
dTensor2 fx_plus_gy( mpoints, meqn ); fx_plus_gy.setall(0.);
for( int mp=1; mp <= mpoints; mp++ )
for( int me=1; me <= meqn; me++ )
{
double tmp = 0.;
for( int k=2; k <= kmax; k++ )
{
tmp += F->get( i, me, k ) * phi_x.get( mp, k );
tmp += G->get( i, me, k ) * phi_y.get( mp, k );
}
fx_plus_gy.set( mp, me, tmp );
}
// Call user-supplied Jacobian to set f'(q) and g'(q):
DFluxFunc( xpts, qvals, auxvals, A );
// place-holders for point values of
// f'(q)( fx + gy ) and g'(q)( fx + gy ):
dTensor2 dt_times_fdot( mpoints, meqn );
dTensor2 dt_times_gdot( mpoints, meqn );
// Compute point values for f'(q) * (fx+gy) and g'(q) * (fx+gy):
for( int mp=1; mp <= mpoints; mp++ )
for( int m1=1; m1 <= meqn; m1++ )
{
double tmp1 = 0.;
double tmp2 = 0.;
for( int m2=1; m2 <= meqn; m2++ )
{
tmp1 += A.get(mp, m1, m2, 1 ) * fx_plus_gy.get(mp, m2);
tmp2 += A.get(mp, m1, m2, 2 ) * fx_plus_gy.get(mp, m2);
}
dt_times_fdot.set( mp, m1, -beta_dt*tmp1 );
dt_times_gdot.set( mp, m1, -beta_dt*tmp2 );
}
// --- Third-order terms --- //
//
// These are the terms that are O( \dt^2 ) in the "time-averaged"
// flux function.
dTensor2 f_tt( mpoints, meqn ); f_tt.setall(0.);
dTensor2 g_tt( mpoints, meqn ); g_tt.setall(0.);
if( mterms > 2 )
{
// Construct the Hessian at each (quadrature) point
D2FluxFunc( xpts, qvals, auxvals, H );
// Second-order derivative terms
dTensor2 qx_vals (mpoints, meqn); qx_vals.setall(0.);
dTensor2 qy_vals (mpoints, meqn); qy_vals.setall(0.);
dTensor2 fxx_vals(mpoints, meqn); fxx_vals.setall(0.);
dTensor2 gxx_vals(mpoints, meqn); gxx_vals.setall(0.);
dTensor2 fxy_vals(mpoints, meqn); fxy_vals.setall(0.);
dTensor2 gxy_vals(mpoints, meqn); gxy_vals.setall(0.);
dTensor2 fyy_vals(mpoints, meqn); fyy_vals.setall(0.);
dTensor2 gyy_vals(mpoints, meqn); gyy_vals.setall(0.);
for( int m=1; m <= mpoints; m++ )
for( int me=1; me <= meqn; me++ )
{
// Can start at k=1, because derivative of a constant is
// zero.
double tmp_qx = 0.;
double tmp_qy = 0.;
for( int k=2; k <= kmax; k++ )
{
tmp_qx += phi_x.get(m,k) * qin->get(i,me,k);
tmp_qy += phi_y.get(m,k) * qin->get(i,me,k);
}
qx_vals.set(m,me, tmp_qx );
qy_vals.set(m,me, tmp_qy );
// First non-zero terms start at third-order.
for( int k=4; k <= kmax; k++ )
{
fxx_vals.set(m,me, fxx_vals.get(m,me) + phi_xx.get(m,k)*F->get(i,me,k) );
gxx_vals.set(m,me, gxx_vals.get(m,me) + phi_xx.get(m,k)*G->get(i,me,k) );
fxy_vals.set(m,me, fxy_vals.get(m,me) + phi_xy.get(m,k)*F->get(i,me,k) );
gxy_vals.set(m,me, gxy_vals.get(m,me) + phi_xy.get(m,k)*G->get(i,me,k) );
fyy_vals.set(m,me, fyy_vals.get(m,me) + phi_yy.get(m,k)*F->get(i,me,k) );
gyy_vals.set(m,me, gyy_vals.get(m,me) + phi_yy.get(m,k)*G->get(i,me,k) );
}
}
// ----------------------------------- //
// Part I: Compute (f_x + g_y)_{,t}
// ----------------------------------- //
// Compute terms that get multiplied by \pd2{ f }{ q } and \pd2{ g }{ q }.
dTensor2 fx_plus_gy_t( mpoints, meqn );
for( int m = 1; m <= mpoints; m++ )
for( int me = 1; me <= meqn; me++ )
{
double tmp = 0.;
// Terms that get multiplied by the Hessian:
for( int m1=1; m1 <= meqn; m1++ )
for( int m2=1; m2 <= meqn; m2++ )
{
tmp += H.get(m,me,m1,m2,1)*qx_vals.get(m,m1)*fx_plus_gy.get(m,m2);
tmp += H.get(m,me,m1,m2,2)*qy_vals.get(m,m1)*fx_plus_gy.get(m,m2);
}
// Terms that get multiplied by f'(q) and g'(q):
for( int m1=1; m1 <= meqn; m1++ )
{
tmp += A.get(m,me,m1,1)*( fxx_vals.get(m,m1)+gxy_vals.get(m,m1) );
tmp += A.get(m,me,m1,2)*( fxy_vals.get(m,m1)+gyy_vals.get(m,m1) );
}
fx_plus_gy_t.set( m, me, tmp );
}
// ----------------------------------- //
// Part II: Compute
// f'(q) * fx_plus_gy_t and
// g'(q) * fx_plus_gy_t
// ----------------------------------- //
// Add in the third term that gets multiplied by A:
for( int m=1; m <= mpoints; m++ )
for( int m1=1; m1 <= meqn; m1++ )
{
double tmp1 = 0.;
double tmp2 = 0.;
for( int m2=1; m2 <= meqn; m2++ )
{
tmp1 += A.get(m,m1,m2,1)*fx_plus_gy_t.get(m,m2);
tmp2 += A.get(m,m1,m2,2)*fx_plus_gy_t.get(m,m2);
}
f_tt.set( m, m1, tmp1 );
g_tt.set( m, m1, tmp2 );
}
// ----------------------------------------------- //
// Part III: Add in contributions from
// f''(q) * (fx_plus_gy, fx_plus_gy ) and
// g''(q) * (fx_plus_gy, fx_plus_gy ).
// ----------------------------------------------- //
for( int m =1; m <= mpoints; m++ )
for( int me =1; me <= meqn; me++ )
{
double tmp1 = 0.;
double tmp2 = 0.;
// Terms that get multiplied by the Hessian:
for( int m1=1; m1 <= meqn; m1++ )
for( int m2=1; m2 <= meqn; m2++ )
{
tmp1 += H.get(m,me,m1,m2,1)*fx_plus_gy.get(m,m1)*fx_plus_gy.get(m,m2);
tmp2 += H.get(m,me,m1,m2,2)*fx_plus_gy.get(m,m1)*fx_plus_gy.get(m,m2);
}
f_tt.set( m, me, f_tt.get(m,me) + tmp1 );
g_tt.set( m, me, g_tt.get(m,me) + tmp2 );
}
} // End of computing "third"-order terms
// ---------------------------------------------------------- //
//
// Construct basis coefficients (integrate_on_current_cell)
//
// ---------------------------------------------------------- //
for (int me=1; me<=mcomps_out; me++)
for (int k=1; k<=kmax; k++)
{
double tmp1 = 0.0;
double tmp2 = 0.0;
for (int mp=1; mp<=mpoints; mp++)
{
tmp1 += wgts.get(mp)*phi.get(mp,k)*(
dt_times_fdot.get(mp, me) + charlie_dt*f_tt.get(mp, me) );
tmp2 += wgts.get(mp)*phi.get(mp,k)*(
dt_times_gdot.get(mp, me) + charlie_dt*g_tt.get(mp, me) );
}
F->set(i,me,k, F->get(i,me,k) + 2.0*tmp1 );
G->set(i,me,k, G->get(i,me,k) + 2.0*tmp2 );
}
}
}
void ConstructL_Unst(
const double t,
const dTensor2* vel_vec,
const mesh& Mesh,
const edge_data_Unst& EdgeData,
dTensor3& aux, // SetBndValues_Unst modifies ghost cells
dTensor3& q, // SetBndValues_Unst modifies ghost cells
dTensor3& Lstar,
dTensor1& smax)
{
const int NumElems = Mesh.get_NumElems();
const int NumPhysElems = Mesh.get_NumPhysElems();
const int NumEdges = Mesh.get_NumEdges();
const int meqn = q.getsize(2);
const int kmax = q.getsize(3);
const int maux = aux.getsize(2);
const int space_order = dogParams.get_space_order();
dTensor3 EdgeFluxIntegral(NumElems,meqn,kmax);
dTensor3 ElemFluxIntegral(NumElems,meqn,kmax);
dTensor3 Psi(NumElems,meqn,kmax);
// ---------------------------------------------------------
// Boundary Conditions
SetBndValues_Unst(Mesh,&q,&aux);
// Positivity limiter
void ApplyPosLimiter_Unst(const mesh& Mesh, const dTensor3& aux, dTensor3& q);
if( dogParams.using_moment_limiter() )
{ ApplyPosLimiter_Unst(Mesh, aux, q); }
// ---------------------------------------------------------
// ---------------------------------------------------------
// Part I: compute flux integral on element edges
// ---------------------------------------------------------
// Loop over all interior edges and solve Riemann problems
// dTensor1 nvec(2);
// Loop over all interior edges
EdgeFluxIntegral.setall(0.);
ElemFluxIntegral.setall(0.);
// Loop over all interior edges
#pragma omp parallel for
for (int i=1; i<=NumEdges; i++)
{
// Edge coordinates
double x1 = Mesh.get_edge(i,1);
double y1 = Mesh.get_edge(i,2);
double x2 = Mesh.get_edge(i,3);
double y2 = Mesh.get_edge(i,4);
// Elements on either side of edge
int ileft = Mesh.get_eelem(i,1);
int iright = Mesh.get_eelem(i,2);
double Areal = Mesh.get_area_prim(ileft);
double Arear = Mesh.get_area_prim(iright);
// Scaled normal to edge
dTensor1 nhat(2);
nhat.set(1, (y2-y1) );
nhat.set(2, (x1-x2) );
// Variables to store flux integrals along edge
dTensor2 Fr_tmp(meqn,dogParams.get_space_order());
dTensor2 Fl_tmp(meqn,dogParams.get_space_order());
// Loop over number of quadrature points along each edge
for (int ell=1; ell<=dogParams.get_space_order(); ell++)
{
dTensor1 Ql(meqn),Qr(meqn);
dTensor1 Auxl(maux),Auxr(maux);
// Riemann data - q
for (int m=1; m<=meqn; m++)
{
Ql.set(m, 0.0 );
Qr.set(m, 0.0 );
for (int k=1; k<=kmax; k++)
{
Ql.set(m, Ql.get(m) + EdgeData.phi_left->get(i,ell,k)
*q.get(ileft, m,k) );
Qr.set(m, Qr.get(m) + EdgeData.phi_right->get(i,ell,k)
*q.get(iright,m,k) );
}
}
// Riemann data - aux
for (int m=1; m<=maux; m++)
{
Auxl.set(m, 0.0 );
Auxr.set(m, 0.0 );
for (int k=1; k<=kmax; k++)
{
Auxl.set(m, Auxl.get(m) + EdgeData.phi_left->get(i,ell,k)
*aux.get(ileft, m,k) );
Auxr.set(m, Auxr.get(m) + EdgeData.phi_right->get(i,ell,k)
*aux.get(iright,m,k) );
}
}
// Solve Riemann problem
dTensor1 xedge(2);
double s = EdgeData.xpts1d->get(ell);
xedge.set(1, x1 + 0.5*(s+1.0)*(x2-x1) );
xedge.set(2, y1 + 0.5*(s+1.0)*(y2-y1) );
dTensor1 Fl(meqn),Fr(meqn);
const double smax_edge = RiemannSolve(vel_vec, nhat, xedge, Ql, Qr, Auxl, Auxr, Fl, Fr);
smax.set(i, Max(smax_edge,smax.get(i)) );
// Construct fluxes
for (int m=1; m<=meqn; m++)
{
Fr_tmp.set(m,ell, Fr.get(m) );
Fl_tmp.set(m,ell, Fl.get(m) );
}
}
// Add edge integral to line integral around the full element
for (int m=1; m<=meqn; m++)
for (int k=1; k<=kmax; k++)
{
double Fl_sum = 0.0;
double Fr_sum = 0.0;
for (int ell=1; ell<=dogParams.get_space_order(); ell++)
{
Fl_sum = Fl_sum + 0.5*EdgeData.wgts1d->get(ell)
*EdgeData.phi_left->get(i,ell,k) *Fl_tmp.get(m,ell);
Fr_sum = Fr_sum + 0.5*EdgeData.wgts1d->get(ell)
*EdgeData.phi_right->get(i,ell,k)*Fr_tmp.get(m,ell);
}
EdgeFluxIntegral.set(ileft, m,k, EdgeFluxIntegral.get(ileft, m,k) + Fl_sum/Areal );
EdgeFluxIntegral.set(iright,m,k, EdgeFluxIntegral.get(iright,m,k) - Fr_sum/Arear );
}
}
// ---------------------------------------------------------
// ---------------------------------------------------------
// Part II: compute intra-element contributions
// ---------------------------------------------------------
L2ProjectGrad_Unst(vel_vec, 1,NumPhysElems,
space_order,space_order,space_order,space_order,
Mesh,&q,&aux,&ElemFluxIntegral,&FluxFunc);
// ---------------------------------------------------------
// ---------------------------------------------------------
// Part III: compute source term
// ---------------------------------------------------------
if ( dogParams.get_source_term()>0 )
{
// Set source term on computational grid
// Set values and apply L2-projection
L2Project_Unst(t, vel_vec, 1,NumPhysElems,
space_order,space_order,space_order,space_order,
Mesh,&q,&aux,&Psi,&SourceTermFunc);
}
// ---------------------------------------------------------
// ---------------------------------------------------------
// Part IV: construct Lstar
// ---------------------------------------------------------
if (dogParams.get_source_term()==0) // Without Source Term
{
#pragma omp parallel for
for (int i=1; i<=NumPhysElems; i++)
for (int m=1; m<=meqn; m++)
for (int k=1; k<=kmax; k++)
{
double tmp = ElemFluxIntegral.get(i,m,k) - EdgeFluxIntegral.get(i,m,k);
Lstar.set(i,m,k, tmp );
}
}
else // With Source Term
{
#pragma omp parallel for
for (int i=1; i<=NumPhysElems; i++)
for (int m=1; m<=meqn; m++)
for (int k=1; k<=kmax; k++)
{
double tmp = ElemFluxIntegral.get(i,m,k)
- EdgeFluxIntegral.get(i,m,k)
+ Psi.get(i,m,k);
Lstar.set(i,m,k, tmp );
}
}
// ---------------------------------------------------------
// ---------------------------------------------------------
// Part V: add extra contributions to Lstar
// ---------------------------------------------------------
// Call LstarExtra
LstarExtra_Unst(Mesh,&q,&aux,&Lstar);
// ---------------------------------------------------------
}
