# Cylinder embedded in another cylinder—smooth

 Title Cylinder embedded in another cylinder—smooth Tags elasticity compression bending Runnng time a few seconds See also 115-cyl-cyl-rough CAEplex case https://caeplex.com/p/f7916 Available in HTML PDF ePub

# 1 Problem description

Consider a vertical cylinder aligned with the z axis of radius r_1=25~\text{mm} and height h=50~\text{mm} which is embedded into another larger vertical cylinder of radius r_2=50~\text{mm} with the same height h. The base of the larger embedding cylinder lies on the x-y plane and the embedded cylinder is shifted h/2=25~\text{mm} upwards (fig. 1. The material properties are given in tbl. 1

Table 1: Material properties
Young modulus E [GPa] Poisson’s coefficient \nu
Small cylinder (stem) 120 0.26
Large cylinder (base) 2.5 0.36

The base and the lateral surface of the large cylinder are fully fixed. The upper surface of the stem has a traction condition \sigma_t = (+1,0,-10)~\text{MPa} so both compression and bending solicitations exist.

Figure 1: A small cylinder embedded into another one. CAD from CAEplex https://caeplex.com/p/f7916 (rotate and zoom it).

# 2 Geometry and mesh

The geometry was created in FreeCAD and exported as a BREP file. The following cyl-cyl-smooth.geo loads the geometry and defines the physical groups:

• volume stem is the small cylinder,
• volume base is the large cylinder,
• surfaces fixed are the base and the lateral surfaces of the large cylinder (base) which are to be fixed, and
• surface load is the top surface of the small cylinder (stem).
Merge "cyl-cyl-freecad.brep";  // load geometry

// physical groups
Physical Volume("stem") = {1};
Physical Volume("base") = {2};
Physical Surface("fixed") = {5, 7};

// mesh options
Mesh.CharacteristicLengthMax = 3.0;

Mesh.SecondOrderLinear = 0;  // curved
Mesh.ElementOrder = 2;       // second-order elements

Mesh.Algorithm = 6;
Mesh.Algorithm3D = 1;

Mesh.Optimize = 1;
Mesh.OptimizeNetgen = 1;
Mesh.HighOrderOptimize = 1;

# 3 Input file

The annotated input file cyl-cyl-smooth.fin explains what it does. Properties in multi-material problems are given using the MATERIAL keyword.

MESH FILE_PATH cyl-cyl-smooth.msh DIMENSIONS 3    # load mesh

# assign per-material properties
MATERIAL stem E 120e3  nu 0.26
MATERIAL base E 2.5e3  nu 0.35

# set boundary conditions
PHYSICAL_ENTITY fixed BC fixed

# explicitly ask Fino to always smooth stresses and to flat-average stresses
FINO_SOLVER SMOOTH always ELEMENT_WEIGHT flat
FINO_STEP

# write output
MESH_POST FILE_PATH cyl-cyl-smooth-fino.vtk VECTOR u v w sigma

# report maximum diplacement in scientific notation
PRINT "Maximum displacement magnitude:" %e displ_max "mm"

# 4 Execution

Besides reporting the maximum displacement, which will be used when comparing results with CalculiX, a single VTK file cyl-cyl-smooth-fino.vtk with the displacement field and the von Mises stress distribution is created.

$gmsh -v 0 -3 cyl-cyl-smooth.geo$ fino cyl-cyl-smooth.fin
Maximum displacement magnitude: 2.542721e-02    mm
\$ 

Note that we ask Fino to always smooth stresses, unlike Cylinder embedded in another cylinder—rough where we investigate what happens if stresses are never averaged.

# 5 Results

Figs. 2 (a), 2 (b) show the stresses over the warped geometry. As expected, both compression and bending is obtained. The “curved” tetrahedra (and triangles) can be seen, especially on the stem as each actual second-order triangle is shown as composed of four smaller ones which are not co-planar.

Figure 2: Von Mises stresses obtained by Fino. a — Full view, b — Clipped & warped \times 250 view

# 6 Check

The same problem is solved with CalculiX using an input file created with FreeCAD FEM module (this is the reason the original geometry was created with FreecAD) with the same Gmsh-generated mesh as when solving with Fino. CalculiX’ output FRD file and Fino’s output VTK file are both read back by Fino (actually by the wasora framework) and an algebraic difference is taken at each point of space in order to create a new VTK file comparing the two solutions:

# read Fino's results
MESH NAME fino FILE_PATH cyl-cyl-smooth-fino.vtk DIMENSIONS 3 {
}

MESH NAME ccx FILE_PATH cyl-cyl-smooth.frd DIMENSIONS 3 {
}

# compute Von Mises for ccx out of the stress tensor
SVM(x,y,z) := sqrt(0.5*((SXX(x,y,z)-SYY(x,y,z))^2 + \
(SYY(x,y,z)-SZZ(x,y,z))^2 + \
(SZZ(x,y,z)-SXX(x,y,z))^2 + \
6*(SXY(x,y,z)^2 + SYZ(x,y,z)^2 + SZX(x,y,z)^2)))

# compute algebraic differences
diff_sigma(x,y,z) := SVM(x,y,z) - sigma(x,y,z)
diff_u(x,y,z) := D1(x,y,z) - u(x,y,z)
diff_v(x,y,z) := D2(x,y,z) - v(x,y,z)
diff_w(x,y,z) := D3(x,y,z) - w(x,y,z)

# write VTK files using both grids to make sure they are the same
MESH_POST MESH fino   FILE_PATH diff-smooth-fino.vtk  VECTOR diff_u diff_v diff_w diff_sigma
MESH_POST MESH ccx    FILE_PATH diff-smooth-ccx.vtk   VECTOR diff_u diff_v diff_w diff_sigma

Fig. 3 (a) shows the results of the abolute differences in displacements as computed by Fino and CalculiX. The maximum magnitude is 1.4 \times 10^{-4}~\text{mm} whereas the maximum computed displacement, as reported in the terminal mimic, is 2.5 \times 10^{-2}~\text{mm}—although these maxima do not occur at the same locations. On the other hand, it can be seen in fig. 3 (b) that the maximum differences in stresses are in the order of 0.3%.