disk_compression.cc
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25 //LIC//====================================================================
26 //Driver function for a simple test elasticity problem: the
27 //compression of an axisymmetric disk. We also demonstrate how
28 //to incorporate isotropic growth into the model and how to
29 //switch between different constitutive equations.
30 #include <iostream>
31 #include <fstream>
32 #include <cmath>
33 
34 //My own includes
35 #include "generic.h"
36 #include "solid.h"
37 
38 //Need to instantiate templated mesh
39 #include "meshes/quarter_circle_sector_mesh.h"
40 
41 using namespace std;
42 
43 using namespace oomph;
44 
45 
46 //============namespace_for_problem_parameters=====================
47 /// Global variables
48 //=================================================================
50 {
51  /// Pointer to strain energy function
52  StrainEnergyFunction* Strain_energy_function_pt;
53 
54  /// Pointer to constitutive law
55  ConstitutiveLaw* Constitutive_law_pt;
56 
57  /// Elastic modulus
58  double E=1.0;
59 
60  /// Poisson's ratio
61  double Nu=0.3;
62 
63  /// "Mooney Rivlin" coefficient for generalised Mooney Rivlin law
64  double C1=1.3;
65 
66  /// Uniform pressure
67  double P = 0.0;
68 
69  /// Constant pressure load
70  void constant_pressure(const Vector<double> &xi,const Vector<double> &x,
71  const Vector<double> &n, Vector<double> &traction)
72  {
73  unsigned dim = traction.size();
74  for(unsigned i=0;i<dim;i++)
75  {
76  traction[i] = -P*n[i];
77  }
78  } // end of pressure load
79 
80 
81  /// Uniform volumetric expansion
82  double Uniform_gamma=1.1;
83 
84  /// Growth function
85  void growth_function(const Vector<double>& xi, double& gamma)
86  {
87  gamma = Uniform_gamma;
88  }
89 
90 } // end namespace
91 
92 
93 /// ////////////////////////////////////////////////////////////////////
94 /// ////////////////////////////////////////////////////////////////////
95 /// ////////////////////////////////////////////////////////////////////
96 
97 
98 
99 //==========start_mesh=================================================
100 /// Elastic quarter circle sector mesh with functionality to
101 /// attach traction elements to the curved surface. We "upgrade"
102 /// the RefineableQuarterCircleSectorMesh to become an
103 /// SolidMesh and equate the Eulerian and Lagrangian coordinates,
104 /// thus making the domain represented by the mesh the stress-free
105 /// configuration.
106 /// \n\n
107 /// The member function \c make_traction_element_mesh() creates
108 /// a separate mesh of SolidTractionElements that are attached to the
109 /// mesh's curved boundary (boundary 1).
110 //=====================================================================
111 template <class ELEMENT>
113  public virtual RefineableQuarterCircleSectorMesh<ELEMENT>,
114  public virtual SolidMesh
115 {
116 
117 
118 public:
119 
120  /// Constructor: Build mesh and copy Eulerian coords to Lagrangian
121  /// ones so that the initial configuration is the stress-free one.
123  const double& xi_lo,
124  const double& fract_mid,
125  const double& xi_hi,
126  TimeStepper* time_stepper_pt=
127  &Mesh::Default_TimeStepper) :
128  RefineableQuarterCircleSectorMesh<ELEMENT>(wall_pt,xi_lo,fract_mid,xi_hi,
129  time_stepper_pt)
130  {
131  /// Make the current configuration the undeformed one by
132  /// setting the nodal Lagrangian coordinates to their current
133  /// Eulerian ones
134  set_lagrangian_nodal_coordinates();
135  }
136 
137 
138  /// Function to create mesh made of traction elements
139  void make_traction_element_mesh(SolidMesh*& traction_mesh_pt)
140  {
141 
142  // Make new mesh
143  traction_mesh_pt = new SolidMesh;
144 
145  // Loop over all elements on boundary 1:
146  unsigned b=1;
147  unsigned n_element = this->nboundary_element(b);
148  for (unsigned e=0;e<n_element;e++)
149  {
150  // The element itself:
151  FiniteElement* fe_pt = this->boundary_element_pt(b,e);
152 
153  // Find the index of the face of element e along boundary b
154  int face_index = this->face_index_at_boundary(b,e);
155 
156  // Create new element
157  traction_mesh_pt->add_element_pt(new SolidTractionElement<ELEMENT>
158  (fe_pt,face_index));
159  }
160  }
161 
162 };
163 
164 
165 //======================================================================
166 /// Uniform compression of a circular disk in a state of plane strain,
167 /// subject to uniform growth.
168 //======================================================================
169 template<class ELEMENT>
170 class StaticDiskCompressionProblem : public Problem
171 {
172 
173 public:
174 
175  /// Constructor:
177 
178  /// Run simulation: Pass case number to label output files
179  void parameter_study(const unsigned& case_number);
180 
181  /// Doc the solution
182  void doc_solution(DocInfo& doc_info);
183 
184  /// Update function (empty)
186 
187  /// Update function (empty)
189 
190 private:
191 
192  /// Trace file
193  ofstream Trace_file;
194 
195  /// Vector of pointers to nodes whose position we're tracing
196  Vector<Node*> Trace_node_pt;
197 
198  /// Pointer to solid mesh
200 
201  /// Pointer to mesh of traction elements
202  SolidMesh* Traction_mesh_pt;
203 
204 };
205 
206 //======================================================================
207 /// Constructor:
208 //======================================================================
209 template<class ELEMENT>
211 {
212  // Build the geometric object that describes the curvilinear
213  // boundary of the quarter circle domain
214  Ellipse* curved_boundary_pt = new Ellipse(1.0,1.0);
215 
216  // The curved boundary of the mesh is defined by the geometric object
217  // What follows are the start and end coordinates on the geometric object:
218  double xi_lo=0.0;
219  double xi_hi=2.0*atan(1.0);
220 
221  // Fraction along geometric object at which the radial dividing line
222  // is placed
223  double fract_mid=0.5;
224 
225  //Now create the mesh using the geometric object
227  curved_boundary_pt,xi_lo,fract_mid,xi_hi);
228 
229  // Setup trace nodes as the nodes on boundary 1 (=curved boundary)
230  // in the original mesh.
231  unsigned n_boundary_node = Solid_mesh_pt->nboundary_node(1);
232  Trace_node_pt.resize(n_boundary_node);
233  for(unsigned j=0;j<n_boundary_node;j++)
234  {Trace_node_pt[j]=Solid_mesh_pt->boundary_node_pt(1,j);}
235 
236  // Refine the mesh uniformly
237  Solid_mesh_pt->refine_uniformly();
238 
239  // Now construct the traction element mesh
240  Solid_mesh_pt->make_traction_element_mesh(Traction_mesh_pt);
241 
242  // Solid mesh is first sub-mesh
243  add_sub_mesh(Solid_mesh_pt);
244 
245  // Traction mesh is second sub-mesh
246  add_sub_mesh(Traction_mesh_pt);
247 
248  // Build combined "global" mesh
249  build_global_mesh();
250 
251 
252  // Pin the left edge in the horizontal direction
253  unsigned n_side = mesh_pt()->nboundary_node(2);
254  for(unsigned i=0;i<n_side;i++)
255  {Solid_mesh_pt->boundary_node_pt(2,i)->pin_position(0);}
256 
257  // Pin the bottom in the vertical direction
258  unsigned n_bottom = mesh_pt()->nboundary_node(0);
259  for(unsigned i=0;i<n_bottom;i++)
260  {Solid_mesh_pt->boundary_node_pt(0,i)->pin_position(1);}
261 
262  // Pin the redundant solid pressures (if any)
263  PVDEquationsBase<2>::pin_redundant_nodal_solid_pressures(
264  Solid_mesh_pt->element_pt());
265 
266  //Complete the build process for elements in "bulk" solid mesh
267  unsigned n_element =Solid_mesh_pt->nelement();
268  for(unsigned i=0;i<n_element;i++)
269  {
270  //Cast to a solid element
271  ELEMENT *el_pt = dynamic_cast<ELEMENT*>(Solid_mesh_pt->element_pt(i));
272 
273  // Set the constitutive law
274  el_pt->constitutive_law_pt() =
276 
277  // Set the isotropic growth function pointer
278  el_pt->isotropic_growth_fct_pt()=Global_Physical_Variables::growth_function;
279  }
280 
281  // Complete build process for SolidTractionElements
282  n_element=Traction_mesh_pt->nelement();
283  for(unsigned i=0;i<n_element;i++)
284  {
285  //Cast to a solid traction element
286  SolidTractionElement<ELEMENT> *el_pt =
287  dynamic_cast<SolidTractionElement<ELEMENT>*>
288  (Traction_mesh_pt->element_pt(i));
289 
290  //Set the traction function
291  el_pt->traction_fct_pt() = Global_Physical_Variables::constant_pressure;
292  }
293 
294  //Set up equation numbering scheme
295  cout << "Number of equations: " << assign_eqn_numbers() << std::endl;
296 }
297 
298 
299 //==================================================================
300 /// Doc the solution
301 //==================================================================
302 template<class ELEMENT>
304 {
305 
306  ofstream some_file;
307  char filename[100];
308 
309  // Number of plot points
310  unsigned npts = 5;
311 
312  // Output shape of deformed body
313  sprintf(filename,"%s/soln%i.dat",doc_info.directory().c_str(),
314  doc_info.number());
315  some_file.open(filename);
316  Solid_mesh_pt->output(some_file,npts);
317  some_file.close();
318 
319  //Find number of solid elements
320  unsigned nelement = Solid_mesh_pt->nelement();
321 
322  // Work out volume
323  double volume = 0.0;
324  for(unsigned e=0;e<nelement;e++)
325  {volume+= Solid_mesh_pt->finite_element_pt(e)->size();}
326 
327  // Exact outer radius for linear elasticity
329  double exact_r=sqrt(Global_Physical_Variables::Uniform_gamma)*
331  *((1.0+nu)*(1.0-2.0*nu)));
332 
333 
334  // Write trace file: Problem parameters
335  Trace_file << Global_Physical_Variables::P << " "
337  << volume << " "
338  << exact_r << " ";
339 
340  // Write radii of trace nodes
341  unsigned ntrace_node=Trace_node_pt.size();
342  for (unsigned j=0;j<ntrace_node;j++)
343  {
344  Trace_file << sqrt(pow(Trace_node_pt[j]->x(0),2)+
345  pow(Trace_node_pt[j]->x(1),2)) << " ";
346  }
347  Trace_file << std::endl;
348 
349 } // end of doc_solution
350 
351 
352 //==================================================================
353 /// Run the paramter study
354 //==================================================================
355 template<class ELEMENT>
357  const unsigned& case_number)
358 {
359  // Output
360  DocInfo doc_info;
361 
362  char dirname[100];
363  sprintf(dirname,"RESLT%i",case_number);
364 
365  // Set output directory
366  doc_info.set_directory(dirname);
367 
368  // Step number
369  doc_info.number()=0;
370 
371  // Open trace file
372  char filename[100];
373  sprintf(filename,"%s/trace.dat",doc_info.directory().c_str());
374  Trace_file.open(filename);
375 
376  //Parameter incrementation
377  double delta_p=0.0125;
378  unsigned nstep=21;
379 
380  // Perform fewer steps if run as self-test (indicated by nonzero number
381  // of command line arguments)
382  if (CommandLineArgs::Argc!=1)
383  {
384  nstep=3;
385  }
386 
387  // Offset external pressure so that the computation sweeps
388  // over a range of positive and negative pressures
389  Global_Physical_Variables::P =-delta_p*double(nstep-1)*0.5;
390 
391  // Do the parameter study
392  for(unsigned i=0;i<nstep;i++)
393  {
394  //Solve the problem for current load
395  newton_solve();
396 
397  // Doc solution
398  doc_solution(doc_info);
399  doc_info.number()++;
400 
401  // Increment pressure load
402  Global_Physical_Variables::P += delta_p;
403  }
404 
405 } // end of parameter study
406 
407 
408 //=====start_of_main====================================================
409 /// Driver code for disk-compression
410 //======================================================================
411 int main(int argc, char* argv[])
412 {
413 
414  // Store command line arguments
415  CommandLineArgs::setup(argc,argv);
416 
417  // Define a strain energy function: Generalised Mooney Rivlin
419  new GeneralisedMooneyRivlin(&Global_Physical_Variables::Nu,
422 
423  // Define a constitutive law (based on strain energy function)
425  new IsotropicStrainEnergyFunctionConstitutiveLaw(
427 
428  // Case 0: No pressure, generalised Mooney Rivlin
429  //-----------------------------------------------
430  {
431  //Set up the problem
433 
434  cout << "gen. M.R.: RefineableQPVDElement<2,3>" << std::endl;
435 
436  //Run the simulation
437  problem.parameter_study(0);
438 
439  } // done case 0
440 
441 
442  // Case 1: Continuous pressure formulation with generalised Mooney Rivlin
443  //------------------------------------------------------------------------
444  {
445  //Set up the problem
447  RefineableQPVDElementWithContinuousPressure<2> > problem;
448 
449  cout << "gen. M.R.: RefineableQPVDElementWithContinuousPressure<2> "
450  << std::endl;
451 
452  //Run the simulation
453  problem.parameter_study(1);
454 
455  } // done case 1
456 
457 
458 
459  // Case 2: Discontinuous pressure formulation with generalised Mooney Rivlin
460  //--------------------------------------------------------------------------
461  {
462  //Set up the problem
464  problem;
465 
466  cout << "gen. M.R.: RefineableQPVDElementWithPressure<2>" << std::endl;
467 
468  //Run the simulation
469  problem.parameter_study(2);
470 
471  } // done case 2
472 
473 
474  // Change the consitutive law: Delete the old one
476 
477  // Create oomph-lib's generalised Hooke's law constitutive equation
479  new GeneralisedHookean(&Global_Physical_Variables::Nu,
481 
482  // Case 3: No pressure, generalised Hooke's law
483  //----------------------------------------------
484  {
485  //Set up the problem
487 
488  cout << "gen. Hooke: RefineableQPVDElement<2,3> " << std::endl;
489 
490  //Run the simulation
491  problem.parameter_study(3);
492 
493  } // done case 3
494 
495  // Case 4: Continuous pressure formulation with generalised Hooke's law
496  //---------------------------------------------------------------------
497  {
498 
499  //Set up the problem
501  RefineableQPVDElementWithContinuousPressure<2> > problem;
502 
503  cout << "gen. Hooke: RefineableQPVDElementWithContinuousPressure<2> "
504  << std::endl;
505 
506  //Run the simulation
507  problem.parameter_study(4);
508 
509  } // done case 4
510 
511 
512  // Case 5: Discontinous pressure formulation with generalised Hooke's law
513  //------------------------------------------------------------------------
514  {
515 
516  //Set up the problem
518 
519  cout << "gen. Hooke: RefineableQPVDElementWithPressure<2> " << std::endl;
520 
521  //Run the simulation
522  problem.parameter_study(5);
523 
524  } // done case 5
525 
526  // Clean up
529 
530 } // end of main
531 
532 
533 
534 
535 
536 
537 
538 
//////////////////////////////////////////////////////////////////// ////////////////////////////////...
void make_traction_element_mesh(SolidMesh *&traction_mesh_pt)
Function to create mesh made of traction elements.
Uniform compression of a circular disk in a state of plane strain, subject to uniform growth.
void actions_before_newton_solve()
Update function (empty)
StaticDiskCompressionProblem()
Constructor:
void actions_after_newton_solve()
Update function (empty)
SolidMesh * Traction_mesh_pt
Pointer to mesh of traction elements.
ElasticRefineableQuarterCircleSectorMesh< ELEMENT > * Solid_mesh_pt
Pointer to solid mesh.
ofstream Trace_file
Trace file.
Vector< Node * > Trace_node_pt
Vector of pointers to nodes whose position we're tracing.
void doc_solution(DocInfo &doc_info)
Doc the solution.
void parameter_study(const unsigned &case_number)
Run simulation: Pass case number to label output files.
int main(int argc, char *argv[])
Driver code for disk-compression.
double E
Elastic modulus.
void constant_pressure(const Vector< double > &xi, const Vector< double > &x, const Vector< double > &n, Vector< double > &traction)
Constant pressure load.
double P
Uniform pressure.
ConstitutiveLaw * Constitutive_law_pt
Pointer to constitutive law.
double Nu
Poisson's ratio.
void growth_function(const Vector< double > &xi, double &gamma)
Growth function.
StrainEnergyFunction * Strain_energy_function_pt
Pointer to strain energy function.
double C1
"Mooney Rivlin" coefficient for generalised Mooney Rivlin law
double Uniform_gamma
Uniform volumetric expansion.