DEMO_febio_0026_hexlattice_compression
Below is a demonstration for:
- Building geometry for a cube with hexahedral elements
- Defining the boundary conditions
- Coding the febio structure
- Running the model
- Importing and visualizing the displacement and stress results
Contents
Keywords
- febio_spec version 4.0
- febio, FEBio
- uniaxial loading
- compression, tension, compressive, tensile
- displacement control, displacement boundary condition
- hexahedral elements, hex8
- cube, box, rectangular
- static, solid
- hyperelastic, Ogden
- displacement logfile
- stress logfile
clear; close all; clc;
Plot settings
Plot settings
fontSize=15; faceAlpha1=0.8; faceAlpha2=1; edgeColor=0.25*ones(1,3); edgeWidth=1.5; markerSize=25; cMap=gjet(4);
Control parameters
% Path names defaultFolder = fileparts(fileparts(mfilename('fullpath'))); savePath=fullfile(defaultFolder,'data','temp'); % Defining file names febioFebFileNamePart='tempModel'; febioFebFileName=fullfile(savePath,[febioFebFileNamePart,'.feb']); %FEB file name febioLogFileName=[febioFebFileNamePart,'.txt']; %FEBio log file name febioLogFileName_disp=[febioFebFileNamePart,'_disp_out.txt']; %Log file name for exporting displacement febioLogFileName_force=[febioFebFileNamePart,'_force_out.txt']; %Log file name for exporting force febioLogFileName_stress=[febioFebFileNamePart,'_stress_out.txt']; %Log file name for exporting stress %Specifying dimensions and number of elements sampleSize=10; shrinkFactor=0.2; nSplitPattern=1; %Define applied displacement appliedStrain=0.3; %Linear strain (Only used to compute applied stretch) loadingOption='compression'; % or 'tension' switch loadingOption case 'compression' stretchLoad=1-appliedStrain; %The applied stretch for uniaxial loading case 'tension' stretchLoad=1+appliedStrain; %The applied stretch for uniaxial loading end displacementMagnitude=(stretchLoad*sampleSize)-sampleSize; %The displacement magnitude %Material parameter set E_youngs1=0.1; %Material Young's modulus nu1=0.4; %Material Poisson's ratio % FEA control settings numTimeSteps=10; %Number of time steps desired max_refs=25; %Max reforms max_ups=0; %Set to zero to use full-Newton iterations opt_iter=6; %Optimum number of iterations max_retries=5; %Maximum number of retires dtmin=(1/numTimeSteps)/100; %Minimum time step size dtmax=1/numTimeSteps; %Maximum time step size runMode='external';% 'internal' or 'external'
Creating example geometry.
X=[-1; 1; 1; -1; -1; 1; 1; -1;]; Y=[-1; -1; 1; 1; -1; -1; 1; 1;]; Z=[-1; -1;-1; -1; 1; 1; 1; 1;]; V=sampleSize*[X(:) Y(:) Z(:)]/2; E=1:8; %Element description of the 8-node cube (hexahedral element) [E,V,C]=subHex(E,V,nSplitPattern); %Subdevide into 8 sub-cubes [E,V,C]=hex2tet(E,V,C,1); %Convert to tetrahedral elements [F,~]=element2patch(E,C); %Patch data for plotting [indBoundary]=tesBoundary(F);
Create lattice structure
testCase=1; controlParameter.meshType='hex'; %desired output mesh type controlParameter.indBoundary=indBoundary; %indices of the boundary faces switch testCase case 1 controlParameter.shrinkFactor=shrinkFactor; %Strut sides are formed by shrinking the input mesh faces by this factor controlParameter.hexSplit=1; %Number of beam hex split steps controlParameter.latticeSide=2; %1=side 1 the edge lattice, 2=side 2 the dual lattice to the edge lattice [Es,Vs,Cs]=element2lattice(E,V,controlParameter); case 2 end % Create patch Data for visualization [Fs,CsF,CFs]=element2patch(Es,Cs); %Patch data for plotting % Fs0=Fs(CsF==0,:); % CsF0=CsF(CsF==0); indB=tesBoundary(Fs); Fb=Fs(indB,:); CsFb=CsF(indB,:); CFsb=CFs(indB,:);
Visualizing input mesh and lattic structures
cFigure; hs=subplot(1,2,1); title('The input mesh','fontSize',fontSize) hold on; gpatch(F,V,0.5*ones(1,3),'k',0.5); axisGeom(gca,fontSize); camlight headlight; lighting flat; subplot(1,2,2); title('Lattice side 1','fontSize',fontSize) hold on; gpatch(F,V,'none','k',0,2); gpatch(Fb,Vs,'bw','k',0.5); axisGeom(gca,fontSize); camlight headlight; lighting flat; drawnow;
faceBoundaryMarker=zeros(size(Fb,1),1);
%Find top and bottom face sets
[Nb]=patchNormal(Fb,Vs);
zVec=[0 0 1];
d=dot(Nb,zVec(ones(size(Nb,1),1),:),2);
Z=Vs(:,3);
ZF=mean(Z(Fb),2);
logicTop_Fb=(d>0.9) & ZF>=(max(Vs(:,3))-eps(sampleSize));
logicBottom_Fb=(d<-0.9) & ZF<=(min(Vs(:,3))+eps(sampleSize));
xVec=[1 0 0];
d=dot(Nb,xVec(ones(size(Nb,1),1),:),2);
X=Vs(:,1);
XF=mean(X(Fb),2);
logicSides_Fb1=(d>0.9) & XF>=(max(Vs(:,1))-eps(sampleSize));
logicSides_Fb2=(d<-0.9) & XF<=(min(Vs(:,1))+eps(sampleSize));
yVec=[0 1 0];
d=dot(Nb,yVec(ones(size(Nb,1),1),:),2);
Y=Vs(:,2);
YF=mean(Y(Fb),2);
logicSides_Fb3=(d>0.9) & YF>=(max(Vs(:,2))-eps(sampleSize));
logicSides_Fb4=(d<-0.9) & YF<=(min(Vs(:,2))+eps(sampleSize));
faceBoundaryMarker(logicBottom_Fb)=1;
faceBoundaryMarker(logicTop_Fb)=2;
faceBoundaryMarker(logicSides_Fb1)=3;
faceBoundaryMarker(logicSides_Fb2)=4;
faceBoundaryMarker(logicSides_Fb3)=5;
faceBoundaryMarker(logicSides_Fb4)=6;
Smoothen lattice
%Get "clean" surface mesh for only the boundary [Fb_clean,Vb_clean,indFix]=patchCleanUnused(Fb,Vs); %Find indices of points to hold on to during smoothing indKeep=Fb_clean(faceBoundaryMarker>0,:); indKeep=unique(indKeep(:)); %Smoothing cPar.Method='HC'; cPar.n=15; cPar.RigidConstraints=indKeep; [Vb_clean]=tesSmooth(Fb_clean,Vb_clean,[],cPar); %Override coordinates in full mesh with smoothed coordinates ind=Fb(:); ind=unique(ind(:)); Vs(ind,:)=Vb_clean;
Visualize smoothed mesh
cFigure; hold on; title('Smoothed mesh','FontSize',fontSize); gpatch(F,V,'kw','none',0.1); gpatch(Fb,Vs,faceBoundaryMarker,'k',1); % plotV(Vb_clean(indKeep,:),'r.','markerSize',15) axisGeom; camlight headlight; set(gca,'FontSize',fontSize); % axis off drawnow;
DEFINE BC's
%Supported nodes bcSupportList=unique(Fb(faceBoundaryMarker==1,:)); %Prescribed force nodes bcPrescribeList=unique(Fb(faceBoundaryMarker==2,:));
Visualize BC's
cFigure; hold on; title('Boundary conditions','FontSize',fontSize); gpatch(Fb,Vs,'kw','none',0.4); hl(1)=plotV(Vs(bcSupportList,:),'k.','MarkerSize',markerSize); hl(2)=plotV(Vs(bcPrescribeList,:),'r.','MarkerSize',markerSize); legend(hl,{'BC full support','BC prescribed Z displacement'}) axisGeom; camlight headlight; set(gca,'FontSize',fontSize); drawnow;
logicNotBeam=CsF==1; Fss=Fs(logicNotBeam,:); controlParGroup.outputType='label'; g=tesgroup(Fss,controlParGroup); R=nan(max(g),1); for q=1:1:max(g) logicNow= (g==q); F_now=Fss(logicNow,:); indNow=unique(F_now(:)); indNow=indNow(ismember(indNow,Fb)); V_now=Vs(indNow,:); V_now=V_now-mean(V_now); R(q)=mean(sqrt(sum(V_now.^2,2))); end strutThicknessMean=2*mean(R);
cFigure; hold on; gpatch(F,V,'none','k',0,2); gpatch(Fb,Vs,'none','k',1,1); gpatch(Fss,Vs,g,'k',0.5); axisGeom(gca,fontSize); camlight headlight; lighting flat; % colormap spectral; icolorbar drawnow;
Check porosity
vol_lattice=sum(hexVol(Es,Vs)); %Volume of hexahedra porosity_lattice=vol_lattice./sampleSize.^3; %Porosity
Defining the FEBio input structure
See also febioStructTemplate and febioStruct2xml and the FEBio user manual.
%Get a template with default settings [febio_spec]=febioStructTemplate; %febio_spec version febio_spec.ATTR.version='4.0'; %Module section febio_spec.Module.ATTR.type='solid'; %Control section febio_spec.Control.analysis='STATIC'; febio_spec.Control.time_steps=numTimeSteps; febio_spec.Control.step_size=1/numTimeSteps; febio_spec.Control.solver.max_refs=max_refs; febio_spec.Control.solver.qn_method.max_ups=max_ups; febio_spec.Control.time_stepper.dtmin=dtmin; febio_spec.Control.time_stepper.dtmax=dtmax; febio_spec.Control.time_stepper.max_retries=max_retries; febio_spec.Control.time_stepper.opt_iter=opt_iter; %Material section materialName1='Material1'; febio_spec.Material.material{1}.ATTR.name=materialName1; febio_spec.Material.material{1}.ATTR.type='neo-Hookean'; febio_spec.Material.material{1}.ATTR.id=1; febio_spec.Material.material{1}.E=E_youngs1; febio_spec.Material.material{1}.v=nu1; %Mesh section % -> Nodes febio_spec.Mesh.Nodes{1}.ATTR.name='nodeSet_all'; %The node set name febio_spec.Mesh.Nodes{1}.node.ATTR.id=(1:size(Vs,1))'; %The node id's febio_spec.Mesh.Nodes{1}.node.VAL=Vs; %The nodel coordinates % -> Elements partName1='Part1'; febio_spec.Mesh.Elements{1}.ATTR.name=partName1; %Name of this part febio_spec.Mesh.Elements{1}.ATTR.type='hex8'; %Element type febio_spec.Mesh.Elements{1}.elem.ATTR.id=(1:1:size(Es,1))'; %Element id's febio_spec.Mesh.Elements{1}.elem.VAL=Es; %The element matrix % -> NodeSets nodeSetName1='bcSupportList'; febio_spec.Mesh.NodeSet{1}.ATTR.name=nodeSetName1; febio_spec.Mesh.NodeSet{1}.VAL=mrow(bcSupportList); nodeSetName2='bcPrescribeList'; febio_spec.Mesh.NodeSet{2}.ATTR.name=nodeSetName2; febio_spec.Mesh.NodeSet{2}.VAL=mrow(bcPrescribeList); %MeshDomains section febio_spec.MeshDomains.SolidDomain.ATTR.name=partName1; febio_spec.MeshDomains.SolidDomain.ATTR.mat=materialName1; %Boundary condition section % -> Fix boundary conditions febio_spec.Boundary.bc{1}.ATTR.name='zero_displacement_xyz'; febio_spec.Boundary.bc{1}.ATTR.type='zero displacement'; febio_spec.Boundary.bc{1}.ATTR.node_set=nodeSetName1; febio_spec.Boundary.bc{1}.x_dof=1; febio_spec.Boundary.bc{1}.y_dof=1; febio_spec.Boundary.bc{1}.z_dof=1; febio_spec.Boundary.bc{2}.ATTR.name='zero_displacement_xy'; febio_spec.Boundary.bc{2}.ATTR.type='zero displacement'; febio_spec.Boundary.bc{2}.ATTR.node_set=nodeSetName2; febio_spec.Boundary.bc{2}.x_dof=1; febio_spec.Boundary.bc{2}.y_dof=1; febio_spec.Boundary.bc{2}.z_dof=0; febio_spec.Boundary.bc{3}.ATTR.name='prescibed_displacement_z'; febio_spec.Boundary.bc{3}.ATTR.type='prescribed displacement'; febio_spec.Boundary.bc{3}.ATTR.node_set=nodeSetName2; febio_spec.Boundary.bc{3}.dof='z'; febio_spec.Boundary.bc{3}.value.ATTR.lc=1; febio_spec.Boundary.bc{3}.value.VAL=displacementMagnitude; febio_spec.Boundary.bc{3}.relative=0; %LoadData section % -> load_controller febio_spec.LoadData.load_controller{1}.ATTR.name='LC_1'; febio_spec.LoadData.load_controller{1}.ATTR.id=1; febio_spec.LoadData.load_controller{1}.ATTR.type='loadcurve'; febio_spec.LoadData.load_controller{1}.interpolate='LINEAR'; %febio_spec.LoadData.load_controller{1}.extend='CONSTANT'; febio_spec.LoadData.load_controller{1}.points.pt.VAL=[0 0; 1 1]; %Output section % -> log file febio_spec.Output.logfile.ATTR.file=febioLogFileName; febio_spec.Output.logfile.node_data{1}.ATTR.file=febioLogFileName_disp; febio_spec.Output.logfile.node_data{1}.ATTR.data='ux;uy;uz'; febio_spec.Output.logfile.node_data{1}.ATTR.delim=','; febio_spec.Output.logfile.node_data{2}.ATTR.file=febioLogFileName_force; febio_spec.Output.logfile.node_data{2}.ATTR.data='Rx;Ry;Rz'; febio_spec.Output.logfile.node_data{2}.ATTR.delim=','; febio_spec.Output.logfile.element_data{1}.ATTR.file=febioLogFileName_stress; febio_spec.Output.logfile.element_data{1}.ATTR.data='s1'; febio_spec.Output.logfile.element_data{1}.ATTR.delim=','; % Plotfile section febio_spec.Output.plotfile.compression=0;
Quick viewing of the FEBio input file structure
The febView function can be used to view the xml structure in a MATLAB figure window.
febView(febio_spec); %Viewing the febio file
Exporting the FEBio input file
Exporting the febio_spec structure to an FEBio input file is done using the febioStruct2xml function.
febioStruct2xml(febio_spec,febioFebFileName); %Exporting to file and domNode
Running the FEBio analysis
To run the analysis defined by the created FEBio input file the runMonitorFEBio function is used. The input for this function is a structure defining job settings e.g. the FEBio input file name. The optional output runFlag informs the user if the analysis was run succesfully.
febioAnalysis.run_filename=febioFebFileName; %The input file name febioAnalysis.run_logname=febioLogFileName; %The name for the log file febioAnalysis.disp_on=1; %Display information on the command window febioAnalysis.runMode=runMode; [runFlag]=runMonitorFEBio(febioAnalysis);%START FEBio NOW!!!!!!!!
%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% --------> RUNNING/MONITORING FEBIO JOB <-------- 20-Apr-2023 10:45:51 FEBio path: /home/kevin/FEBioStudio2/bin/febio4 # Attempt removal of existing log files 20-Apr-2023 10:45:51 * Removal succesful 20-Apr-2023 10:45:51 # Attempt removal of existing .xplt files 20-Apr-2023 10:45:51 * Removal succesful 20-Apr-2023 10:45:51 # Starting FEBio... 20-Apr-2023 10:45:51 Max. total analysis time is: Inf s * Waiting for log file creation 20-Apr-2023 10:45:51 Max. wait time: 30 s * Log file found. 20-Apr-2023 10:45:52 # Parsing log file... 20-Apr-2023 10:45:52 number of iterations : 3 20-Apr-2023 10:45:53 number of reformations : 3 20-Apr-2023 10:45:53 ------- converged at time : 0.1 20-Apr-2023 10:45:53 number of iterations : 3 20-Apr-2023 10:45:54 number of reformations : 3 20-Apr-2023 10:45:54 ------- converged at time : 0.2 20-Apr-2023 10:45:54 number of iterations : 4 20-Apr-2023 10:45:55 number of reformations : 4 20-Apr-2023 10:45:55 ------- converged at time : 0.3 20-Apr-2023 10:45:55 number of iterations : 4 20-Apr-2023 10:45:57 number of reformations : 4 20-Apr-2023 10:45:57 ------- converged at time : 0.4 20-Apr-2023 10:45:57 number of iterations : 4 20-Apr-2023 10:45:58 number of reformations : 4 20-Apr-2023 10:45:58 ------- converged at time : 0.5 20-Apr-2023 10:45:58 number of iterations : 4 20-Apr-2023 10:45:59 number of reformations : 4 20-Apr-2023 10:45:59 ------- converged at time : 0.6 20-Apr-2023 10:45:59 number of iterations : 4 20-Apr-2023 10:46:01 number of reformations : 4 20-Apr-2023 10:46:01 ------- converged at time : 0.7 20-Apr-2023 10:46:01 number of iterations : 4 20-Apr-2023 10:46:02 number of reformations : 4 20-Apr-2023 10:46:02 ------- converged at time : 0.8 20-Apr-2023 10:46:02 number of iterations : 4 20-Apr-2023 10:46:03 number of reformations : 4 20-Apr-2023 10:46:03 ------- converged at time : 0.9 20-Apr-2023 10:46:03 number of iterations : 3 20-Apr-2023 10:46:04 number of reformations : 3 20-Apr-2023 10:46:04 ------- converged at time : 1 20-Apr-2023 10:46:04 Elapsed time : 0:00:12 20-Apr-2023 10:46:04 N O R M A L T E R M I N A T I O N # Done 20-Apr-2023 10:46:04 %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
Import FEBio results
if runFlag==1 %i.e. a succesful run
Importing nodal displacements from a log file
dataStruct=importFEBio_logfile(fullfile(savePath,febioLogFileName_disp),0,1); %Access data N_disp_mat=dataStruct.data; %Displacement timeVec=dataStruct.time; %Time %Create deformed coordinate set Vs_DEF=N_disp_mat+repmat(Vs,[1 1 size(N_disp_mat,3)]);
Plotting the simulated results using anim8 to visualize and animate deformations
DN_magnitude=sqrt(sum(N_disp_mat(:,:,end).^2,2)); %Current displacement magnitude % Create basic view and store graphics handle to initiate animation hf=cFigure; %Open figure gtitle([febioFebFileNamePart,': Press play to animate']); title('Displacement magnitude [mm]','Interpreter','Latex') hp=gpatch(Fb,Vs_DEF(:,:,end),DN_magnitude,'k',1); %Add graphics object to animate hp.FaceColor='interp'; axisGeom(gca,fontSize); colormap(gjet(250)); colorbar; caxis([0 max(DN_magnitude)]); axis(axisLim(Vs_DEF)); %Set axis limits statically camlight headlight; % Set up animation features animStruct.Time=timeVec; %The time vector for qt=1:1:size(N_disp_mat,3) %Loop over time increments DN_magnitude=sqrt(sum(N_disp_mat(:,:,qt).^2,2)); %Current displacement magnitude %Set entries in animation structure animStruct.Handles{qt}=[hp hp]; %Handles of objects to animate animStruct.Props{qt}={'Vertices','CData'}; %Properties of objects to animate animStruct.Set{qt}={Vs_DEF(:,:,qt),DN_magnitude}; %Property values for to set in order to animate end anim8(hf,animStruct); %Initiate animation feature drawnow;
Importing element stress from a log file
dataStruct=importFEBio_logfile(fullfile(savePath,febioLogFileName_stress),0,1);
%Access data
E_stress_mat=dataStruct.data;
E_stress_mat(isnan(E_stress_mat))=0;
Plotting the simulated results using anim8 to visualize and animate deformations
[CV]=faceToVertexMeasure(Es,Vs,E_stress_mat(:,:,end)); % Create basic view and store graphics handle to initiate animation hf=cFigure; %Open figure gtitle([febioFebFileNamePart,': Press play to animate']); title('$\sigma_{zz}$ [MPa]','Interpreter','Latex') hp=gpatch(Fb,Vs_DEF(:,:,end),CV,'k',1); %Add graphics object to animate hp.FaceColor='interp'; axisGeom(gca,fontSize); colormap(gjet(250)); colorbar; caxis([min(E_stress_mat(:)) max(E_stress_mat(:))]/3); axis(axisLim(Vs_DEF)); %Set axis limits statically camlight headlight; % Set up animation features animStruct.Time=timeVec; %The time vector for qt=1:1:size(N_disp_mat,3) %Loop over time increments [CV]=faceToVertexMeasure(Es,Vs,E_stress_mat(:,:,qt)); %Set entries in animation structure animStruct.Handles{qt}=[hp hp]; %Handles of objects to animate animStruct.Props{qt}={'Vertices','CData'}; %Properties of objects to animate animStruct.Set{qt}={Vs_DEF(:,:,qt),CV}; %Property values for to set in order to animate end anim8(hf,animStruct); %Initiate animation feature drawnow;
Importing nodal forces from a log file
[dataStruct]=importFEBio_logfile(fullfile(savePath,febioLogFileName_force),0,1); %Nodal forces %Access data timeVec=dataStruct.time; f_sum_x=squeeze(sum(dataStruct.data(bcPrescribeList,1,:),1)); f_sum_y=squeeze(sum(dataStruct.data(bcPrescribeList,2,:),1)); f_sum_z=squeeze(sum(dataStruct.data(bcPrescribeList,3,:),1));
Visualize force data
displacementApplied=timeVec.*displacementMagnitude; cFigure; hold on; xlabel('$u$ [mm]','Interpreter','Latex'); ylabel('$F_z$ [N]','Interpreter','Latex'); hp=plot(displacementApplied(:),f_sum_z(:),'b-','LineWidth',3); grid on; box on; axis square; axis tight; set(gca,'FontSize',fontSize); drawnow;
end
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Kevin Mattheus Moerman, [email protected]
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License: https://github.com/gibbonCode/GIBBON/blob/master/LICENSE
GIBBON: The Geometry and Image-based Bioengineering add-On. A toolbox for image segmentation, image-based modeling, meshing, and finite element analysis.
Copyright (C) 2006-2022 Kevin Mattheus Moerman and the GIBBON contributors
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