4.1 Example 1: Link modeled with solid elements

This example models a simple flexible link component using three-dimensional continuum elements.

To perform the analysis for the link modeled with solid elements:

  1. Enter the following commands to extract the input files from the compressed archive files provided with the Abaqus release:

    abaqus fetch job=adams_ex1
    abaqus fetch job=adams_ex1_nodes
    abaqus fetch job=adams_ex1_elements

  2. Enter the following command to execute the Abaqus analysis:

    abaqus job=adams_ex1

  3. Enter the following command to execute the Abaqus Interface for MSC.ADAMS and translate the results file generated in the Abaqus analysis to a modal neutral file for use with ADAMS/Flex:

    abaqus adams job=adams_ex1

The solid element link model used in the MSC.ADAMS four-bar linkage model is shown in Figure 4–1.

Figure 4–1 Solid link model.

The link is modeled with 642 C3D10 tetrahedral solid elements (1368 nodes).

Because the solid elements have only displacement degrees of freedom at their nodes, multi-point constraints are used to provide a connection to the other components in the MSC.ADAMS model. Two nodes are added along the centerline of the beam at the centers of the hinge holes. The C3D10 nodes that lie on the faces of the hinge holes are connected to the extra nodes with BEAM-type multi-point constraints, allowing the nodes to transmit both forces and moments between the link and other MSC.ADAMS components.

The options used to define the single substructure are those described in The Abaqus substructure model, Section 2.1. Twenty fixed-interface vibration modes are computed to represent the dynamic behavior of the link.

MSC.ADAMS uses the fixed-interface vibration modes and the constraint modes to characterize the flexibility of the link. The eight lowest fixed-interface vibration frequencies computed by Abaqus are shown in Table 4–1. These frequencies are reported in the adams_ex1.dat file.

Table 4–1 Fixed-interface vibration frequencies for the solid link model.

Frequency, Hz
206
391
570
1124
1228
1817
1879
2541
The Abaqus Interface for MSC.ADAMS combines these fixed-interface modes with the static constraint modes to compute an equivalent modal basis to be used by ADAMS/Flex. The first six frequencies of this equivalent basis are approximately zero. The next eight frequencies for the unconstrained model are shown in Table 4–2. These frequencies are written to the screen when executing the Abaqus Interface for MSC.ADAMS.

Table 4–2 Nonzero frequencies for the solid link model that are used by ADAMS/Flex.

Frequency, Hz
194
535
574
1055
1551
1762
1801
2653

The Abaqus input file for the solid model, adams_ex1.inp, is shown below.

*HEADING
Link modeled with C3D10 solid elements
**  ----------------------------------------------
**
**               NODE DEFINITION
**
*NODE,input=adams_ex1_nodes.inp
**
**
*NSET, NSET=LEFTCYL
8,9,17,18,70,71,72,73,125,126,127,128,134,135,207,
229,230,278,309,310,311,312,313,314,373,374,375,376,
377,378,389,390,391,392,498,533,534,535,546,565,566,
677,688,734,1058,1059,1073,1085,1114,1115,1311,1312,
1325,1335,1356,1357
**
*NSET, NSET=RIGHTCYL
6,7,15,16,66,67,68,69,121,122,123,124,136,137,231,
232,303,304,305,306,307,308,367,368,369,370,371,372,
393,394,395,396,479,480,481,487,488,506,635,654,957,
958,976,977,1004,1026,1219,1220,1234,1235,1257,1287
**
*MPC
BEAM,LEFTCYL,10000
BEAM,RIGHTCYL,20000
**  ----------------------------------------------
**
**               ELEMENT DEFINITION
**
*ELEMENT,TYPE=C3D10,ELSET=PROP1,INPUT=adams_ex1_elements.inp
**
**
**  ----------------------------------------------
**
**               ELEMENT PROPERTY DEFINITION
**
*SOLID SECTION,ELSET=PROP1,MATERIAL=STEEL
**
**  ----------------------------------------------
**
**               MATERIAL DEFINITION
**
*MATERIAL,NAME=STEEL
*ELASTIC
 2.069999944E+11, 3.000000119E-01,
*DENSITY
 7.800000000E+03,
**
*NSET,NSET=RETNODES
10000,20000
**
**  ----------------------------------------------
**
*STEP
*FREQUENCY,EIGENSOLVER=LANCZOS
20,
*BOUNDARY
RETNODES, 1,6
*ELEMENT MATRIX OUTPUT, MASS=YES, ELSET=PROP1
*NODE FILE
U
*END STEP
**
**  ----------------------------------------------
**
**               SUBSTRUCTURE GENERATION
**
*STEP
*SUBSTRUCTURE GENERATE, TYPE=Z1, RECOVERY MATRIX=YES, 
 MASS MATRIX=YES, OVERWRITE
*RETAINED NODAL DOFS, SORTED=NO
RETNODES, 1,6 
*SELECT EIGENMODES,generate
1,20
*SUBSTRUCTURE MATRIX OUTPUT, STIFFNESS=YES, MASS=YES, 
 RECOVERY=YES
*END STEP