unstructured_time_harmonic_elastic_annulus.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//====================================================================
// Time-harmonic deformation of an T-rib reinforced elastic annulus subject to 
// a nonuniform pressure load.
 
//Oomph-lib includes
#include "generic.h"
#include "time_harmonic_linear_elasticity.h"
 
//The meshes
#include "meshes/triangle_mesh.h"
 
using namespace std;
using namespace oomph;
 
/// ////////////////////////////////////////////////////////////////////
/// ////////////////////////////////////////////////////////////////////
// Straight line as geometric object
/// ////////////////////////////////////////////////////////////////////
/// ////////////////////////////////////////////////////////////////////
 
 
 
//=========================================================================
/// Straight 1D line in 2D space 
//=========================================================================
class MyStraightLine : public GeomObject
{
 
public:
 
 /// Constructor:  Pass start and end points
 MyStraightLine(const Vector<double>& r_start, const Vector<double>& r_end) 
  :  GeomObject(1,2), R_start(r_start), R_end(r_end)
  { }
 
 
 /// Broken copy constructor
 MyStraightLine(const MyStraightLine& dummy) 
  { 
   BrokenCopy::broken_copy("MyStraightLine");
  } 
 
 /// Broken assignment operator
 void operator=(const MyStraightLine&) 
  {
   BrokenCopy::broken_assign("MyStraightLine");
  }
 
 
 /// Destructor:  Empty
 ~MyStraightLine(){}
 
 /// Position Vector at Lagrangian coordinate zeta 
 void position(const Vector<double>& zeta, Vector<double>& r) const
  {
   // Position Vector
   r[0] = R_start[0]+(R_end[0]-R_start[0])*zeta[0];
   r[1] = R_start[1]+(R_end[1]-R_start[1])*zeta[0];
  }
 
private:
 
 /// Start point of line
 Vector<double> R_start;
 
 /// End point of line
 Vector<double> R_end;
 
};
 
 
 
/// ///////////////////////////////////////////////////////////////////
/// ///////////////////////////////////////////////////////////////////
/// ///////////////////////////////////////////////////////////////////
 
 
//=======start_namespace==========================================
/// Global variables
//================================================================
namespace Global_Parameters
{
 
 /// Poisson's ratio
 double Nu=0.3;
 
 /// Square of non-dim frequency 
 double Omega_sq=10.0; 
 
 /// Square of non-dim frequency for the two regions
 Vector<double> Omega_sq_region(2,Omega_sq);
  
 /// The elasticity tensors for the two regions
 Vector<TimeHarmonicIsotropicElasticityTensor*> E_pt;
 
 /// Thickness of annulus
 double H_annulus=0.1;
 
 /// Uniform pressure
 double P = 0.1;
 
 /// Peakiness parameter for pressure load
 double Alpha=200.0;
 
 /// Constant pressure load (real and imag part)
 void pressure_load(const Vector<double> &x,
                        const Vector<double> &n, 
                        Vector<std::complex<double> >&traction)
 {
  double phi=atan2(x[1],x[0]);
  double magnitude=exp(-Alpha*pow(phi-0.25*MathematicalConstants::Pi,2));
 
  unsigned dim = traction.size();
  for(unsigned i=0;i<dim;i++)
   {
    traction[i] = complex<double>(-magnitude*P*n[i],magnitude*P*n[i]);
   }
 } // end_of_pressure_load
 
 /// Output directory
 string Directory="RESLT";
 
} //end namespace
 
 
 
//=============begin_problem============================================ 
/// Annular disk
//====================================================================== 
template<class ELASTICITY_ELEMENT>
class RingWithTRibProblem : public Problem
{
 
public:
 
 /// Constructor:
 RingWithTRibProblem();
 
 /// Update function (empty)
 void actions_after_newton_solve() {}
 
 /// Update function (empty)
 void actions_before_newton_solve() {}
 
 /// Actions before adapt: Wipe the mesh of traction elements
 void actions_before_adapt();
 
 /// Actions after adapt: Rebuild the mesh of traction elements
 void actions_after_adapt();
 
 /// Doc the solution
 void doc_solution();
 
private:
 
 /// Create traction elements
 void create_traction_elements();
 
 /// Delete traction elements
 void delete_traction_elements();
 
 /// Helper function to complete problem setup
 void complete_problem_setup();
 
#ifdef ADAPTIVE
 
 /// Pointer to refineable solid mesh
 RefineableTriangleMesh<ELASTICITY_ELEMENT>* Solid_mesh_pt;
 
#else
 
 /// Pointer to solid mesh
 TriangleMesh<ELASTICITY_ELEMENT>* Solid_mesh_pt;
 
#endif
 
 /// Pointer to mesh of traction elements
 Mesh* Traction_mesh_pt;
 
 /// DocInfo object for output
 DocInfo Doc_info;
 
 /// Boundary ID of upper symmetry boundary
 unsigned Upper_symmetry_boundary_id;
 
 /// Boundary ID of lower symmetry boundary
 unsigned Lower_symmetry_boundary_id;
 
 /// Boundary ID of outer boundary
 unsigned Outer_boundary_id;
 
};
 
 
//===========start_of_constructor======================================= 
/// Constructor: 
//====================================================================== 
template<class ELASTICITY_ELEMENT>
RingWithTRibProblem<ELASTICITY_ELEMENT>::RingWithTRibProblem() 
{
 
 // Solid mesh
 //-----------
 
 // Start and end coordinates
 Vector<double> r_start(2);
 Vector<double> r_end(2);
 
 // Outer radius of hull
 double r_outer = 1.0;
 
 // Inner radius of hull
 double r_inner = r_outer-Global_Parameters::H_annulus;
 
 // Thickness of rib
 double rib_thick=0.05;
 
 // Depth of rib
 double rib_depth=0.2;
 
 // Total width of T
 double t_width=0.2;
 
 // Thickness of T
 double t_thick=0.05;
 
 // Half-opening angle of rib
 double half_phi_rib=asin(0.5*rib_thick/r_inner);
 
 // Pointer to the closed curve that defines the outer boundary
 TriangleMeshClosedCurve* closed_curve_pt=0;
 
 // Provide storage for pointers to the parts of the curvilinear boundary
 Vector<TriangleMeshCurveSection*> curvilinear_boundary_pt;
 
 // Outer boundary
 //---------------
 Ellipse* outer_boundary_circle_pt = new Ellipse(r_outer,r_outer);
 double zeta_start=-0.5*MathematicalConstants::Pi;
 double zeta_end=0.5*MathematicalConstants::Pi;
 unsigned nsegment=50;
 unsigned boundary_id=curvilinear_boundary_pt.size();
 curvilinear_boundary_pt.push_back(
  new TriangleMeshCurviLine(
   outer_boundary_circle_pt,zeta_start,zeta_end,nsegment,boundary_id));
 
 // Remember it
 Outer_boundary_id=boundary_id;
 
 
 // Upper straight line segment on symmetry axis
 //---------------------------------------------
 r_start[0]=0.0;
 r_start[1]=r_outer;
 r_end[0]=0.0;
 r_end[1]=r_inner;
 MyStraightLine* upper_sym_pt = new MyStraightLine(r_start,r_end);
 zeta_start=0.0;
 zeta_end=1.0;
 nsegment=1;
 boundary_id=curvilinear_boundary_pt.size();
 curvilinear_boundary_pt.push_back(
  new TriangleMeshCurviLine(
   upper_sym_pt,zeta_start,zeta_end,nsegment,boundary_id));
                                                        
 // Remember it
 Upper_symmetry_boundary_id=boundary_id;
 
 // Upper part of inner boundary
 //-----------------------------
 Ellipse* upper_inner_boundary_pt = 
  new Ellipse(r_inner,r_inner);
 zeta_start=0.5*MathematicalConstants::Pi;
 zeta_end=half_phi_rib;
 nsegment=20;
 boundary_id=curvilinear_boundary_pt.size();
 curvilinear_boundary_pt.push_back(
  new TriangleMeshCurviLine(
   upper_inner_boundary_pt,
   zeta_start,zeta_end,nsegment,boundary_id));
 
 // Upper half of inward rib
 //-------------------------
 r_start[0]=r_inner*cos(half_phi_rib);
 r_start[1]=r_inner*sin(half_phi_rib);
 r_end[0]=r_start[0]-rib_depth;
 r_end[1]=r_start[1];
 MyStraightLine* upper_inward_rib_pt = new MyStraightLine(r_start,r_end);
 zeta_start=0.0;
 zeta_end=1.0;
 nsegment=1;
 boundary_id=curvilinear_boundary_pt.size();
 TriangleMeshCurviLine* upper_inward_rib_curviline_pt=
  new TriangleMeshCurviLine(
   upper_inward_rib_pt,zeta_start,zeta_end,nsegment,boundary_id);
 curvilinear_boundary_pt.push_back(upper_inward_rib_curviline_pt);
 
 // Vertical upper bit of T
 //------------------------
 r_start[0]=r_end[0];
 r_start[1]=r_end[1];
 r_end[0]=r_start[0];
 r_end[1]=r_start[1]+0.5*(t_width-rib_thick);
 MyStraightLine* vertical_upper_t_rib_pt = new MyStraightLine(r_start,r_end);
 zeta_start=0.0;
 zeta_end=1.0;
 nsegment=1;
 boundary_id=curvilinear_boundary_pt.size();
 curvilinear_boundary_pt.push_back(
  new TriangleMeshCurviLine(
   vertical_upper_t_rib_pt,zeta_start,zeta_end,nsegment,boundary_id));
 
 
 // Horizontal upper bit of T
 //-----------==-------------
 r_start[0]=r_end[0];
 r_start[1]=r_end[1];
 r_end[0]=r_start[0]-t_thick;
 r_end[1]=r_start[1];
 MyStraightLine* horizontal_upper_t_rib_pt = new MyStraightLine(r_start,r_end);
 zeta_start=0.0;
 zeta_end=1.0;
 nsegment=1;
 boundary_id=curvilinear_boundary_pt.size();
 curvilinear_boundary_pt.push_back(
  new TriangleMeshCurviLine(
   horizontal_upper_t_rib_pt,zeta_start,zeta_end,nsegment,boundary_id));
 
 // Vertical end of rib end
 //------------------------
 r_start[0]=r_end[0];
 r_start[1]=r_end[1];
 r_end[0]=r_start[0];
 r_end[1]=-r_start[1];
 MyStraightLine* inner_vertical_rib_pt = new MyStraightLine(r_start,r_end);
 zeta_start=0.0;
 zeta_end=1.0;
 nsegment=1;
 boundary_id=curvilinear_boundary_pt.size();
 curvilinear_boundary_pt.push_back(
  new TriangleMeshCurviLine(
   inner_vertical_rib_pt,zeta_start,zeta_end,nsegment,boundary_id));
 
 
 // Horizontal lower bit of T
 //-----------==-------------
 r_start[0]=r_end[0];
 r_start[1]=r_end[1];
 r_end[0]=r_start[0]+t_thick;
 r_end[1]=r_start[1];
 MyStraightLine* horizontal_lower_t_rib_pt = new MyStraightLine(r_start,r_end);
 zeta_start=0.0;
 zeta_end=1.0;
 nsegment=1;
 boundary_id=curvilinear_boundary_pt.size();
 curvilinear_boundary_pt.push_back(
  new TriangleMeshCurviLine(
   horizontal_lower_t_rib_pt,zeta_start,zeta_end,nsegment,boundary_id));
 
 
 // Vertical lower bit of T
 //------------------------
 r_start[0]=r_end[0];
 r_start[1]=r_end[1];
 r_end[0]=r_start[0];
 r_end[1]=r_start[1]+0.5*(t_width-rib_thick);
 MyStraightLine* vertical_lower_t_rib_pt = new MyStraightLine(r_start,r_end);
 zeta_start=0.0;
 zeta_end=1.0;
 nsegment=1;
 boundary_id=curvilinear_boundary_pt.size();
 curvilinear_boundary_pt.push_back(
  new TriangleMeshCurviLine(
   vertical_lower_t_rib_pt,zeta_start,zeta_end,nsegment,boundary_id));
 
 
 // Lower half of inward rib
 //-------------------------
 r_end[0]=r_inner*cos(half_phi_rib);
 r_end[1]=-r_inner*sin(half_phi_rib);
 r_start[0]=r_end[0]-rib_depth;
 r_start[1]=r_end[1];
 MyStraightLine* lower_inward_rib_pt = new MyStraightLine(r_start,r_end);
 zeta_start=0.0;
 zeta_end=1.0;
 nsegment=1;
 boundary_id=curvilinear_boundary_pt.size();
 TriangleMeshCurviLine* lower_inward_rib_curviline_pt=
  new TriangleMeshCurviLine(
   lower_inward_rib_pt,zeta_start,zeta_end,nsegment,boundary_id);
 curvilinear_boundary_pt.push_back(lower_inward_rib_curviline_pt);
 
 
 // Lower part of inner boundary
 //-----------------------------
 Ellipse* lower_inner_boundary_circle_pt = new Ellipse(r_inner,r_inner);
 zeta_start=-half_phi_rib;
 zeta_end=-0.5*MathematicalConstants::Pi;
 nsegment=20;
 boundary_id=curvilinear_boundary_pt.size();
 curvilinear_boundary_pt.push_back(
  new TriangleMeshCurviLine(
   lower_inner_boundary_circle_pt,zeta_start,zeta_end,nsegment,boundary_id));
 
 
 // Lower straight line segment on symmetry axis
 //---------------------------------------------
 r_start[0]=0.0;
 r_start[1]=-r_inner;
 r_end[0]=0.0;
 r_end[1]=-r_outer;
 MyStraightLine* lower_sym_pt = new MyStraightLine(r_start,r_end);
 zeta_start=0.0;
 zeta_end=1.0;
 nsegment=1;
 boundary_id=curvilinear_boundary_pt.size();
 curvilinear_boundary_pt.push_back(
  new TriangleMeshCurviLine(
   lower_sym_pt,zeta_start,zeta_end,nsegment,boundary_id));
      
 // Remember it
 Lower_symmetry_boundary_id=boundary_id;
 
 // Combine to curvilinear boundary
 //--------------------------------
 closed_curve_pt=
  new TriangleMeshClosedCurve(curvilinear_boundary_pt); 
 
  // Vertical dividing line across base of T-rib
 //--------------------------------------------
 Vector<TriangleMeshCurveSection*> internal_polyline_pt(1);
 r_start[0]=r_inner*cos(half_phi_rib);
 r_start[1]=r_inner*sin(half_phi_rib);
 r_end[0]=r_inner*cos(half_phi_rib);
 r_end[1]=-r_inner*sin(half_phi_rib);
 
 Vector<Vector<double> > boundary_vertices(2);
 boundary_vertices[0]=r_start;
 boundary_vertices[1]=r_end;
 boundary_id=100;
 TriangleMeshPolyLine* rib_divider_pt=
  new TriangleMeshPolyLine(boundary_vertices,boundary_id); 
 internal_polyline_pt[0]=rib_divider_pt;
 
 // Make connection
 double s_connect=0.0;
 internal_polyline_pt[0]->connect_initial_vertex_to_curviline(
  upper_inward_rib_curviline_pt,s_connect);
 
 // Make connection
 s_connect=1.0;
 internal_polyline_pt[0]->connect_final_vertex_to_curviline(
  lower_inward_rib_curviline_pt,s_connect);
 
 // Create open curve that defines internal bondary
 Vector<TriangleMeshOpenCurve*> inner_boundary_pt;
 inner_boundary_pt.push_back(new TriangleMeshOpenCurve(internal_polyline_pt));
 
 // Define coordinates of a point inside the rib
 Vector<double> rib_center(2);
 rib_center[0]=r_inner-rib_depth;
 rib_center[1]=0.0;
 
 // Now build the mesh
 //===================
 
 
 // Use the TriangleMeshParameters object for helping on the manage of the
 // TriangleMesh parameters. The only parameter that needs to take is the
 // outer boundary.
 TriangleMeshParameters triangle_mesh_parameters(closed_curve_pt);
 
 // Target area
 triangle_mesh_parameters.element_area()=0.2;
 
 // Specify the internal open boundary
 triangle_mesh_parameters.internal_open_curves_pt()=inner_boundary_pt;
 
 // Define the region
 triangle_mesh_parameters.add_region_coordinates(1,rib_center);
 
#ifdef ADAPTIVE
 
 // Build the mesh
 Solid_mesh_pt=new 
  RefineableTriangleMesh<ELASTICITY_ELEMENT>(triangle_mesh_parameters);
 
 // Set error estimator
 Solid_mesh_pt->spatial_error_estimator_pt()=new Z2ErrorEstimator;
 
#else
 
 // Build the mesh
 Solid_mesh_pt=new 
  TriangleMesh<ELASTICITY_ELEMENT>(triangle_mesh_parameters);
 
#endif
 
 
 // Let's have a look where the boundaries are
 Solid_mesh_pt->output("solid_mesh.dat");
 Solid_mesh_pt->output_boundaries("solid_mesh_boundary.dat");
 
 // Construct the traction element mesh
 Traction_mesh_pt=new Mesh;
 create_traction_elements(); 
 
 // Solid mesh is first sub-mesh
 add_sub_mesh(Solid_mesh_pt);
 
 // Add traction sub-mesh
 add_sub_mesh(Traction_mesh_pt);
 
 // Build combined "global" mesh
 build_global_mesh();
 
 // Create elasticity tensors
 Global_Parameters::E_pt.resize(2);
 Global_Parameters::E_pt[0]=new TimeHarmonicIsotropicElasticityTensor(
    Global_Parameters::Nu);
 Global_Parameters::E_pt[1]=new TimeHarmonicIsotropicElasticityTensor(
  Global_Parameters::Nu);
 
 // Complete problem setup
 complete_problem_setup();
 
 //Assign equation numbers
 cout << assign_eqn_numbers() << std::endl; 
 
 // Set output directory
 Doc_info.set_directory(Global_Parameters::Directory);
 
} //end_of_constructor
 
 
 
 
//=====================start_of_complete_problem_setup====================
/// Complete problem setup
//========================================================================
template<class ELASTICITY_ELEMENT>
void RingWithTRibProblem<ELASTICITY_ELEMENT>::complete_problem_setup()
{
 
#ifdef ADAPTIVE
 
 // Min element size allowed during adaptation
 if (!CommandLineArgs::command_line_flag_has_been_set("--validation"))
  {   
   Solid_mesh_pt->min_element_size()=1.0e-5;
  }
 
#endif
 
 //Assign the physical properties to the elements
 //----------------------------------------------
 unsigned nreg=Solid_mesh_pt->nregion();
 for (unsigned r=0;r<nreg;r++)
  {
   unsigned nel=Solid_mesh_pt->nregion_element(r);
   for (unsigned e=0;e<nel;e++)
    {     
     //Cast to a solid element
     ELASTICITY_ELEMENT *el_pt = 
      dynamic_cast<ELASTICITY_ELEMENT*>(Solid_mesh_pt->region_element_pt(r,e));
 
     // Set the constitutive law
     el_pt->elasticity_tensor_pt() = Global_Parameters::E_pt[r];
 
     // Square of non-dim frequency
     el_pt->omega_sq_pt()= &Global_Parameters::Omega_sq_region[r];
    }
  }                         
 
 
 // Solid boundary conditions:
 //---------------------------
 // Pin real and imag part of horizontal displacement components 
 //-------------------------------------------------------------
 // on vertical boundaries
 //-----------------------
 {  
  //Loop over the nodes to pin and assign boundary displacements on 
  //solid boundary
  unsigned n_node = Solid_mesh_pt->nboundary_node(Upper_symmetry_boundary_id);
  for(unsigned i=0;i<n_node;i++)
   {
    Node* nod_pt=Solid_mesh_pt->boundary_node_pt(Upper_symmetry_boundary_id,i);
    
    // Real part of x-displacement 
    nod_pt->pin(0);
    nod_pt->set_value(0,0.0);
    
    // Imag part of x-displacement
    nod_pt->pin(2);
    nod_pt->set_value(2,0.0);
   }
 }
 {
  //Loop over the nodes to pin and assign boundary displacements on 
  //solid boundary
  unsigned n_node = Solid_mesh_pt->nboundary_node(Lower_symmetry_boundary_id);
  for(unsigned i=0;i<n_node;i++)
   {
    Node* nod_pt=Solid_mesh_pt->boundary_node_pt(Lower_symmetry_boundary_id,i);
 
    // Real part of x-displacement 
    nod_pt->pin(0);
    nod_pt->set_value(0,0.0);
    
    // Imag part of x-displacement
    nod_pt->pin(2);
    nod_pt->set_value(2,0.0);
   }
 }
}
 
 
 
//=====================start_of_actions_before_adapt======================
/// Actions before adapt: Wipe the mesh of traction elements
//========================================================================
template<class ELASTICITY_ELEMENT>
void RingWithTRibProblem<ELASTICITY_ELEMENT>::actions_before_adapt()
{
 // Kill the traction elements and wipe surface mesh
 delete_traction_elements();
 
 // Rebuild the Problem's global mesh from its various sub-meshes
 rebuild_global_mesh();
 
}// end of actions_before_adapt
 
 
 
//=====================start_of_actions_after_adapt=======================
///  Actions after adapt: Rebuild the mesh of traction elements
//========================================================================
template<class ELASTICITY_ELEMENT>
void RingWithTRibProblem<ELASTICITY_ELEMENT>::actions_after_adapt()
{
 // Create traction elements from all elements that are 
 // adjacent to FSI boundaries and add them to surface meshes
 create_traction_elements();
 
 // Rebuild the Problem's global mesh from its various sub-meshes
 rebuild_global_mesh();
 
 // Complete problem setup
 complete_problem_setup();   
 
}// end of actions_after_adapt
 
 
//============start_of_create_traction_elements==============================
/// Create traction elements 
//=======================================================================
template<class ELASTICITY_ELEMENT>
void RingWithTRibProblem<ELASTICITY_ELEMENT>::create_traction_elements()
{
 
 unsigned b=Outer_boundary_id;
 {
  // How many bulk elements are adjacent to boundary b?
  unsigned n_element = Solid_mesh_pt->nboundary_element(b);
   
  // Loop over the bulk elements adjacent to boundary b
  for(unsigned e=0;e<n_element;e++)
   {
    // Get pointer to the bulk element that is adjacent to boundary b
    ELASTICITY_ELEMENT* bulk_elem_pt = dynamic_cast<ELASTICITY_ELEMENT*>(
     Solid_mesh_pt->boundary_element_pt(b,e));
    
    //Find the index of the face of element e along boundary b
    int face_index = Solid_mesh_pt->face_index_at_boundary(b,e);
    
    // Create element
    TimeHarmonicLinearElasticityTractionElement<ELASTICITY_ELEMENT>* el_pt=
     new TimeHarmonicLinearElasticityTractionElement<ELASTICITY_ELEMENT>
     (bulk_elem_pt,face_index);   
    
    // Add to mesh
    Traction_mesh_pt->add_element_pt(el_pt);
    
    // Associate element with bulk boundary (to allow it to access
    // the boundary coordinates in the bulk mesh)
    el_pt->set_boundary_number_in_bulk_mesh(b); 
    
    //Set the traction function
    el_pt->traction_fct_pt() = Global_Parameters::pressure_load;
    
   }
 }
 
} // end_of_create_traction_elements
 
 
 
 
//============start_of_delete_traction_elements==============================
/// Delete traction elements and wipe the  traction meshes
//=======================================================================
template<class ELASTICITY_ELEMENT>
void RingWithTRibProblem<ELASTICITY_ELEMENT>::delete_traction_elements()
{
 // How many surface elements are in the surface mesh
 unsigned n_element = Traction_mesh_pt->nelement();
 
 // Loop over the surface elements
 for(unsigned e=0;e<n_element;e++)
  {
   // Kill surface element
   delete Traction_mesh_pt->element_pt(e);
  }
 
 // Wipe the mesh
 Traction_mesh_pt->flush_element_and_node_storage();
 
} // end of delete_traction_elements
 
 
 
 
 
//==============start_doc===========================================
/// Doc the solution
//==================================================================
template<class ELASTICITY_ELEMENT>
void RingWithTRibProblem<ELASTICITY_ELEMENT>::doc_solution()
{
 
 ofstream some_file;
 char filename[100];
 
 // Number of plot points
 unsigned n_plot=5; 
 
 // Output displacement field
 //--------------------------
 sprintf(filename,"%s/elast_soln%i.dat",Doc_info.directory().c_str(),
         Doc_info.number());
 some_file.open(filename);
 Solid_mesh_pt->output(some_file,n_plot);
 some_file.close();
 
 // Output traction elements
 //-------------------------
 sprintf(filename,"%s/traction_soln%i.dat",Doc_info.directory().c_str(),
         Doc_info.number());
 some_file.open(filename);
 Traction_mesh_pt->output(some_file,n_plot);
 some_file.close();
 
 // Output regions
 //---------------
 unsigned nreg=Solid_mesh_pt->nregion();
 for (unsigned r=0;r<nreg;r++)
  {
   sprintf(filename,"%s/region%i_%i.dat",Doc_info.directory().c_str(),
           r,Doc_info.number());   
   some_file.open(filename);   
   unsigned nel=Solid_mesh_pt->nregion_element(r);
   for (unsigned e=0;e<nel;e++)
    {     
     FiniteElement* el_pt=Solid_mesh_pt->region_element_pt(r,e);
     el_pt->output(some_file,n_plot);
    }
   some_file.close();
  }
 
 // Output norm of solution (to allow validation of solution even
 // if triangle generates a slightly different mesh)
 sprintf(filename,"%s/norm%i.dat",Doc_info.directory().c_str(),
         Doc_info.number());   
 some_file.open(filename);   
 double norm=0.0;
 unsigned nel=Solid_mesh_pt->nelement();
 for (unsigned e=0;e<nel;e++)
  {
   double el_norm=0.0;
   Solid_mesh_pt->compute_norm(el_norm);
   norm+=el_norm;
  }
 some_file << norm << std::endl;
 
 // Increment label for output files
 Doc_info.number()++;
 
} //end doc
 
 
 
//=======start_of_main==================================================
/// Driver for annular disk loaded by pressure
//======================================================================
int main(int argc, char **argv)
{
 
 // Store command line arguments
 CommandLineArgs::setup(argc,argv);
 
 // Define possible command line arguments and parse the ones that
 // were actually specified 
  
#ifdef ADAPTIVE
 
 // Max. number of adaptations
 unsigned max_adapt=3;
 CommandLineArgs::specify_command_line_flag("--max_adapt",&max_adapt);
 
#endif
 
 // Peakiness parameter for loading
 CommandLineArgs::specify_command_line_flag("--alpha",
                                            &Global_Parameters::Alpha);
 
 // Validation run?
 CommandLineArgs::specify_command_line_flag("--validation");
 
 // Parse command line
 CommandLineArgs::parse_and_assign(); 
 
 // Doc what has actually been specified on the command line
 CommandLineArgs::doc_specified_flags();
 
#ifdef ADAPTIVE
 
 //Set up the problem
 RingWithTRibProblem<ProjectableTimeHarmonicLinearElasticityElement
                    <TTimeHarmonicLinearElasticityElement<2,3> > >
  problem;
 
#else
 
 //Set up the problem
 RingWithTRibProblem<TTimeHarmonicLinearElasticityElement<2,3> > problem;
 
#endif
 
 
 // Initial values for parameter values
 Global_Parameters::P=0.1; 
 
 //Parameter incrementation
 unsigned nstep=2;
 for(unsigned i=0;i<nstep;i++)
  {
 
#ifdef ADAPTIVE
 
   // Solve the problem with Newton's method, allowing
   // up to max_adapt mesh adaptations after every solve.
   problem.newton_solve(max_adapt);
 
#else
 
   // Solve the problem using Newton's method
   problem.newton_solve();
 
#endif
   
   // Doc solution
   problem.doc_solution();
   
   // Now reduce the stiffness of the rib and set its inertia to
   // zero, then re-solve. Resulting displacement field should
   // be approximately axisymmetric in the annular region.
   Global_Parameters::E_pt[1]->update_constitutive_parameters(
    Global_Parameters::Nu,1.0e-10);
   Global_Parameters::Omega_sq_region[1]=0.0;
 
  }
 
} //end of main