Validation Case: Impact of an Elastoplastic Bar

This validation case belongs to an elastoplastic impact in solid mechanics. The aim of this test case is to validate the following parameters:

• Dynamic analysis
• Frictional contact
• Elastoplasticity
• Large deformations

The simulation results of SimScale were compared to the numerical results presented in [SDNV103]\(^1\).

Geometry

The geometry used for the case is as follows:

It represents an elastoplastic bar in the z-direction and a rectangular plate in the x-y plane with the following coordinates for each point:

Point	X [m]	Y [m]	Z [m]
A	0	0	0
B	0.016	0	0
C	0.016	0.016	0
D	0	0.016	0
E	0	0	0.001
F	0.016	0	0.001
G	0.016	0.016	0.001
H	0	0.016	0.001
I	0	0	0.00327
J	0.0032	0	0.00327
K	0	0.0032	0.00327
L	0	0	0.03567
M	0.0032	0	0.03567
N	0	0.0032	0.03567

Analysis Type and Mesh

Tool Type: Code Aster

Analysis Type: Dynamic

Mesh and Element Types:

Case	Mesh Type	Number of Nodes	Number of Prisms	Number of Hexahedrals	Element Type
A	1st order prisms and hexahedrals	764	120	481	Standard
B	2nd order prisms and hexahedral	2861	120	481	Reduced Integration
C	2nd order prisms and hexahedrals	2861	120	481	Standard

The tetrahedral mesh was computed using SimScale’s Standard mesh algorithm and manual sizing. The hexahedral meshes were computed locally and uploaded into the simulation project.

Simulation Setup

Material:

• Bi-linear Plasticity Isotropic:
  • \( E = \) 117 \( GPa \)
  • \( \nu = \) 0.35
  • \( \sigma_y = \) 400 \( MPa \)
  • \( E_T = \) 500 \( MPa \)

Boundary Conditions:

• Initial Conditions:
  • Velocity of 227 \(m/s \) to volume IJKLM (bar)
• Constraints:
  • Volume ABCDEFGH (plate) fixed
  • Face IKLN zero x-displacement
  • Face IJLM zero y-displacement

Reference Solution

The reference solution is from a numerical computation as presented section 2 of [SDNV103]\(^1\), which are taken as the mean results of [Stainer]\(^2\):

\( DX_J = 3.87 mm \)

\( DZ_L = 13.46 mm \)

Result Comparison

Comparison of displacements at points J (DX) and L (DZ) at time \( t = 9×10^{-5}\ s \):

CASE	POINT	COMP	COMPUTED	REF	ERROR
A	J	DX	0.00117536	0.00387	-69.6 %
A	L	DZ	-0.0134496	-0.01346	0.1 %
B	J	DX	0.00301416	0.00387	-22.1 %
B	L	DZ	-0.0126052	-0.01346	6.4 %
C	J	DX	0.00273561	0.00387	-29.3 %
C	L	DZ	-0.0125145	-0.01346	7.0 %

Illustration of the final shape (case B) can be found in Figure 4. The elastoplastic deformation due to the impact can be appreciated:

Related Tutorials

Tutorial: Crash Test of FSAE Impact Attenuator

Last updated: October 8th, 2020