Home / Examples / Stress Analysis [Galileo] / Example 29: Contact Analysis of Two Cantilevers

Example 29: Contact Analysis of Two Cantilevers


General

 

Analysis Space

Item

Settings

Analysis Space

3D

Model Unit

mm

 

Analysis Conditions

The model is symmetric over XZ plane, so a half model, cut at XZ plane, is analyzed.

[Large Displacement] is selected as a type of large deformation.

[Large Displacement] is more suitable than [Large Strain] for this model.

Item

Settings

Solver

Stress Analysis [Galileo]

Analysis Type

Static Analysis

Large Deformation

Select Large Displacement

 

The nonlinear analysis is set up on the Step/Thermal Load tab as follows.

Number of Substeps is set to 40, which is larger than the default setting of 20, because a large deformation is expected.

As Save results of substeps is selected, states at intermediate substeps through the final step will be saved.

Add unloading step is selected as well to analyze the state without forced displacement.

Tab

Setting Item

Settings

Step/Thermal Load

Step/Reached Temperature Setting

Substeps of Step 1 : 40

Options for the Nonlinear Analysis

Save the results of substeps : Select

Add unloading step : Select

 

Model

The bottom face of the upper cantilever and the top face of the lower cantilever are set with the boundary conditions of contactor and contactee respectively.

The side faces on X=0 pane are fixed in all directions, whereas the side faces on Y=0 plane are fixed in Y direction.

 

Body Attributes and Materials

Body Number/Type

Body Attribute Name

Material Name

0/Solid

Body1

Mat1

1/Solid

Body2

Mat2

 

The material properties are set up as follows:

Material Name

Tab

Properties

Mat1

Elasticity

Material Type: Elasto-plastic/Bilinear, Isotropic

Young's Modulus: 1×109 [Pa]

Poisson's Ratio: 0.3

Strain Hardening Rate : 0.2x109 [Pa]

Initial Yield Stress: 8x106 [Pa]

Mat2

Elasticity

Material Type: Elastic/Isotropic

Young's modulus: 1×109 [Pa]

Poisson's Ratio: 0.3

Boundary Conditions

On the tip end of the upper cantilever, the forced displacement of 1.5 [mm] is applied in -Z direction.

The fixed ends of the cantilever are fixed completely.

Boundary Condition Name/Topology

Tab

Boundary Condition Type

Settings

Fix_all/Sheet

Mechanical

Displacement

Select all X/Y/Z components.

UX=0, UY=0, UZ=0

Fix_y/Sheet

Mechanical

Displacement

Select the Y component.

UY=0

Down/Edge

Mechanical

Displacement

Select the Z component.

UZ=1.5x10-3[m]

Contactor/Edge

Mechanical

Contact Surface

Select [Contactor Surface].

Target/Edge

Mechanical

Contact Surface

Select [Contactee Surface].

The contactor and contactee surfaces are designated as a contact pair in the [Boundary Pair] dialog. In contact analyses, the contact surfaces must be designated as a boundary pair.

Results

The displacement at the step 0.5 (corresponding to -0.75 mm displacement in Z direction of Down) is shown below.

The left figure shows the principal plastic strain. The right figure shows the contour of von Mises equivalent strain.

The upper body is contacting the lower. The plastic strain is exhibited in the lower body.

 

The displacement at the step 1 (corresponding to -1.50mm displacement in Z direction of Down) is shown below.

The left figure shows the principal plastic strain. The right figure shows the contour of von Mises equivalent strain.

The plastic strains are created in the wide area of the lower body. The difference of von Mises equivalent stresses between the two bodies is becoming large.

 

The displacement at the step 1.025 which is an unloading stage (1st substep of the unloading stage : No Z displacement of Down) is shown below.

The left figure shows the principal plastic strain. The right figure shows the contour of von Mises equivalent strain.

Upper body returns to the original form because it has no Z displacement. Plastic strain remains in the lower body.

 

The displacement at the step 2 which is an unloading stage (last substep of the unloading stage : No Z displacement of Down) is shown below.

The left figure shows the principal plastic strain. The right figure shows the contour of von Mises equivalent strain.

The state is same as step 1.025 with the same results of plastic strain and stress.

 

With the results displayed, go to the [Show Results] tab



and click [Create Animation] . The animation file (.avi) will be created.

The animation gives you a visual understanding of the large deformation.