Difference between revisions of "Sample FEA Input Command File"

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  cd nairn-mpm-fea/NairnFEA/input
  cd nairn-mpm-fea/NairnFEA/input
  ./NairnFEA Cantilever.fmcmd > output.fea
  ./NairnFEA XML_Input/Cantilever.fmcmd > Cantilever.fea


The first command <tt>cd</tt>'s to the folder with the executable and the example <tt>XML</tt> input file <tt>Cantilever.fmcmd</tt> that is provided in the <tt>nairn-mpm-fea</tt> project. The second command runs the FEA calculations. This sample calculation is for an end-loaded cantilever beam and it will finish quickly. The file <tt>output.fea</tt> will have the text output results. To verify the results, open <tt>output.fea</tt> in your visualization tools (e.g., [[NairnFEAMPM]] or [[NairnFEAMPMViz]]). A sample plot of beam stresses is give [[#Trial Run with Scripted FEA Input|above]].
The first command <tt>cd</tt>'s to the <tt>nairn-mpm-fea</tt> project folder with the executable and a folder with an example <tt>XML</tt> input file <tt>Cantilever.fmcmd</tt>. The second command runs the FEA calculations. This sample calculation is for an end-loaded cantilever beam and it will finish quickly. The outfile file <tt>Cantilever.fea</tt> will have the plain text output results. To verify the results, open the new <tt>Cantilever.fea</tt> in your visualization tools (''e.g.'', [[NairnFEAMPM]] or [[NairnFEAMPMViz]]). A sample plot of beam stresses is given [[#Trial Run with Scripted FEA Input|above]].

Revision as of 07:59, 30 August 2013

The two sample FEA input command files given below will run an analysis of an end-loaded cantilever beam.

Scripted FEA Input Command File

! ********** Preamble Section **********
Title "FEA Analysis of Cantilever Beam"
Name "A nairn-mpm-fea Project Member"

! Header
Header
  A cantilever beam that is clamped at its base and
  loaded on its free end with a single point load.
EndHeader

Analysis "Plane Stress FEA"
Element "8 Node Quadrilateral"

! ********** Parameters Section **********
! Define variables for more general mesh generation capabilities
#length=50               ! Length in mm
#depth=10                ! Depth in mm
#thick=10                ! Thickness in mm
#horiz=6                 ! Elements in horizontal direction
#vert=3                  ! Elements in vertical direction
#load=500                ! End load in N
#matname$="polymer"      ! which material to use

! ********** Materials Section **********
Material "polymer","Polymer","Isotropic"
  E 2300
  nu .33
  a 60
Done

! ********** Meshing Section **********
Area #matname$,#thick
  Path "Bottom",#horiz
    Keypoint "BotLeft",0,0
    Keypoint "BotRight",#length,0
  EndPath
  Path "Right",#vert
    Keypoint "BotRight"
    Keypoint "TopRight",#length,#depth
  EndPath
  Path "Top",#horiz
    Keypoint "TopRight"
    Keypoint "TopLeft",0,#depth
  EndPath
  Path "Left",#vert
    Keypoint "TopLeft"
    Keypoint "BotLeft"
  EndPath
EndArea
Resequence "BotRight"

! ********** Boundary Condition Section **********
FixLine 0,0,0,#depth
  Displacement x
  Displacement y
EndFixLine

FixPoint "TopRight"
  Load y,#load
EndFixPoint

Trial Run with Scripted FEA Input

These scripted commands can be tried out by copying all the commands and pasting them into an empty window in NairnFEAMPM or in NairnFEAMPMViz. When done, choose the "Analyze → Run FEA/MPM Analysis" menu command. The results will stream to a window. When they are done, you can visualize the results. These sample calculations are for an end-loaded cantilever beam. The image below shows plot of stress in the x-direction for this sample problem.

Beam.jpg

XML FEA Input Command File

<?xml version='1.0'?>
<!DOCTYPE JANFEAInput SYSTEM '/Users/jnairn/Programming/Cocoa_Projects/nairn-mpm-fea/NairnFEA/input/NairnFEA.dtd'>
<JANFEAInput version="3">

  <Header>
    <Description>
A cantilever beam that is clamped at its base and
loaded on its free end with a single point load.
    </Description>
    <Analysis>1</Analysis>
  </Header>

  <Mesh>
    <Keypoints>
      <pt x="0.000000" y="0.000000" id="BotLeft"/>
      <pt x="50.000000" y="0.000000" id="BotRight"/>
      <pt x="50.000000" y="10.000000" id="TopRight"/>
      <pt x="0.000000" y="10.000000" id="TopLeft"/>
    </Keypoints>
    
    <Path id="Bottom" intervals="6">
      <keypt id="BotLeft"/>
      <keypt id="BotRight"/>
    </Path>
    <Path id="Right" intervals="3">
      <keypt id="BotRight"/>
      <keypt id="TopRight"/>
    </Path>
    <Path id="Top" intervals="6">
      <keypt id="TopRight"/>
      <keypt id="TopLeft"/>
    </Path>
    <Path id="Left" intervals="3">
      <keypt id="TopLeft"/>
      <keypt id="BotLeft"/>
    </Path>
    
    <Area mat="1" thick="10.000000" type="3" flip="0">
      <path id="Bottom"/>
      <path id="Right"/>
      <path id="Top"/>
      <path id="Left"/>
    </Area>
  </Mesh>

  <Material Type="1" Name="Polymer">
    <E>2300</E>
    <nu>0.33</nu>
    <alpha>60</alpha>
  </Material>

  <GridBCs>
    <BCLine x1="0" y1="0" x2="0" y2="10">
      <DisBC dof="1" disp="0"/>
      <DisBC dof="2" disp="0"/>
    </BCLine>
    <BCPt keypt="TopRight">
      <LoadBC dof="2" load="500"/>
    </BCPt>
    <Resequence keypt="BotRight"/>
  </GridBCs>

</JANFEAInput>

Trial Run with XML FEA Input

These <XML> commands can be tried in NairnFEAMPM or NairnFEAMPMViz as described above. Alternatively, they can be used to try out command line execution. To do a command-line trial run, first compile NairnFEA using the command-line method, which will install the executable in the NairnFEA/input folder. Next, run the following commands:

cd nairn-mpm-fea/NairnFEA/input
./NairnFEA XML_Input/Cantilever.fmcmd > Cantilever.fea

The first command cd's to the nairn-mpm-fea project folder with the executable and a folder with an example XML input file Cantilever.fmcmd. The second command runs the FEA calculations. This sample calculation is for an end-loaded cantilever beam and it will finish quickly. The outfile file Cantilever.fea will have the plain text output results. To verify the results, open the new Cantilever.fea in your visualization tools (e.g., NairnFEAMPM or NairnFEAMPMViz). A sample plot of beam stresses is given above.