1. Reference problem#

1.1. Geometry#

_images/10002144000018E800001389091CE90579E56117.svg

The geometry represents only a quarter of the test piece CTJ25

planes of symmetry: \((x{B}_{0}y)\) and \((x{B}_{0}z)\)

Thickness: \(\mathrm{DD}’=12.5\mathrm{mm}\)

Face1: \((A,\mathrm{B0},\mathrm{B1},\mathrm{B2},\mathrm{B3},\mathrm{B4},\mathrm{B5},C,D,E)\)

Face2: \((A,\mathrm{B0},\mathrm{B0}\text{'},A\text{'})\)

Coordinates of the points (\(\mathrm{mm}\)):

min

max

\(B0\)

\(F\)

\(B5’\)

\(x\)

-20.

42.5

\(y\)

20.25

3.5

\(z\)

12.5

12.5

12.5

1.2. Material properties#

\(E=2.027027{10}^{11}\mathrm{Pa}\)

\(\nu =0.3\)

1.3. Boundary conditions and loads#

All the nodes on face1:

\(\mathrm{DZ}=0\)

All the nodes on face2:

\(\mathrm{DY}=0\)

All the nodes in line \(\mathrm{FF}\text{'}\):

\(\mathrm{DX}=0\)

\(\mathrm{DY}=0.01\)