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# Reduced Input

*Node and *Element Cards are removed.
```*KEYWORD
*TITLE
Fuse plate being pulled a part exhibits hourglassing troubles.
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\$  LSTC Example
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\$  Really good hourglassing on fuse plate - part 3
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\$  Switch to shell formulation S/R Hughes-Liu (6) - eliminates HG
\$     ===> *SECTION_SHELL - ELFORM
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\$  Units: mm, kg, ms, kN, GPa, kN-mm
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\$
\$\$\$\$  Control Ouput
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\$...>....1....>....2....>....3....>....4....>....5....>....6....>....7....>....8
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*CONTROL_TERMINATION
\$   endtim    endcyc     dtmin    endneg    endmas
10.01
\$
*CONTROL_ENERGY
\$     HGEN      RWEN    SLNTEN     RYLEN
2         2         1         1
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*CONTROL_OUTPUT
\$    NPOPT    NEECHO    NREFUP    IACCOP     OPIFS    IPNINT    IKEDIT
1         3
\$
\$
*DATABASE_BINARY_D3PLOT
\$       dt      lcdt
1.0
\$
*DATABASE_BINARY_D3THDT
\$       dt      lcdt
999999
\$
*DATABASE_GLSTAT
\$       dt
0.1
\$
*DATABASE_MATSUM
\$       dt
0.1
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*DATABASE_SWFORC
\$       dt
0.1
\$
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\$
\$\$\$\$  Constrain the Plates Together
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\$
\$\$\$  Spotweld the fuse plate to the post flanges.
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*CONSTRAINED_SPOTWELD
\$       n1        n2        sn        sf         n         m
284       511
247       512
428       527
417       517
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\$
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\$
\$
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\$...>....1....>....2....>....3....>....4....>....5....>....6....>....7....>....8
\$
*BOUNDARY_SPC_NODE
\$      nid       cid         x         y         z        rx        ry        rz
150         0         1         1         1         1         1         1
151         0         1         1         1         1         1         1
152         0         1         1         1         1         1         1
179         0         1         1         1         1         1         1
180         0         1         1         1         1         1         1
181         0         1         1         1         1         1         1
204         0         1         1         1         1         1         1
205         0         1         1         1         1         1         1
\$
\$      nid       dof      lcid        sf       cid        m1        m2        m3
17         1         2 2.000E+03         0
18         1         2 2.000E+03         0
19         1         2 2.000E+03         0
61         1         2 2.000E+03         0
62         1         2 2.000E+03         0
63         1         2 2.000E+03         0
100         1         2 2.000E+03         0
101         1         2 2.000E+03         0
\$
*DEFINE_CURVE
\$     lcid      sidr      scla      sclo      offa      offo
2
\$           abscissa            ordinate
0.00000000000000E+00 1.0000000000000E+00
1.00000000000000E+04 1.0000000000000E+04
\$
\$
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\$
\$\$\$\$  Define Parts and Materials
\$
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\$...>....1....>....2....>....3....>....4....>....5....>....6....>....7....>....8
\$
*PART
\$      pid       sid       mid     eosid      hgid      grav    adpopt
pstflang
1         1         1
postweb
2         2         1
fuseplat
3         3         1
\$
\$
\$\$\$\$  Materials
\$
\$
*MAT_PIECEWISE_LINEAR_PLASTICITY
\$...>....1....>....2....>....3....>....4....>....5....>....6....>....7....>....8
\$      mid        ro         e        pr      sigy      etan      eppf      tdel
1 0.783E-05 2.000E+02       0.3 2.070E-01           7.500E-01
\$  Cowper/Symonds Strain Rate Parameters
\$        c         p      lcss      lcsr
40         5
\$  Plastic stress/strain curve
0.000E+00 8.000E-02 1.600E-01 4.000E-01 9.900E+01
2.070E-01 2.500E-01 2.750E-01 2.899E-01 3.000E-01
\$
\$
\$\$\$\$  Sections
\$
*SECTION_SHELL
\$      sid    elform      shrf       nip     propt   qr/irid     icomp
1         6
\$       t1        t2        t3        t4      nloc
5.4600E+00 5.460E+00 5.460E+00 5.460E+00
\$
*SECTION_SHELL
\$      sid    elform      shrf       nip     propt   qr/irid     icomp
2         6
\$       t1        t2        t3        t4      nloc
4.3200E+00 4.320E+00 4.320E+00 4.320E+00
\$
\$
*SECTION_SHELL
\$      sid    elform      shrf       nip     propt   qr/irid     icomp
3         2
\$         3         6
\$       t1        t2        t3        t4      nloc
4.7625E+00 4.762E+00 4.762E+00 4.762E+00
\$
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\$
\$\$\$\$  Define Nodes and Elements
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\$...>....1....>....2....>....3....>....4....>....5....>....6....>....7....>....8
\$
\$
*END```