*Heading
** FESA projection of the Abaqus 2024 cantilever reference model.
** Geometry, material, section, boundary conditions, and load are unchanged.
** SCF is set to zero because FESA does not use Abaqus slenderness compensation.
*Preprint, echo=NO, model=NO, history=NO, contact=NO
*Part, name=PART-1_1
*Node
      1,           0.,           0.,           0.
      2,           1.,           0.,           0.
      3,           2.,           0.,           0.
      4,           3.,           0.,           0.
      5,           4.,           0.,           0.
      6,           5.,           0.,           0.
      7,           6.,           0.,           0.
      8,           7.,           0.,           0.
      9,           8.,           0.,           0.
     10,           9.,           0.,           0.
     11,          10.,           0.,           0.
*Element, type=B31
 1,  1,  2
 2,  2,  3
 3,  3,  4
 4,  4,  5
 5,  5,  6
 6,  6,  7
 7,  7,  8
 8,  8,  9
 9,  9, 10
10, 10, 11
*Elset, elset=Set-1, generate
  1,  10,   1
*Beam General Section, elset=Set-1, material=Material-1, section=GENERAL
1., 0.0833333, 0., 0.0833333, 0.140833
0.,1.,0.
*Transverse Shear Stiffness
6.73077e+10, 6.73077e+10, 0.
*End Part
*Assembly, name=Assembly
*Instance, name=PART-1_1-1, part=PART-1_1
*End Instance
*Nset, nset=Set-3, instance=PART-1_1-1
 1,
*Nset, nset=Set-4, instance=PART-1_1-1
 11,
*End Assembly
*Material, name=Material-1
*Elastic
 2.1e+11, 0.3
*Boundary
Set-3, 1, 1
Set-3, 2, 2
Set-3, 3, 3
Set-3, 4, 4
Set-3, 5, 5
Set-3, 6, 6
*Step, name=Step-1, nlgeom=NO
*Static
1., 1., 1e-05, 1.
*Cload
Set-4, 3, -1e+06
*End Step
