Different properties are available in RADIOSS and used to describe different elements. Like solid (8-node brick, 4-node or 10-node tetra, shell (3-node or 4-node shell), spring, beam, truss or joint. Together with material it was assembled with /PART for each structure member.
Property Type |
Fixed Format Number |
Description |
Keywords |
Application |
---|---|---|---|---|
Truss property |
2 |
TYPE2, TRUSS |
Truss, bar |
|
Beam properties |
3 |
TYPE3, BEAM |
Used for simulate beam under axial loading, torsion and bending. |
|
18 |
TYPE18, INT_BEAM |
Used for deep beam cases (short beams). Beam section and position of integration points can be either used as predefined or stated directly. |
||
Spring and Joint properties |
4 |
TYPE4, SPRING |
Physical spring or physical dashpot |
|
8 |
TYPE8, SPR_GENE |
With 6 independent DOF to describe general spring joint |
||
12 |
TYPE12, SPR_PUL |
Pully, seatbelt |
||
13 |
TYPE13, SPR_BEAM |
Spotweld |
||
25 |
TYPE25, SPR_AXI |
Axisymmetric Spring |
||
26 |
TYPE26, SPR_TAB |
Spring, spotweld |
||
28 |
TYPE28, NSTRAND |
Seat belt |
||
32 |
TYPE32, SPR_PRE |
pretension spring |
||
33 |
TYPE33, KJOINT |
Used for different kinematic joint (spherical, revolute, cylindrical, planar, universal, translational, Oldham, rigid or free joint) |
||
35 |
TYPE35, STITCH |
"stitch" spring in airbag simulation |
||
36 |
TYPE36, PREDIT |
Beam-like spring element for spot-weld |
||
44 |
TYPE44, SPR_CRUS |
Used to simulate crushable frame in car body to quick reproduce buckling behavior |
||
45 |
TYPE45, KJOINT2 |
Used for different kinematic joint (spherical, revolute, cylindrical, planar, universal, translational, Oldham, rigid or free joint) |
||
46 |
TYPE46, SPR_MUSCLE |
Muscle |
||
Shell properties |
1 |
TYPE1, SHELL |
Used for general 3-node or 4-node shell |
|
9 |
TYPE9, SH_ORTH |
For orthotropic material |
||
10 |
TYPE10, SH_COMP |
For composite material |
||
11 |
TYPE11, SH_SANDW |
For composite material |
||
16 |
TYPE16, SH_FABR |
For composite material |
||
17 |
TYPE17, STACK |
For composite material |
||
19 |
TYPE19, PLY |
For composite material |
||
51 |
Stacking information for ply-based Sandwich Shell Property Set |
TYPE51 |
For composite material |
|
-- |
PCOMPP |
For composite material |
||
Composite options |
-- |
Stacking information for ply-based Sandwich Shell Property Set |
STACK |
For composite material |
-- |
PLY |
For composite material |
||
-- |
Define Fiber Orientation Change and Thinning for a Ply, due to draping |
DRAPE |
For composite material |
|
Thick Shell properties |
20 |
TYPE20, TSHELL |
Thick wall structure , massive junctions |
|
21 |
TYPE21, TSH_ORTH |
Orthotropic thick wall structure or massive junctions |
||
22 |
TYPE22, TSH_COMP |
Thick wall structure or massive junctions for composite |
||
Brick properties |
6 |
TYPE6, SOL_ORTH |
Fiber plane, steel reinforcement direction or cell direction for honeycomb |
|
14 |
TYPE14, SOLID |
Used for general solid element like 8-node brick, 4-node or 10-node tetra |
||
43 |
TYPE43, CONNECT |
Used with LAW59 or LAW83 to describe solid spot-weld or adhesive structure |
||
SPH property |
34 |
TYPE34, SPH |
Used for SPH part |
|
CFD properties |
14 |
TYPE14, FLUID |
General Fluid |
|
15 |
TYPE15, POROUS |
Air, gas |
||
Other properties |
0 |
TYPE0, VOID |
Used for contact interface |
|
29 |
TYPE29, USER1 |
User defined property |
||
30 |
TYPE30, USER2 |
User defined property |
||
31 |
TYPE31, USER3 |
User defined property |
1. | Property types 1, 2, 3, 4, 6, 8, 9, 10, 11, 12, 13, 14 (SOLID), 16, 18, 19, 20, 21, 22, 25, 26, 28, 32, 33, 35, 36, 43, 44, 46, 51 and PCOMPP are compatible with local units system. |
2. | For shell and thick shell composite parts, with /PROP/SH_COMP, /PROP/SH_SANDW, /PROP/TSH_ORTH or /PROP/TSH_COMP, materials are defined directly in the property card. The failure criteria defined within these materials (for example, LAW25) are accounted for. Material referred to in the /PART card is only for calculation of time step and contact stiffness. |
3. | TYPE1 (SHELL), TYPE11 (SH_SANDW), or TYPE51 properties are compatible with XFEM, provided failure model FLD, JOHNSON, TAB1, or TBUTCHER is used. |
4. | /PROP/TYPE51 and /FAIL/TAB1 cannot be used with XFEM yet. |
5. | Currently, XFEM is only 2D element compatible. |
See Also:
Implicit Features and Compatibility Information
Solid-Shell Elements Guideline