4. B modeling#

4.1. Characteristics of modeling#

Model A is repeated, but by adding damping to the mass/spring system.

Discreet element in type translation DIS_T

_images/10000262000010F30000048C5BF6BDB2083723BD.svg

Characteristics of the elements:

At nodes \(\mathrm{P1}\) and \(\mathrm{P2}\): mass matrices of type M_T_D_N with \(m=100\mathrm{kg}\).

Between \(\mathrm{P1}\) and \(\mathrm{P2}\): a K_T_D_L stiffness matrix with \({K}_{x}={10}^{6}N/m\)

Boundary conditions:

All degrees of freedom are locked except degree of freedom \(\mathrm{DX}\) from node \(\mathrm{P2}\).

Damping: A \(\mathrm{0,1}\text{}\) reduction in damping is added to the system.

It is introduced into the test case, either usually by the keyword AMOR_REDUIT, or, to validate the functionality RELA_EFFO_VITE, by a linear relationship between the mass/spring speed and a force applied to the node \(\mathrm{P2}\).

4.2. Characteristics of the mesh#

Number of knots: 2

Number of meshes and types: 1 SEG2, 2 POI1

4.3. Features tested#

In particular, in this modeling, the functionality RELA_EFFO_VITE of the DYNA_VIBRA operator (BASE_CALCUL =” GENE “) is tested in this modeling. Through its use, it is possible to introduce a non-linear behavior dependent on the speed of a point. Here we validate this relationship in a simple way in the linear case by comparing it with a modal damping behavior (which, in the case of a single mode, amounts to viscous damping).

4.4. Tested sizes and results#

Identification

Reference

Tolerance

DYNA_VIBRA (BASE_CALCUL =” GENE “) AMOR_REDUIT

\(\mathrm{0,53}\text{m}\)

1%

DYNA_VIBRA (BASE_CALCUL =” GENE “) RELA_EFFO_VITE

\(\mathrm{0,53}\text{m}\)

1%

DYNA_VIBRA (BASE_CALCUL =” GENE “) AMOR_REDUIT

\(0.531338\) (non regression)

1.E -4%

DYNA_VIBRA (BASE_CALCUL =” GENE “) RELA_EFFO_VITE

\(0.531338\) (non regression)

1.E -4%