interface_elements.cc

Go to the documentation of this file.

// LIC// ====================================================================
// LIC// This file forms part of oomph-lib, the object-oriented,
// LIC// multi-physics finite-element library, available
// LIC// at http://www.oomph-lib.org.
// LIC//
// LIC// Copyright (C) 2006-2024 Matthias Heil and Andrew Hazel
// LIC//
// LIC// This library is free software; you can redistribute it and/or
// LIC// modify it under the terms of the GNU Lesser General Public
// LIC// License as published by the Free Software Foundation; either
// LIC// version 2.1 of the License, or (at your option) any later version.
// LIC//
// LIC// This library is distributed in the hope that it will be useful,
// LIC// but WITHOUT ANY WARRANTY; without even the implied warranty of
// LIC// MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE.  See the GNU
// LIC// Lesser General Public License for more details.
// LIC//
// LIC// You should have received a copy of the GNU Lesser General Public
// LIC// License along with this library; if not, write to the Free Software
// LIC// Foundation, Inc., 51 Franklin Street, Fifth Floor, Boston, MA
// LIC// 02110-1301  USA.
// LIC//
// LIC// The authors may be contacted at oomph-lib@maths.man.ac.uk.
// LIC//
// LIC//====================================================================
// Non-inline functions for fluid free surface elements
 
// OOMPH-LIB headers
#include "interface_elements.h"
#include "../generic/integral.h"
 
 
namespace oomph
{
  /// ///////////////////////////////////////////////////////////////
  /// ///////////////////////////////////////////////////////////////
  /// ///////////////////////////////////////////////////////////////
 
 
  //=========================================================================
  /// Set a pointer to the desired contact angle. Optional boolean
  /// (defaults to true)
  /// chooses strong imposition via hijacking (true) or weak imposition
  /// via addition to momentum equation (false). The default strong imposition
  /// is appropriate for static contact problems.
  //=========================================================================
  void FluidInterfaceBoundingElement::set_contact_angle(double* const& angle_pt,
                                                        const bool& strong)
  {
    // Set the pointer to the contact angle
    Contact_angle_pt = angle_pt;
 
    // If we are hijacking the kinematic condition (the default)
    // to do the strong (pointwise form of the contact-angle condition)
    if (strong)
    {
      // Remember what we're doing
      Contact_angle_flag = 1;
 
      // Hijack the bulk element residuals
      dynamic_cast<FluidInterfaceElement*>(bulk_element_pt())
        ->hijack_kinematic_conditions(Bulk_node_number);
    }
    // Otherwise, we'll impose it weakly via the momentum equations.
    // This will require that the appropriate velocity node is unpinned,
    // which is why this is a bad choice for static contact problems in which
    // there is a no-slip condition on the wall. In that case, the momentum
    // equation is never assembled and so the contact angle condition is not
    // applied unless we use the strong version above.
    else
    {
      Contact_angle_flag = 2;
    }
  }
 
 
  /// ///////////////////////////////////////////////////////////////
  /// ///////////////////////////////////////////////////////////////
  /// ///////////////////////////////////////////////////////////////
 
 
  //=========================================================================
  /// Add contribution to element's residual vector and Jacobian
  //=========================================================================
  void PointFluidInterfaceBoundingElement::
    fill_in_generic_residual_contribution_interface_boundary(
      Vector<double>& residuals, DenseMatrix<double>& jacobian, unsigned flag)
  {
    // Let's get the info from the parent
    FiniteElement* parent_pt = bulk_element_pt();
 
    // Find the dimension of the problem
    unsigned spatial_dim = this->nodal_dimension();
 
    // Outer unit normal to the wall
    Vector<double> wall_normal(spatial_dim);
 
    // Outer unit normal to the free surface
    Vector<double> unit_normal(spatial_dim);
 
    // Storage for the coordinate
    Vector<double> x(spatial_dim);
 
    // Find the dimension of the parent
    unsigned n_dim = parent_pt->dim();
 
    // Dummy local coordinate, of size zero
    Vector<double> s_local(0);
 
    // Get the x coordinate
    this->interpolated_x(s_local, x);
 
    // Get the unit normal to the wall
    wall_unit_normal(x, wall_normal);
 
    // Find the local coordinates in the parent
    Vector<double> s_parent(n_dim);
    this->get_local_coordinate_in_bulk(s_local, s_parent);
 
    // Just get the outer unit normal
    dynamic_cast<FaceElement*>(parent_pt)->outer_unit_normal(s_parent,
                                                             unit_normal);
 
    // Find the dot product of the two vectors
    double dot = 0.0;
    for (unsigned i = 0; i < spatial_dim; i++)
    {
      dot += unit_normal[i] * wall_normal[i];
    }
 
    // Get the value of sigma from the parent
    double sigma_local =
      dynamic_cast<FluidInterfaceElement*>(parent_pt)->sigma(s_parent);
 
    // Are we doing the weak form replacement
    if (Contact_angle_flag == 2)
    {
      // Get the wall tangent vector
      Vector<double> wall_tangent(spatial_dim);
      wall_tangent[0] = -wall_normal[1];
      wall_tangent[1] = wall_normal[0];
 
      // Get the capillary number
      double ca_local = ca();
 
      // Just add the appropriate contribution to the momentum equations
      for (unsigned i = 0; i < 2; i++)
      {
        int local_eqn = nodal_local_eqn(0, this->U_index_interface_boundary[i]);
        if (local_eqn >= 0)
        {
          residuals[local_eqn] +=
            (sigma_local / ca_local) * (sin(contact_angle()) * wall_normal[i] +
                                        cos(contact_angle()) * wall_tangent[i]);
        }
      }
    }
    // Otherwise [strong imposition (by hijacking) of contact angle or
    // "no constraint at all"], add the appropriate contribution to
    // the momentum equation
    else
    {
      // Need to find the current outer normal from the surface
      // which does not necessarily correspond to an imposed angle.
      // It is whatever it is...
      Vector<double> m(spatial_dim);
      this->outer_unit_normal(s_local, m);
 
      // Get the capillary number
      double ca_local = ca();
 
      // Just add the appropriate contribution to the momentum equations
      // This will, of course, not be added if the equation is pinned
      //(no slip)
      for (unsigned i = 0; i < 2; i++)
      {
        int local_eqn = nodal_local_eqn(0, this->U_index_interface_boundary[i]);
        if (local_eqn >= 0)
        {
          residuals[local_eqn] += (sigma_local / ca_local) * m[i];
        }
      }
    }
 
    // If we are imposing the contact angle strongly (by hijacking)
    // overwrite the kinematic equation
    if (Contact_angle_flag == 1)
    {
      // Read out the kinematic equation number
      int local_eqn = kinematic_local_eqn(0);
 
      // Note that because we have outer unit normals for the free surface
      // and the wall, the cosine of the contact angle is equal to
      // MINUS the dot product computed above
      if (local_eqn >= 0)
      {
        residuals[local_eqn] = cos(contact_angle()) + dot;
      }
      // NOTE: The jacobian entries will be computed automatically
      // by finite differences.
    }
 
    // Dummy arguments
    Shape psif(1);
    DShape dpsifds(1, 1);
    Vector<double> interpolated_n(1);
    double W = 0.0;
 
    // Now add the additional contributions
    add_additional_residual_contributions_interface_boundary(
      residuals, jacobian, flag, psif, dpsifds, interpolated_n, W);
  }
 
 
  /// ///////////////////////////////////////////////////////////////
  /// ///////////////////////////////////////////////////////////////
  /// ///////////////////////////////////////////////////////////////
 
 
  //=========================================================================
  /// Add contribution to element's residual vector and Jacobian
  //=========================================================================
  void LineFluidInterfaceBoundingElement::
    fill_in_generic_residual_contribution_interface_boundary(
      Vector<double>& residuals, DenseMatrix<double>& jacobian, unsigned flag)
  {
    // Let's get the info from the parent
    FiniteElement* parent_pt = bulk_element_pt();
 
    // Find the dimension of the problem
    unsigned spatial_dim = this->nodal_dimension();
 
    // Outer unit normal to the wall
    Vector<double> wall_normal(spatial_dim);
 
    // Outer unit normal to the free surface
    Vector<double> unit_normal(spatial_dim);
 
    // Find the dimension of the parent
    unsigned n_dim = parent_pt->dim();
 
    // Find the local coordinates in the parent
    Vector<double> s_parent(n_dim);
 
    // Storage for the shape functions
    unsigned n_node = this->nnode();
    Shape psi(n_node);
    DShape dpsids(n_node, 1);
    Vector<double> s_local(1);
 
    // Loop over intergration points
    unsigned n_intpt = this->integral_pt()->nweight();
    for (unsigned ipt = 0; ipt < n_intpt; ++ipt)
    {
      // Get the local coordinate of the integration point
      s_local[0] = this->integral_pt()->knot(ipt, 0);
      get_local_coordinate_in_bulk(s_local, s_parent);
 
      // Get the local shape functions
      this->dshape_local(s_local, psi, dpsids);
 
      // Zero the position
      Vector<double> x(spatial_dim, 0.0);
 
      // Now construct the position and the tangent
      Vector<double> interpolated_t1(spatial_dim, 0.0);
      for (unsigned n = 0; n < n_node; n++)
      {
        const double psi_local = psi(n);
        const double dpsi_local = dpsids(n, 0);
        for (unsigned i = 0; i < spatial_dim; i++)
        {
          double pos = this->nodal_position(n, i);
          interpolated_t1[i] += pos * dpsi_local;
          x[i] += pos * psi_local;
        }
      }
 
      // Now we can calculate the Jacobian term
      double t_length = 0.0;
      for (unsigned i = 0; i < spatial_dim; ++i)
      {
        t_length += interpolated_t1[i] * interpolated_t1[i];
      }
      double W = std::sqrt(t_length) * this->integral_pt()->weight(ipt);
 
      // Imposition of contact angle in weak form
      if (Contact_angle_flag == 2)
      {
        // Get the outer unit normal of the entire interface
        dynamic_cast<FaceElement*>(parent_pt)->outer_unit_normal(s_parent,
                                                                 unit_normal);
 
        // Calculate the wall normal
        wall_unit_normal(x, wall_normal);
 
        // Find the dot product of the two
        double dot = 0.0;
        for (unsigned i = 0; i < spatial_dim; i++)
        {
          dot += unit_normal[i] * wall_normal[i];
        }
 
        // Find the projection of the outer normal of the surface into the plane
        Vector<double> binorm(spatial_dim);
        for (unsigned i = 0; i < spatial_dim; i++)
        {
          binorm[i] = unit_normal[i] - dot * wall_normal[i];
        }
 
        // Get the value of sigma from the parent
        const double sigma_local =
          dynamic_cast<FluidInterfaceElement*>(parent_pt)->sigma(s_parent);
 
        // Get the capillary number
        const double ca_local = ca();
 
        // Get the contact angle
        const double theta = contact_angle();
 
        // Add the contributions to the momentum equation
 
        // Loop over the shape functions
        for (unsigned l = 0; l < n_node; l++)
        {
          // Loop over the velocity components
          for (unsigned i = 0; i < 3; i++)
          {
            // Get the equation number for the momentum equation
            int local_eqn =
              this->nodal_local_eqn(l, this->U_index_interface_boundary[i]);
 
            // If it's not a boundary condition
            if (local_eqn >= 0)
            {
              // Add the surface-tension contribution to the momentum equation
              residuals[local_eqn] +=
                (sigma_local / ca_local) *
                (sin(theta) * wall_normal[i] + cos(theta) * binorm[i]) *
                psi(l) * W;
            }
          }
        }
      }
      // Otherwise [strong imposition (by hijacking) of contact angle or
      // "no constraint at all"], add the appropriate contribution to
      // the momentum equation
      else
      {
        // Storage for the outer vector
        Vector<double> m(3);
 
        // Get the outer unit normal of the line
        this->outer_unit_normal(s_local, m);
 
        // Get the value of sigma from the parent
        const double sigma_local =
          dynamic_cast<FluidInterfaceElement*>(parent_pt)->sigma(s_parent);
 
        // Get the capillary number
        const double ca_local = ca();
 
        // Loop over the shape functions
        for (unsigned l = 0; l < n_node; l++)
        {
          // Loop over the velocity components
          for (unsigned i = 0; i < 3; i++)
          {
            // Get the equation number for the momentum equation
            int local_eqn =
              this->nodal_local_eqn(l, this->U_index_interface_boundary[i]);
 
            // If it's not a boundary condition
            if (local_eqn >= 0)
            {
              // Add the surface-tension contribution to the momentum equation
              residuals[local_eqn] +=
                m[i] * (sigma_local / ca_local) * psi(l) * W;
            }
          }
        }
      } // End of the line integral terms
 
 
      // If we are imposing the contact angle strongly (by hijacking)
      // overwrite the kinematic equation
      if (Contact_angle_flag == 1)
      {
        // Get the outer unit normal of the whole interface
        dynamic_cast<FaceElement*>(parent_pt)->outer_unit_normal(s_parent,
                                                                 unit_normal);
 
        // Calculate the wall normal
        wall_unit_normal(x, wall_normal);
 
        // Find the dot product
        double dot = 0.0;
        for (unsigned i = 0; i < spatial_dim; i++)
        {
          dot += unit_normal[i] * wall_normal[i];
        }
 
        // Loop over the test functions
        for (unsigned l = 0; l < n_node; l++)
        {
          // Read out the kinematic equation number
          int local_eqn = kinematic_local_eqn(l);
 
          // Note that because we have outer unit normals for the free surface
          // and the wall, the cosine of the contact angle is equal to
          // MINUS the dot product
          if (local_eqn >= 0)
          {
            residuals[local_eqn] += (cos(contact_angle()) + dot) * psi(l) * W;
          }
          // NOTE: The jacobian entries will be computed automatically
          // by finite differences.
        }
      } // End of strong form of contact angle condition
 
      // Add any additional residual contributions
      add_additional_residual_contributions_interface_boundary(
        residuals, jacobian, flag, psi, dpsids, unit_normal, W);
    }
  }
 
 
  /// //////////////////////////////////////////////////////////////
  /// //////////////////////////////////////////////////////////////
  /// //////////////////////////////////////////////////////////////
 
 
  //============================================================
  /// Default value for physical constant (static)
  //============================================================
  double FluidInterfaceElement::Default_Physical_Constant_Value = 1.0;
 
 
  //================================================================
  /// Calculate the i-th velocity component at local coordinate s
  //================================================================
  double FluidInterfaceElement::interpolated_u(const Vector<double>& s,
                                               const unsigned& i)
  {
    // Find number of nodes
    unsigned n_node = FiniteElement::nnode();
 
    // Storage for the local shape function
    Shape psi(n_node);
 
    // Get values of shape function at local coordinate s
    this->shape(s, psi);
 
    // Initialise value of u
    double interpolated_u = 0.0;
 
    // Loop over the local nodes and sum
    for (unsigned l = 0; l < n_node; l++)
    {
      interpolated_u += u(l, i) * psi(l);
    }
 
    return (interpolated_u);
  }
 
  //===========================================================================
  /// Calculate the contribution to the residuals from the interface
  /// implemented generically with geometric information to be
  /// added from the specific elements
  //========================================================================
  void FluidInterfaceElement::fill_in_generic_residual_contribution_interface(
    Vector<double>& residuals, DenseMatrix<double>& jacobian, unsigned flag)
  {
    // Find out how many nodes there are
    unsigned n_node = this->nnode();
 
    // Set up memeory for the shape functions
    Shape psif(n_node);
 
    // Find out the number of surface coordinates
    const unsigned el_dim = this->dim();
    // We have el_dim local surface coordinates
    DShape dpsifds(n_node, el_dim);
 
    // Find the dimension of the problem
    // Note that this will return 2 for the axisymmetric case
    // which is correct in the sense that no
    // terms will be added in the azimuthal direction
    const unsigned n_dim = this->nodal_dimension();
 
    // Storage for the surface gradient
    // and divergence terms
    // These will actually be identical
    // apart from in the axisymmetric case
    DShape dpsifdS(n_node, n_dim);
    DShape dpsifdS_div(n_node, n_dim);
 
    // Set the value of n_intpt
    unsigned n_intpt = this->integral_pt()->nweight();
 
    // Get the value of the Capillary number
    double Ca = ca();
 
    // Get the value of the Strouhal numer
    double St = st();
 
    // Get the value of the external pressure
    double p_ext = pext();
 
    // Integers used to hold the local equation numbers and local unknowns
    int local_eqn = 0, local_unknown = 0;
 
    // Storage for the local coordinate
    Vector<double> s(el_dim);
 
    // Loop over the integration points
    for (unsigned ipt = 0; ipt < n_intpt; ipt++)
    {
      // Get the value of the local coordiantes at the integration point
      for (unsigned i = 0; i < el_dim; i++)
      {
        s[i] = this->integral_pt()->knot(ipt, i);
      }
 
      // Get the integral weight
      double W = this->integral_pt()->weight(ipt);
 
      // Call the derivatives of the shape function
      this->dshape_local_at_knot(ipt, psif, dpsifds);
 
      // Define and zero the tangent Vectors and local velocities
      Vector<double> interpolated_x(n_dim, 0.0);
      Vector<double> interpolated_u(n_dim, 0.0);
      Vector<double> interpolated_dx_dt(n_dim, 0.0);
      ;
      DenseMatrix<double> interpolated_t(el_dim, n_dim, 0.0);
 
      // Loop over the shape functions
      for (unsigned l = 0; l < n_node; l++)
      {
        const double psi_ = psif(l);
        // Loop over directional components
        for (unsigned i = 0; i < n_dim; i++)
        {
          // Coordinate
          interpolated_x[i] += this->nodal_position(l, i) * psi_;
 
          // Calculate velocity of mesh
          interpolated_dx_dt[i] += this->dnodal_position_dt(l, i) * psi_;
 
          // Calculate the tangent vectors
          for (unsigned j = 0; j < el_dim; j++)
          {
            interpolated_t(j, i) += this->nodal_position(l, i) * dpsifds(l, j);
          }
 
          // Calculate velocity and tangent vector
          interpolated_u[i] += u(l, i) * psi_;
        }
      }
 
 
      // Calculate the surface gradient and divergence
      double J = this->compute_surface_derivatives(
        psif, dpsifds, interpolated_t, interpolated_x, dpsifdS, dpsifdS_div);
      // Get the normal vector
      //(ALH: This could be more efficient because
      // there is some recomputation of shape functions here)
      Vector<double> interpolated_n(n_dim);
      this->outer_unit_normal(s, interpolated_n);
 
      // Now also get the (possible variable) surface tension
      double Sigma = this->sigma(s);
 
      // Loop over the shape functions
      for (unsigned l = 0; l < n_node; l++)
      {
        // Loop over the velocity components
        for (unsigned i = 0; i < n_dim; i++)
        {
          // Get the equation number for the momentum equation
          local_eqn = this->nodal_local_eqn(l, this->U_index_interface[i]);
 
          // If it's not a boundary condition
          if (local_eqn >= 0)
          {
            // Add the surface-tension contribution to the momentum equation
            residuals[local_eqn] -= (Sigma / Ca) * dpsifdS_div(l, i) * J * W;
 
            // If the element is a free surface, add in the external pressure
            if (Pext_data_pt != 0)
            {
              // External pressure term
              residuals[local_eqn] -=
                p_ext * interpolated_n[i] * psif(l) * J * W;
 
              // Add in the Jacobian term for the external pressure
              // The correct area is included in the length of the normal
              // vector
              if (flag)
              {
                local_unknown = pext_local_eqn();
                if (local_unknown >= 0)
                {
                  jacobian(local_eqn, local_unknown) -=
                    interpolated_n[i] * psif(l) * J * W;
                }
              }
            } // End of pressure contribution
          }
        } // End of contribution to momentum equation
 
 
        // Kinematic BC
        local_eqn = kinematic_local_eqn(l);
        if (local_eqn >= 0)
        {
          // Assemble the kinematic condition
          // The correct area is included in the normal vector
          for (unsigned k = 0; k < n_dim; k++)
          {
            residuals[local_eqn] +=
              (interpolated_u[k] - St * interpolated_dx_dt[k]) *
              interpolated_n[k] * psif(l) * J * W;
          }
 
          // Add in the jacobian
          if (flag)
          {
            // Loop over shape functions
            for (unsigned l2 = 0; l2 < n_node; l2++)
            {
              // Loop over the components
              for (unsigned i2 = 0; i2 < n_dim; i2++)
              {
                local_unknown =
                  this->nodal_local_eqn(l2, this->U_index_interface[i2]);
                // If it's a non-zero dof add
                if (local_unknown >= 0)
                {
                  jacobian(local_eqn, local_unknown) +=
                    psif(l2) * interpolated_n[i2] * psif(l) * J * W;
                }
              }
            }
          } // End of Jacobian contribution
        }
      } // End of loop over shape functions
 
 
      // Add additional contribution required from the implementation
      // of the node update (e.g. Lagrange multpliers etc)
      add_additional_residual_contributions_interface(residuals,
                                                      jacobian,
                                                      flag,
                                                      psif,
                                                      dpsifds,
                                                      dpsifdS,
                                                      dpsifdS_div,
                                                      s,
                                                      interpolated_x,
                                                      interpolated_n,
                                                      W,
                                                      J);
 
    } // End of loop over integration points
  }
 
  //========================================================
  /// Overload the output functions generically
  //=======================================================
  void FluidInterfaceElement::output(std::ostream& outfile,
                                     const unsigned& n_plot)
  {
    const unsigned el_dim = this->dim();
    const unsigned n_dim = this->nodal_dimension();
    const unsigned n_velocity = this->U_index_interface.size();
    // Set output Vector
    Vector<double> s(el_dim);
 
    // Tecplot header info
    outfile << tecplot_zone_string(n_plot);
 
    // Loop over plot points
    unsigned num_plot_points = nplot_points(n_plot);
    for (unsigned iplot = 0; iplot < num_plot_points; iplot++)
    {
      // Get local coordinates of pliot point
      get_s_plot(iplot, n_plot, s);
 
      // Output the x,y,u,v
      for (unsigned i = 0; i < n_dim; i++)
        outfile << this->interpolated_x(s, i) << " ";
      for (unsigned i = 0; i < n_velocity; i++)
        outfile << interpolated_u(s, i) << " ";
 
      // Output a dummy pressure
      outfile << 0.0 << "\n";
    }
 
    write_tecplot_zone_footer(outfile, n_plot);
 
    outfile << "\n";
  }
 
 
  //===========================================================================
  /// Overload the output function
  //===========================================================================
  void FluidInterfaceElement::output(FILE* file_pt, const unsigned& n_plot)
  {
    const unsigned el_dim = this->dim();
    const unsigned n_dim = this->nodal_dimension();
    const unsigned n_velocity = this->U_index_interface.size();
    // Set output Vector
    Vector<double> s(el_dim);
 
    // Tecplot header info
    fprintf(file_pt, "%s", tecplot_zone_string(n_plot).c_str());
 
    // Loop over plot points
    unsigned num_plot_points = nplot_points(n_plot);
    for (unsigned iplot = 0; iplot < num_plot_points; iplot++)
    {
      // Get local coordinates of plot point
      get_s_plot(iplot, n_plot, s);
 
      // Coordinates
      for (unsigned i = 0; i < n_dim; i++)
      {
        fprintf(file_pt, "%g ", interpolated_x(s, i));
      }
 
      // Velocities
      for (unsigned i = 0; i < n_velocity; i++)
      {
        fprintf(file_pt, "%g ", interpolated_u(s, i));
      }
 
      // Dummy Pressure
      fprintf(file_pt, "%g \n", 0.0);
    }
    fprintf(file_pt, "\n");
 
    // Write tecplot footer (e.g. FE connectivity lists)
    write_tecplot_zone_footer(file_pt, n_plot);
  }
 
 
  /// //////////////////////////////////////////////////////////////////////
  /// //////////////////////////////////////////////////////////////////////
  /// //////////////////////////////////////////////////////////////////////
 
  //====================================================================
  /// Specialise the surface derivatives for the line interface case
  //===================================================================
  double LineDerivatives::compute_surface_derivatives(
    const Shape& psi,
    const DShape& dpsids,
    const DenseMatrix<double>& interpolated_t,
    const Vector<double>& interpolated_x,
    DShape& dpsidS,
    DShape& dpsidS_div)
  {
    const unsigned n_shape = psi.nindex1();
    const unsigned n_dim = 2;
 
    // Calculate the only entry of the surface
    // metric tensor (square length of the tangent vector)
    double a11 = interpolated_t(0, 0) * interpolated_t(0, 0) +
                 interpolated_t(0, 1) * interpolated_t(0, 1);
 
    // Now set the derivative terms of the shape functions
    for (unsigned l = 0; l < n_shape; l++)
    {
      for (unsigned i = 0; i < n_dim; i++)
      {
        dpsidS(l, i) = dpsids(l, 0) * interpolated_t(0, i) / a11;
      }
    }
 
    // The surface divergence is the same as the surface
    // gradient operator
    dpsidS_div = dpsidS;
 
    // Return the jacobian
    return sqrt(a11);
  }
 
 
  /// /////////////////////////////////////////////////////////////////////
  /// /////////////////////////////////////////////////////////////////////
  /// /////////////////////////////////////////////////////////////////////
 
  //====================================================================
  /// Specialise the surface derivatives for the axisymmetric interface case
  //===================================================================
  double AxisymmetricDerivatives::compute_surface_derivatives(
    const Shape& psi,
    const DShape& dpsids,
    const DenseMatrix<double>& interpolated_t,
    const Vector<double>& interpolated_x,
    DShape& dpsidS,
    DShape& dpsidS_div)
  {
    // Initially the same as the 2D case
    const unsigned n_shape = psi.nindex1();
    const unsigned n_dim = 2;
 
    // Calculate the only entry of the surface
    // metric tensor (square length of the tangent vector)
    double a11 = interpolated_t(0, 0) * interpolated_t(0, 0) +
                 interpolated_t(0, 1) * interpolated_t(0, 1);
 
    // Now set the derivative terms of the shape functions
    for (unsigned l = 0; l < n_shape; l++)
    {
      for (unsigned i = 0; i < n_dim; i++)
      {
        dpsidS(l, i) = dpsids(l, 0) * interpolated_t(0, i) / a11;
        // Set the standard components of the divergence
        dpsidS_div(l, i) = dpsidS(l, i);
      }
    }
 
    const double r = interpolated_x[0];
 
    // The surface divergence is different because we need
    // to take account of variation of the base vectors
    for (unsigned l = 0; l < n_shape; l++)
    {
      dpsidS_div(l, 0) += psi(l) / r;
    }
 
    // Return the jacobian, needs to be multiplied by r
    return r * sqrt(a11);
  }
 
 
  /// /////////////////////////////////////////////////////////////////////
  /// /////////////////////////////////////////////////////////////////////
  /// /////////////////////////////////////////////////////////////////////
 
  //====================================================================
  /// Specialise the surface derivatives for 2D surface case
  //===================================================================
  double SurfaceDerivatives::compute_surface_derivatives(
    const Shape& psi,
    const DShape& dpsids,
    const DenseMatrix<double>& interpolated_t,
    const Vector<double>& interpolated_x,
    DShape& dpsidS,
    DShape& dpsidS_div)
  {
    const unsigned n_shape = psi.nindex1();
    const unsigned n_dim = 3;
 
    // Calculate the local metric tensor
    // The dot product of the two tangent vectors
    double amet[2][2];
    for (unsigned al = 0; al < 2; al++)
    {
      for (unsigned be = 0; be < 2; be++)
      {
        // Initialise to zero
        amet[al][be] = 0.0;
        // Add the dot product contributions
        for (unsigned i = 0; i < n_dim; i++)
        {
          amet[al][be] += interpolated_t(al, i) * interpolated_t(be, i);
        }
      }
    }
 
    // Work out the determinant
    double det_a = amet[0][0] * amet[1][1] - amet[0][1] * amet[1][0];
    // Also work out the contravariant metric
    double aup[2][2];
    aup[0][0] = amet[1][1] / det_a;
    aup[0][1] = -amet[0][1] / det_a;
    aup[1][0] = -amet[1][0] / det_a;
    aup[1][1] = amet[0][0] / det_a;
 
 
    // Now construct the surface gradient terms
    for (unsigned l = 0; l < n_shape; l++)
    {
      // Do some pre-computation
      const double dpsi_temp[2] = {
        aup[0][0] * dpsids(l, 0) + aup[0][1] * dpsids(l, 1),
        aup[1][0] * dpsids(l, 0) + aup[1][1] * dpsids(l, 1)};
 
      for (unsigned i = 0; i < n_dim; i++)
      {
        dpsidS(l, i) = dpsi_temp[0] * interpolated_t(0, i) +
                       dpsi_temp[1] * interpolated_t(1, i);
      }
    }
 
    // The divergence operator is the same
    dpsidS_div = dpsidS;
 
    // Return the jacobian
    return sqrt(det_a);
  }
 
} // namespace oomph