Elements
Elements are FE idealizations for a portion of a physical part.
Every element must be organized into one component, and therefore are mutually exclusive to a component.
Element Configurations
Each element has an associated element configuration. An element configuration tells HyperWorks how to draw, store, and work with the element.
Bar Elements
1D elements created in a space between two or three nodes of a model where beam properties are desired.
The nodes are related to each other based on the properties of the bar or beam element connecting them. Properties associated with bar elements include vector orientation, offset vectors that end at A and B, or at A, B, and C, and pin flags to tell it what degree of freedom should carry through the beam.
Bar elements are displayed as a line between two nodes with BAR2 or BAR3 written at the centroid of the element.
 Bar2
 Configuration 60  1D (1st order) elements with 2 nodes used to model axial, bending, and torsion behavior. Bar2 elements have a property reference, an orientation vector, offset vectors and ends A and B, and pin flags at ends A and B.
 Bar3
 Configuration 63  1D (2nd order) elements with 3 nodes used to model axial, bending, and torsion behavior. Bar3 elements have a property reference, an orientation vector, offset vectors and ends A and B, and pin flags at ends A and B.
Gap Elements
Configuration 70  1D elements created in a space between two nodes, or between a node and an element, of a model where contact may occur.
Create a gap element when you want to impose a nonlinear constraint on a model; this constraint will limit the amount of movement possible during analysis.
Gap elements have a property reference and an orientation vector.
Gap elements are displayed as a line between two nodes with GAP written at the centroid of the element.
Gap elements can translate to CGAP or CGAPG elements in OptiStruct, CGAP element in Nastran or *GAP option in Abaqus.
Hex Elements
3D hexahedra elements.
 Hex8
 Configuration 208  3D (1st order) hexahedra elements with 8 nodes.
 Hex20
 Configuration 220  3D (2nd order) hexahedra elements with 20 nodes.
Joint Elements
Configuration 22  1D elements with 2, 4, or 6 nodes which have a property and orientation systems or nodes.
Joint element is a definition of a connection between two rigid bodies. Joint elements store a property and orientation information.
Joint elements are displayed with lines between the appropriate nodes and the letter J between nodes 1 and 3 of the element.
Type  Type Name  Number of Nodes  Orientation  Solver Interface 

1  Spherical joint  2 


2  Revolute joint  4 

LSDYNA 
3  Cylindrical joint  4 

LSDYNA 
4  Planar joint  4 

LSDYNA 
5  Universal joint  4 

LSDYNA 
6  Translational joint  6 

LSDYNA 
7  Locking joint  6 

LSDYNA 
8  Ball joint  2  None  OptiStruct 
9  Fixed joint  2  None  OptiStruct 
10  Revolute joint  2 

OptiStruct 
11  Translational1 joint  2 

OptiStruct 
12  Cylindercal 1 joint  2 

OptiStruct 
13  Universal joint  2 

OptiStruct 
14  Constant_velocity joint  2 

OptiStruct 
15  Planar joint  2 

OptiStruct 
16  Inline joint  2 

OptiStruct 
17  Perpendicular joint  2 

OptiStruct 
18  Parallel axes joint  2 

OptiStruct 
19  Inplane joint  2 

OptiStruct 
20  Orient joint  2 

OptiStruct 
21  Point_to_curve joint  2 

OptiStruct 
22  Curve_to_curve joint  2 

OptiStruct 
23  Point_to_deformable_curve joint  2 

OptiStruct 
24  Point_to_deformable_surface joint  2 

OptiStruct 
25  Translational_2N joint  2 

PAMCRASH 
26  Revolute_2N joint  2 

PAMCRASH 
27  Cylindrical_2N joint  2 

PAMCRASH 
28  Universal_2N joint  2 

PAMCRASH 
29  FlexionTorsion joint  2 

PAMCRASH 
30  Planar_2N joint  2 

PAMCRASH 
31  General joint  2 

PAMCRASH 
32  Bracket joint  2 

PAMCRASH 
33  Free joint  2 

PAMCRASH 
Mass Elements
Configuration 1  0D elements with a single node that allow you to assign concentrated mass to the model in order to represent a physical part that may not be modeled with another FE idealization.
Mass elements are displayed as a dot with the letter M written at the centroid of the element.
Master Elements
Master interface elements.
 Master3
 Configuration 123  Master interface elements with 3 nodes. (Must be Type 1).
 Master4
 Configuration 124  Master4 elements are master interface elements with 4 nodes. (Must be Type 1).
Penta Elements
3D triangular prism pentahedra elements.
 Penta6
 Configuration 206  3D (1st order) triangular prism pentahedra elements with 6 nodes.
 Penta15
 Configuration 215  3D (2nd order) triangular prism pentahedra elements with 15 nodes.
Plot Elements
Configuration 2  1D elements with 2 nodes used for display purposes.
Plot elements are displayed as a line between two nodes.
Pyramid Elements
3D pyramid pentahedra elements.
 Pyramid5
 Configuration 205  3D (1st order) pyramid pentahedra elements with 5 nodes.
 Pyramid13
 Configuration 213  3D (2nd order) pyramid pentahedra elements with 5 nodes.
Quad Elements
2D quadrilateral elements.
 Quad4
 Configuration 104  2D (1st order) quadrilateral elements with 4 nodes.
 Quad8
 Configuration 108  2D (2nd order) quadrilateral elements with 8 nodes.
RBE3 Elements
Configuration 56  Rigid elements with one dependent node and variable independent nodes typically used to define the motion at the dependent node as a weighted average of the motions at the independent nodes.
Both the dependent node and independent nodes contain a coefficient (weighting factor) and userdefined degrees of freedom. The dependent degrees of freedom and weighting factors can be specified or automatically calculated based on the geometry.
RBE3 elements are displayed as lines between the dependent node and the independent node(s) with RBE3 displayed at the dependent node of the element.
Rigid Elements
Configuration 5  Rigid 1D elements with 2 nodes used to model rigid connections.
Rigid elements are displayed as a line between two nodes with the letter R written at the centroid of the element.
Rigids can translate to RBE2 in Nastran or *MPC in Abaqus.
Rigidlink Elements
Configuration 55  Rigid elements with one independent node and variable dependent nodes typically used to model rigid bodies.
Rigidlink elements have userdefined degrees of freedom which apply to all dependent nodes.
Rigidlink elements are displayed as lines between the independent node and the dependent node(s) with RL displayed at the independent node of the element.
Rod Elements
Configuration 61  1D elements with 2 nodes used to model axial behavior only.
The two nodes are related to each other based on the properties of the rod element connecting them. Rod elements have property pointers.
Rod elements are displayed as a line between two nodes with ROD written at the centroid of the element.
Rods can translate to CTUBES in Nastran or a C1D2 element in Abaqus.
Slave Elements
Slave interface elements.
 Slave1
 Configuration 135  Slave interface elements with 1 node. (Must be Type 1).
 Slave3
 Configuration 133  Slave interface elements with 3 node. (Must be Type 1).
 Slave4
 Configuration 134  Slave interface elements with 1 node. (Must be Type 1).
Spring Elements
Configuration 21  1D elements used to model spring connections.
Spring elements have userdefined degrees of freedom, an orientation vector, and a property reference.
Spring elements are displayed as a line between two nodes with the letter K written at the centroid of the element.
 Spring
 1D elements with 2 nodes used to model spring connections.
 Spring2N
 1D elements with 2 nodes used to model spring connections.
 Spring3N
 1D elements with 3 nodes used to model spring connections.
 Spring4N
 1D elements with 4 nodes used to model spring connections.
Springs can translate to CELAS2 in Nastran or *SPRING in Abaqus.
Tetra Elements
3D tetrahedra elements.
 Tetra4
 Configuration 204  3D (1st order) tetrahedra elements with 4 nodes.
 Tetra10
 Configuration 210  3D (2nd order) tetrahedra elements with 10 nodes.
Tria Elements
2D triangular elements.
 Tria3
 Configuration 103  2D (1st order) triangular elements with 3 nodes.
 Tria6
 Configuration 106  2D (2nd order) triangular elements with 6 nodes.
Weld Elements
Configuration 3  Rigid 1D elements with 2 nodes used to model welded connections.
Weld elements are displayed as a line between two nodes with the letter W written at the centroid of the element.
Xelems
1D multistrand elements.
Supported Solver Cards
Solver cards supported for elements.
Abaqus Cards
Card  Supported Element Configurations  Description 

*COUPLING  Rigid/RBE3  Define a surfacebased coupling constraint where
the *SURFACE card points to elements. Note: The *COUPLING is also
supported as rigid elements (COUP_KIN) and RBE3 (COUP_DIS)
when *SURFACE points to nodes.

*ELEMENT 

Defines elements by giving their nodes. 
*ELGEN  Generates elements incrementally. These cards are resolved to individual entities on import and are written back on export the same way. Note: Standard 2D
only.


*MPC  Rigid  Defines multipoint constraints. 
*RELEASE 

Releases rotational degrees of freedom at one or
both ends of a beam element. For 2D problems, only dof6 (M1) is active. Add a *RELEASE card to this element by
clicking pins a = and pins b = and type in the HyperMesh dof code for the Abaqus release combination code you
want.

AC1D2  Bar2  2node acoustic link 
AC1D3  Bar3  3node acoustic link 
AC2D3  Tria3  3node linear 2D acoustic triangle 
AC2D4  Quad4  4node linear 2D acoustic quadrilateral 
AC2D6  Tria6  6node quadratic 2D acoustic triangular prism 
AC2D8  Quad8  8node quadratic 2D acoustic quadrilateral 
AC3D10  Tetra10  10node quadratic acoustic tetrahedron 
AC3D15 

15node quadratic acoustic triangular prism 
AC3D20 

20node quadratic acoustic brick 
AC3D4  Tetra4  4node linear acoustic tetrahedron 
AC3D6  Penta6  6node linear acoustic triangular prism 
AC3D8  Hex8  8node linear acoustic brick 
AC3D8R  Hex8  
ACAX3  Tria3  3node linear axisymmetric acoustic triangle 
ACAX4  Quad4  4node linear axisymmetric acoustic quadrilateral 
ACAX6  Tria6  6node quadratic axisymmetric acoustic triangle 
ACAX8  Quad8  8node quadratic axisymmetric acoustic quadrilateral 
ACIN3D3  Tria3  3node linear 3D acoustic infinite element 
ACIN3D4  Quad4  4node linear 3D acoustic infinite element 
ACIN3D6  Tria6  6node quadratic 3D acoustic infinite element 
ACIN3D8  Quad8  8node quadratic 3D acoustic infinite element 
B21  Bar2  2node linear beam in a plane 
B21H  Bar2  2node linear beam in a plane, hybrid formulation 
B22  Bar3  3node quadratic beam in a plane 
B22H  Bar3  3node quadratic beam in a plane, hybrid formulation 
B23  Bar2  2node cubic beam in a plane 
B23H  Bar2  2node cubic beam in a plane, hybrid formulation 
B31  Bar2  2node linear beam 
B31H  Bar2  2node linear beam, hybrid formulation 
B31OS  Bar2  2node linear opensection beam 
B31OSH  Bar2  2node linear opensection beam, hybrid formulation 
B32  Bar3  3node quadratic beam in space 
B32  Bar3  3node quadratic beam 
B32H  Bar3  3node quadratic beam, hybrid formulation 
B32OS  Bar3  3node quadratic opensection beam 
B32OSH  Bar3  3node quadratic opensection beam, hybrid formulation 
B33  Bar2  2node cubic beam 
B33H  Bar2  2node cubic beam, hybrid formulation 
BEAM  Rigid  
C3D10  Tetra10  10node quadratic tetrahedron 
C3D10E  Tetra10  10node quadratic piezoelectric tetrahedron 
C3D10H  Tetra10  10node quadratic tetrahedron, hybrid, constant pressure 
C3D10HS  Tetra10  
C3D10I  Tetra10  10node generalpurpose quadratic tetrahedron, improved surface stress visualization 
C3D10M  Tetra10  10node modified tetrahedron, hourglass control 
C3D10MH  Tetra10  10node modified quadratic tetrahedron, hybrid, linear pressure, hourglass control 
C3D10MP  Tetra10  10node modified displacement and pore pressure tetrahedron, hourglass control 
C3D10MPH  Tetra10  10node modified displacement and pore pressure tetrahedron, hybrid, linear pressure, hourglass control 
C3D10MT  Tetra10  10node thermally coupled modified quadratic tetrahedron, hourglass control 
C3D10S  
C3D15 

15node quadratic triangular prism 
C3D15E 

15node quadratic piezoelectric triangular prism 
C3D15H 

15node quadratic triangular prism, hybrid, linear pressure 
C3D20 

20node quadratic brick 
C3D20E 

20node quadratic piezoelectric brick 
C3D20H 

20node quadratic brick, hybrid, linear pressure 
C3D20HT 

20node thermally coupled brick, triquadratic displacement, trilinear temperature, hybrid, linear pressure 
C3D20PH  Hex20  20node brick, triquadratic displacement, trilinear pore pressure, hybrid, linear pressure 
C3D20R 

20node quadratic brick, reduced integration 
C3D20RE 

20node quadratic piezoelectric brick, reduced integration 
C3D20RH 

20node quadratic brick, hybrid, linear pressure, reduced integration 
C3D20RHT 

20node thermally coupled brick, triquadratic displacement, trilinear temperature, hybrid, linear pressure, reduced integration 
C3D20RP  Hex20  20node brick, triquadratic displacement, trilinear pore pressure, reduced integration 
C3D20RPH  Hex20  20node brick, triquadratic displacement, trilinear pore pressure, hybrid, linear pressure, reduced integration 
C3D20RT 

20node thermally coupled brick, triquadratic displacement, trilinear temperature, reduced integration 
C3D20T 

20node thermally coupled brick, triquadratic displacement, trilinear temperature 
C3D30P  Hex20  20node brick, triquadratic displacement, trilinear pore pressure 
C3D4  Tetra4  4node linear tetrahedron 
C3D4E  Tetra4  4node linear piezoelectric tetrahedron 
C3D4H  Tetra4  4node linear tetrahedron, hybrid, linear pressure 
C3D4P  Tetra4  
C3D4T  Tetra4  4node thermally coupled tetrahedron, linear displacement and temperature 
C3D6 

6node linear triangular prism 
C3D6E 

6node linear piezoelectric triangular prism 
C3D6H 

6node linear triangular prism, hybrid, constant pressure 
C3D6P  Penta6  
C3D6T  Penta6  6node thermally coupled triangular prism, linear displacement and temperature 
C3D8 

8node linear brick 
C3D8E 

8node linear piezoelectric brick 
C3D8H 

8node linear brick, hybrid, constant pressure 
C3D8HS  Hex8  
C3D8HT 

8node thermally coupled brick, trilinear displacement and temperature, hybrid, constant pressure 
C3D8I 

8node linear brick, incompatible modes 
C3D8IH 

8node linear brick, hybrid, linear pressure, incompatible modes 
C3D8P  Hex8  8node brick, trilinear displacement, trilinear pore pressure 
C3D8PH  Hex8  8node brick, trilinear displacement, trilinear pore pressure, hybrid, constant pressure 
C3D8R 

8node linear brick, reduced integration, hourglass control 
C3D8RH 

8node linear brick, hybrid, constant pressure, reduced integration, hourglass control 
C3D8RHT 

8node thermally coupled brick, trilinear displacement and temperature, reduced integration, hourglass control, hybrid, constant pressure 
C3D8RHT  Pyramid5  8node thermally coupled brick, trilinear displacement and temperature, reduced integration, hourglass control, hybrid, constant pressure 
C3D8RP  Hex8  8node brick, trilinear displacement, trilinear pore pressure, reduced integration 
C3D8RPH  Hex8  8node brick, trilinear displacement, trilinear pore pressure, reduced integration, hybrid, constant pressure 
C3D8RT 

8node thermally coupled brick, trilinear displacement and temperature, reduced integration, hourglass control 
C3D8S  Hex8  
C3D8T 

8node thermally coupled brick, trilinear displacement and temperature 
CAX3  Tria3  3node linear axisymmetric triangle 
CAX3E  Tria3  3node linear axisymmetric piezoelectric triangle 
CAX3H  Tria3  3node linear axisymmetric triangle, hybrid, constant pressure 
CAX3T  Tria3  3node axisymmetric thermally coupled triangle, linear displacement and temperature 
CAX4  Quad4  4node bilinear axisymmetric quadrilateral 
CAX4E  Quad4  4node bilinear axisymmetric piezoelectric quadrilateral 
CAX4H  Quad4  4node bilinear axisymmetric quadrilateral, hybrid, constant pressure 
CAX4HT  Quad4  4node axisymmetric thermally coupled quadrilateral, bilinear displacement and temperature, hybrid, constant pressure 
CAX4I  Quad4  4node bilinear axisymmetric quadrilateral, incompatible modes 
CAX4IH  Quad4  4node bilinear axisymmetric quadrilateral, hybrid, linear pressure, incompatible modes 
CAX4R 

4node bilinear axisymmetric quadrilateral, reduced integration, hourglass control 
CAX4RH  Quad4  4node bilinear axisymmetric quadrilateral, hybrid, constant pressure, reduced integration, hourglass control 
CAX4T  Quad4  4node axisymmetric thermally coupled quadrilateral, bilinear displacement and temperature 
CAX6  Tria6  6node quadratic axisymmetric triangle 
CAX6H  Tria6  6node quadratic axisymmetric triangle, hybrid, linear pressure 
CAX6M  Tria6  6node modified axisymmetric triangle, hourglass control 
CAX6MH  Tria6  6node modified quadratic axisymmetric triangle, hybrid, linear pressure, hourglass control 
CAX8  Quad8  8node biquadratic axisymmetric quadrilateral 
CAX8H  Quad8  8node biquadratic axisymmetric quadrilateral, hybrid, linear pressure 
CAX8HT  Quad8  8node axisymmetric thermally coupled quadrilateral, biquadratic displacement, bilinear temperature, hybrid, linear pressure 
CAX8R  Quad8  8node biquadratic axisymmetric quadrilateral, reduced integration 
CAX8RH  Quad8  8node biquadratic axisymmetric quadrilateral, hybrid, linear pressure, reduced integration 
CAX8RHT  Quad8  8node axisymmetric thermally coupled quadrilateral, biquadratic displacement, bilinear temperature, hybrid, linear pressure, reduced integration 
CAX8RT  Quad8  8node axisymmetric thermally coupled quadrilateral, biquadratic displacement, bilinear temperature, reduced integration 
CAX8T  Quad8  8node axisymmetric thermally coupled quadrilateral, biquadratic displacement, bilinear temperature 
CAXA41  Quad4  
CAXA4H1  Quad4  
CAXA4R1  Quad4  
CAXA4RH1  Quad4  
CAXA81  Quad8  
CAXA8H1  Quad8  
CAXA8P1  Quad8  
CAXA8R1  Quad8  
CAXA8R4  Quad8  
CAXA8RH1  Quad8  
CAXA8RH4  Quad8  
CAXA8RP1  Quad8  
CCL12  Hex8  12node cylindrical brick 
CGAX3  Tria3  3node generalized linear axisymmetric triangle, twist 
CGAX3H  Tria3  3node generalized linear axisymmetric triangle, hybrid, constant pressure, twist 
CGAX4  Quad4  4node generalized bilinear axisymmetric quadrilateral, twist 
CGAX4H  Quad4  4node generalized bilinear axisymmetric quadrilateral, hybrid, constant pressure, twist 
CGAX4R  Quad4  4node generalized bilinear axisymmetric quadrilateral, reduced integration, hourglass control, twist 
CGAX4RH  Quad4  4node generalized bilinear axisymmetric quadrilateral, hybrid, constant pressure, reduced integration, hourglass control, twist 
CGAX6  Tria6  6node generalized quadratic axisymmetric triangle, twist 
CGAX6H  Tria6  6node generalized quadratic axisymmetric triangle, hybrid, linear pressure, twist 
CGAX8  Quad8  8node generalized biquadratic axisymmetric quadrilateral, twist 
CGAX8H  Quad8  8node generalized biquadratic axisymmetric quadrilateral, hybrid, linear pressure, twist 
CGAX8R  Quad8  8node generalized biquadratic axisymmetric quadrilateral, reduced integration, twist 
CGAX8RH  Quad8  8node generalized biquadratic axisymmetric quadrilateral, hybrid, linear pressure, reduced integration, twist 
CGAX8T  Quad8  8node generalized axisymmetric thermally coupled quadrilateral, biquadratic displacement, bilinear temperature, twist 
COH2D4  Quad4  4node twodimensional cohesive element 
COH3D6  Penta6  6node threedimensional cohesive element 
COH3D8  Hex8  8node threedimensional cohesive element 
COHAX4  Quad4  4node axisymmetric cohesive element 
CONN2D2 

Connector element in a plane between two nodes or ground and a node 
CONN3D2 

Connector element in space between two nodes or ground and a node 
COUP_DIS  rbe3  
COUP_KIN  Rigid  
CPE  Quad4  
CPE3  Tria3  3node linear plane strain triangle 
CPE3E  Tria3  3node linear plane strain piezoelectric triangle 
CPE3H  Tria3  3node linear plane strain triangle, hybrid, constant pressure 
CPE4E  Quad4  4node bilinear plane strain piezoelectric quadrilateral 
CPE4HT  Quad4  4node plane strain thermally coupled quadrilateral, bilinear displacement and temperature, hybrid, constant pressure 
CPE4I  Quad4  4node bilinear plane strain quadrilateral, incompatible modes 
CPE4IH  Quad4  4node bilinear plane strain quadrilateral, hybrid, linear pressure, incompatible modes 
CPE4P  Quad4  4node plane strain quadrilateral, bilinear displacement, bilinear pore pressure 
CPE4PH  Quad4  4node plane strain quadrilateral, bilinear displacement, bilinear pore pressure, hybrid, constant pressure 
CPE4R  Quad4  4node bilinear plane strain quadrilateral, reduced integration, hourglass control 
CPE4RH  Quad4  4node bilinear plane strain quadrilateral, hybrid, constant pressure, reduced integration, hourglass control 
CPE4RP  Quad4  4node plane strain quadrilateral, bilinear displacement, bilinear pore pressure, reduced integration, hourglass control 
CPE4RPH  Quad4  4node plane strain quadrilateral, bilinear displacement, bilinear pore pressure, hybrid, constant pressure, reduced integration, hourglass control 
CPE4T  Quad4  4node plane strain thermally coupled quadrilateral, bilinear displacement and temperature 
CPE6  Tria6  6node quadratic plane strain triangle 
CPE6H  Tria6  6node quadratic plane strain triangle, hybrid, linear pressure 
CPE6M  Tria6  6node modified quadratic plane strain triangle, hourglass control 
CPE6MH  Tria6  6node modified quadratic plane strain triangle, hybrid, linear pressure, hourglass control 
CPE6MP  Tria6  6node modified displacement and pore pressure plane strain triangle, hourglass control 
CPE6MPH  Tria6  6node modified displacement and pore pressure plane strain triangle, hybrid, linear pressure, hourglass control 
CPE8  Quad8  8node biquadratic plane strain quadrilateral 
CPE8H  Quad8  8node biquadratic plane strain quadrilateral, hybrid, linear pressure 
CPE8P  Quad8  8node plane strain quadrilateral, biquadratic displacement, bilinear pore pressure 
CPE8PH  Quad8  8node plane strain quadrilateral, biquadratic displacement, bilinear pore pressure, hybrid, linear pressure stress 
CPE8R  Quad8  8node biquadratic plane strain quadrilateral, reduced integration 
CPE8RH  Quad8  8node biquadratic plane strain quadrilateral, hybrid, linear pressure, reduced integration 
CPE8RP  Quad8  8node plane strain quadrilateral, biquadratic displacement, bilinear pore pressure, reduced integration 
CPE8RPH  Quad8  8node biquadratic displacement, bilinear pore pressure, reduced integration, hybrid, linear pressure 
CPEG3  Tria3  3node linear generalized plane strain triangle 
CPEG4R  Quad4  4node bilinear generalized plane strain quadrilateral, reduced integration, hourglass control 
CPH4H  Quad4  
CPS3  Tria3  3node linear plane stress triangle 
CPS3E  3node linear plane stress piezoelectric triangle  
CPS4  Quad4  4node bilinear plane stress quadrilateral 
CPS4E  Quad4  4node bilinear plane stress piezoelectric quadrilateral 
CPS4I  Quad4  4node bilinear plane stress quadrilateral, incompatible modes 
CPS4R  Quad4  4node bilinear plane stress quadrilateral, reduced integration, hourglass control 
CPS4T  Quad4  4node plane stress thermally coupled quadrilateral, bilinear displacement and temperature 
CPS6  Tria6  6node quadratic plane stress triangle 
CPS6M  Tria6  6node modified secondorder plane stress triangle, hourglass control 
CPS8  Quad8  8node biquadratic plane stress quadrilateral 
CPS8R  Quad8  8node biquadratic plane stress quadrilateral, reduced integration 
DASHPOT1  Mass  Dashpot between a node and ground, acting in a fixed direction 
DASHPOT2  Spring  Dashpot between two nodes, acting in a fixed direction 
DASHPOTA  Spring  Axial dashpot between two nodes, whose line of action is the line joining the two nodes 
DC1D2  Bar2  2node heat transfer link 
DC1D3  Bar3  3node heat transfer link 
DC2D3  Tria3  3node linear heat transfer triangle 
DC2D3E  Tria3  3node linear coupled thermalelectrical triangle 
DC2D4  Quad4  4node linear heat transfer quadrilateral 
DC2D4E  Quad4  4node linear coupled thermalelectrical quadrilateral 
DC2D6  Tria6  6node quadratic heat transfer triangle 
DC2D6E  Tria6  6node quadratic coupled thermalelectrical triangle 
DC2D8  Quad8  8node quadratic heat transfer quadrilateral 
DC2D8E  Quad8  8node quadratic coupled thermalelectrical quadrilateral 
DC3D10  Tetra10  10node quadratic heat transfer tetrahedron 
DC3D10E  Tetra10  10node quadratic coupled thermalelectrical tetrahedron 
DC3D15  Penta15  15node quadratic heat transfer triangular prism 
DC3D15E  Penta15  15node quadratic coupled thermalelectrical triangular prism 
DC3D20  Hex20  20node quadratic heat transfer brick 
DC3D20E  Hex20  20node quadratic coupled thermalelectrical brick 
DC3D4  Tetra4  4node linear heat transfer tetrahedron 
DC3D4E  Tetra4  4node linear coupled thermalelectrical tetrahedron 
DC3D6  Penta6  6node linear heat transfer triangular prism 
DC3D6E  Penta6  6node linear coupled thermalelectrical triangular prism 
DC3D8  Hex8  8node linear heat transfer brick 
DC3D8E  Hex8  8node linear coupled thermalelectrical brick 
DCAX3  Tria3  3node linear axisymmetric heat transfer triangle 
DCAX3E  Tria3  3node linear axisymmetric coupled thermalelectrical triangle 
DCAX4  Quad4  4node linear axisymmetric heat transfer quadrilateral 
DCAX4E  Quad4  4node linear axisymmetric coupled thermalelectrical quadrilateral 
DCAX6  Tria6  6node quadratic axisymmetric heat transfer triangle 
DCAX6E  Tria6  6node quadratic axisymmetric coupled thermalelectrical triangle 
DCAX8  Quad8  8node quadratic axisymmetric heat transfer quadrilateral 
DCAX8E  Quad8  8node quadratic axisymmetric coupled thermalelectrical quadrilateral 
DCC3D8  Hex8  8node convection/diffusion brick 
DCC3D8D  Hex8  8node convection/diffusion brick, dispersion control 
DCCAX4  Quad4  4node axisymmetric convection/diffusion quadrilateral 
DCCAX4D  Quad4  4node axisymmetric convection/diffusion quadrilateral, dispersion control 
DCOUP2D  rbe3  Twodimensional distributing coupling element 
DCOUP3D  rbe3  Threedimensional distributing coupling element 
DS3  Tria3  3node heat transfer triangular shell 
DS4  Quad4  4node heat transfer quadrilateral shell 
DS6  Tria6  6node heat transfer triangular shell 
DS8  Quad8  8node heat transfer quadrilateral shell 
EC3D8R  Hex8  
EC3D8RT  Hex8  
ELBOW31  Bar2  2node pipe in space with deforming section, linear interpolation along the pipe 
ELBOW31B  Bar2  2node pipe in space with ovalization only, axial gradients of ovalization neglected 
ELBOW31C  Bar2  2node pipe in space with ovalization only, axial gradients of ovalization neglected 
ELBOW32  Bar3  3node pipe in space with deforming section, quadratic interpolation along the pipe 
F2D2  Bar2  
F3D3  Tria3  3node linear 3D triangular hydrostatic fluid element 
F3D4  Quad4  4node linear 3D quadrilateral hydrostatic fluid element 
FAX2  Bar2  2node linear axisymmetric hydrostatic fluid element 
FC3D4  Tetra4  
FC3D5  Pyramid5  
FC3D6  Penta6  
FC3D8  Hex8  
GAPCYL  Gap  Cylindrical gap between two nodes 
GAPSPHER  Gap  Spherical gap between two nodes 
GAPUNI  Gap  Unidirectional gap between two nodes 
GK2D2  Rod  2node twodimensional gasket element 
GK2D2N  Rod  2node twodimensional gasket element with thicknessdirection behavior only 
GK3D12M  Penta6  12node threedimensional gasket element 
GK3D12MN  Penta6  12node threedimensional gasket element with thicknessdirection behavior only 
GK3D18  Hex8  18node threedimensional gasket element 
GK3D18N  Hex8  18node threedimensional gasket element with thicknessdirection behavior only 
GK3D2  Bar2  2node threedimensional gasket element 
GK3D2N  Bar2  2node threedimensional gasket element with thicknessdirection behavior only 
GK3D4L  Quad4  4node threedimensional line gasket element 
GK3D4LN  Quad4  4node threedimensional line gasket element with thicknessdirection behavior only 
GK3D6  Penta6  6node threedimensional gasket element 
GK3D6N  Penta6  6node threedimensional gasket element with thicknessdirection behavior only 
GK3D8  Hex8  8node threedimensional gasket element 
GK3D8N  Hex8  8node threedimensional gasket element with thicknessdirection behavior only 
GKPE4  Quad4  4node plane strain gasket element 
GKPS4  Quad4  4node plane stress gasket element 
GKPS4N  Quad4  4node twodimensional gasket element with thicknessdirection behavior only 
HMCONN  Mass  
ITS  
ITSCYL  Rod  Cylindrical geometry tube support interaction element 
ITSUNI  Rod  Unidirectional tube support interaction element 
ITT21  Mass  Tubetube element for use with firstorder, 2D beam and pipe elements 
ITT31  Mass  Tubetube element for use with firstorder, 3D beam and pipe elements 
JOINTC  Spring  Threedimensional joint interaction element 
KINCOUP  Rigid  
LINK  Rigid  
M3D3  Tria3  3node triangular membrane 
M3D4  Quad4  4node quadrilateral membrane 
M3D4R  Quad4  4node quadrilateral membrane, reduced integration, hourglass control 
M3D6  Tria6  6node triangular membrane 
M3D8  Quad8  8node quadrilateral membrane 
M3D8R  Quad8  8node quadrilateral membrane, reduced integration 
MASS  Mass  Point mass 
MGAX1  Rod  2node linear axisymmetric membrane, twist 
MGAX2  Bar3  3node quadratic axisymmetric membrane, twist 
PC3D  Mass  
PIN  Rigid  
PIPE21  Bar2  2node linear pipe in a plane 
PIPE21H  Bar2  2node linear pipe in a plane, hybrid formulation 
PIPE22  Bar3  3node quadratic pipe in a plane 
PIPE22H  Bar3  3node quadratic pipe in a plane, hybrid formulation 
PIPE31  Bar2  2node linear pipe 
PIPE31H  Bar2  2node linear pipe in space, hybrid formulation 
PIPE32  Bar3  3node quadratic pipe in space 
PIPE32H  Bar3  3node quadratic pipe in space, hybrid formulation 
R2D2  Rigid  
R3D3  Tria3  3node 3D rigid triangular facet 
R3D4  Quad4  4node 3D bilinear rigid quadrilateral 
RAX2  Rigid  
RB2D2  Rigid  
RB3D2  Rigid  2node 3D rigid beam 
RDE 

2node linear axisymmetric rigid link (for use in axisymmetric planar geometries) 
ROTARYI  Mass  Rotary inertia at a point 
S3  Tria3  3node triangular generalpurpose shell, finite membrane strains 
S3R  Tria3  3node triangular generalpurpose shell, finite membrane strains 
S3RS  Tria3  
S3RT  Tria3  3node thermally coupled triangular generalpurpose shell, finite membrane strains 
S4  Quad4  4node generalpurpose shell, finite membrane strains 
S4R  Quad4  4node generalpurpose shell, reduced integration, hourglass control, finite membrane strains 
S4R5  Quad4  4node thin shell, reduced integration, hourglass control, using five degrees of freedom per node 
S4RS  Quad4  
S4RSW  Quad4  
S4RT  Quad4  4node thermally coupled generalpurpose shell, reduced integration, hourglass control, finite membrane strains 
S4T  Quad4  4node thermally coupled generalpurpose shell, finite membrane strains 
S8R  Quad8  8node doubly curved thick shell, reduced integration 
S8R5  Quad8  8node doubly curved thin shell, reduced integration, using five degrees of freedom per node 
S8RT  Quad8  8node thermally coupled quadrilateral general thick shell, biquadratic displacement, bilinear temperature in the shell surface 
SAX1  Bar2  2node linear axisymmetric thin or thick shell 
SAX2  Bar3  3node quadratic axisymmetric thin or thick shell 
SC6R  Penta6  6node triangular inplane continuum shell wedge, generalpurpose continuum shell, finite membrane strains 
SC6RT  Penta6  6node linear displacement and temperature, triangular inplane continuum shell wedge, generalpurpose continuum shell, finite membrane strains 
SC8R  Hex8  8node quadrilateral inplane generalpurpose continuum shell, reduced integration with hourglass control, finite membrane strains 
SC8RT  Hex8  8node linear displacement and temperature, quadrilateral inplane generalpurpose continuum shell, reduced integration with hourglass control, finite membrane strains 
SFM3D3  Tria3  3node triangular surface element 
SFM3D4  Quad4  4node quadrilateral surface element 
SFM3D4R  Quad4  4node quadrilateral surface element, reduced integration 
SFM3D6  Tria6  6node triangular surface element 
SFM3D8  Quad8  8node quadrilateral surface element 
SFM3D8R  Quad8  8node quadrilateral surface element, reduced integration 
SFMAX1  Rod  2node linear axisymmetric surface element 
SFMAX2  Bar3  3node quadratic axisymmetric surface element 
SFMGAX1  Rod  2node linear axisymmetric surface element, twist 
SFMGAX2  Bar3  3node quadratic axisymmetric surface element, twist 
SPRING1  Mass  Spring between a node and ground, acting in a fixed direction 
SPRING2  Spring  Spring between two nodes, acting in a fixed direction 
SPRINGA  Spring  Axial spring between two nodes, whose line of action is the line joining the two nodes 
STRI3  Tria3  3node triangular facet thin shell 
STRI65  Tria6  6node triangular thin shell, using five degrees of freedom per node 
T2D2  Rod  2node linear 2D truss 
T2D2E  Rod  2node 2D piezoelectric truss 
T2D2H  Rod  2node linear 2D truss, hybrid 
T2D2T  Rod  2node 2D thermally coupled truss 
T2D3  Rod  3node quadratic 2D truss 
T3D2  Rod  2node linear 3D truss 
T3D2E  Rod  2node 3D piezoelectric truss 
T3D2H  Rod  2node linear 3D truss, hybrid 
T3D2T  Rod  2node 3D thermally coupled truss 
TIE  Rigid 
ANSYS Cards
Card  Supported Element Configurations  Description 

BEAM3  Bar2  2D Elastic Beam Config 60, Type 2 
BEAM4  Bar2  3D Elastic Beam Config 60, Type 1 
BEAM23  Bar2  2D Plastic Beam Config 60, Type 9 
BEAM24  Bar2  3D Thinwalled Beam Config 60, Type 6 
BEAM44  Bar2  3D Elastic Tapered Unsymmetric Beam Config 60, Type 7 
BEAM54  Bar2  2D Elastic Tapered Unsymmetric Beam Config 60, Type 10 
BEAM188  Bar2  3D Linear Finite Strain Beam Config 60, Type 8 
BEAM189  Bar3  3D Quadratic Finite Strain Beam Config 63, Type 1 
CERIG  Rigid  Ldof, Ldof2, Ldof3, Ldof4, Ldof5 Config 5, Type 1, 2 
CIRCU124  Rod  General circuit element applicable to circuit simulation. 
COMBIN14  Spring  SpringDamper Config 21, Type 1 
COMBIN39  Spring  Nonlinear Spring Config 21, Type 2 
COMBIN40  Spring  Combination Config 21, Type 3 
CONTA171  Plot  2D 2Node SurfacetoSurface Contact Config 2, Type 3 
CONTA172  Bar3  2D 3Node SurfacetoSurface Contact Config 63, Type 12 
CONTA173 

3D 4Node SurfacetoSurface Contact

CONTA174 

3D 8Node SurfacetoSurface Contact

CONTA175  Mass  2D/3D NodetoSurface Contact Config 1, Type 14 
CONTA177 

3D LinetoSurface Contact 
CONTA178  Gap  3D NodetoNode Contact Config 70, Type 3 
CONTAC12  Gap  2D PointtoPoint Contact Config 70, Type 2 
CONTAC48  Tria3  
CONTAC49 


CONTAC52  Gap  3D PointtoPoint Contact Config 70, Type 1 
CP  Rigid  Defines (or modifies) a set of coupled degrees of
freedom. Config 55, Type 1, 2 
CP_ELEC  Rigid  
CP_STRUC  Rigid  
CP_THERM  Rigid  
ELBOW290  Bar3  
FLUID29 

2D Axisymmetric Harmonic Acoustic Fluid 
FLUID30 

3D Acoustic Fluid 
FLUID80  Hex8  3D Contained Fluid Config 208, Type 9 
FLUID116  Rod  Coupled ThermalFluid Pipe Config 61, Type 12 
FLUID220 


FLUID221  Tetra10  
HF118 

2D HighFrequency Quadrilateral Solid

HF119  Tetra10  3D HighFrequency Tetrahedral Solid Config 210, Type 11 
HF120 

3D HighFrequency Brick Solid

HYPER58 

3D 8Node Mixed uP Hyperelastic Solid

INFIN9  Rod  
INFIN110 


INTER192 


INTER193  Quad8  
INTER194 


INTER195 


INTER205 


LINK1  Rod  2D Spar (or Truss) Config 61, Type 5 
LINK8  Rod  3D Spar (or Truss) Config 61, Type 1 
LINK10  Rod  Tensiononly or Compressiononly Spar Config 61, Type 2 
LINK11  Bar2  Linear actuator Config 61, Type 25 
LINK31  Rod  Radiation Link Config 61, Type 6 
LINK32  Rod  2D Conduction Bar Config 61, Type 7 
LINK33  Rod  3D Conduction Bar Config 61, Type 8 
LINK34  Rod  Convection Link Config 61, Type 9 
LINK68  Rod  Coupled ThermalElectric Line Config 61, Type 14 
LINK180  Rod  3D Finite Strain Spar (or Truss) Config 61, Type 11 
MASS21  Mass  Structural Mass Config 1, Type 1 
MASS71  Mass  Thermal Mass Config 1, Type 2 
MESH200 

Meshing Facet

MPC184  Rod  Multipoint Constraint Elements: Rigid Link, Rigid Beam,
Slider, Spherical, Revolute, Universal Config 61, Type 13 
PIPE16  Bar2  Elastic Straight Pipe Config 60, Type 3 
PIPE18  Bar2  Elastic Curved Pipe (Elbow) Config 60, Type 4 
PIPE20  Rod  Plastic Straight Pipe Config 61, Type 4 
PIPE60  Bar2  Plastic Curved Pipe (Elbow) Config 60, Type 5 
PIPE288  Bar2  
PIPE289  Bar3  
PLANE2  Tria6  2D 6Node Triangular Structural Solid Config 106, Type 21 
PLANE13 

2D CoupledField Solid

PLANE25 

AxisymmetricHarmonic 4Node Structural Solid

PLANE35  Tria6  2D 6Node Triangular Thermal Solid Config 106, Type 7 
PLANE42 

2D Structural Solid

PLANE53 

2D 8Node Magnetic Solid

PLANE55 

2D Thermal Solid

PLANE67 

2D Coupled ThermalElectric Solid

PLANE75 

AxisymmetricHarmonic 4Node Thermal Solid

PLANE77 

2D 8Node Thermal Solid

PLANE78 

AxisymmetricHarmonic 8Node Thermal Solid

PLANE82 

2D 8Node Structural Solid

PLANE83 

AxisymmetricHarmonic 8Node Structural Solid

PLANE121 

2D 8Node Electrostatic Solid

PLANE145 

2D Quadrilateral Structural Solid pElement

PLANE146  Tria6  Config 106, Type 31 
PLANE162 

Explicit 2D Structural Solid

PLANE182 

2D 4Node Structural Solid

PLANE183 

2D 8Node Structural Solid

PLANE223 

2D 8Node CoupledField Solid 
PRETS179  Bar2  Define a 2D or 3D pretension section within a meshed
structure. Config 60, Type 17 
RBE3  RBE3  Distributes the force/moment applied at the main node to a set of secondary nodes, taking into account the geometry of the secondary nodes as well as weighting factors. 
SHELL28  Quad4  Shear/Twist Panel Config 104, Type 12 
SHELL41 

Membrane Shell

SHELL43 

4Node Plastic Large Strain Shell

SHELL51  Bar2  Axisymmetric Structural Shell Config 60, Type 14 
SHELL57 

Thermal Shell

SHELL61  Bar2  AxisymmetricHarmonic Structural Shell Config 60, Type 15 
SHELL63 

Elastic Shell

SHELL91 

Nonlinear Layered Structural Shell

SHELL93 

8Node Structural Shell

SHELL99 

Linear Layered Structural Shell

SHELL131 

4Node Layered Thermal Shell

SHELL132 

8Node Layered Thermal Shell

SHELL143 

4Node Plastic Small Strain Shell

SHELL150 

8Node Structural Shell pElement

SHELL157 

ThermalElectric Shell

SHELL163 

Explicit Thin Structural Shell

SHELL181 

4Node Finite Strain Shell

SHELL208  Bar2  2Node Finite Strain Axisymmetric Shell 
SHELL209  Bar2  3Node Finite Strain Axisymmetric Shell 
SHELL281 

8Node Finite Strain Shell 
SOLID5 

3D CoupledField Solid

SOLID45 

3D Structural Solid

SOLID46 

3D 8Node Layered Structural Solid

SOLID62 

3D MagnetoStructural Solid

SOLID64 

3D Anisotropic Structural Solid

SOLID69 

3D Coupled ThermalElectric Solid

SOLID70 

3D Thermal Solid

SOLID72  Tetra4  
SOLID73 


SOLID87  Tetra10  3D 10Node Tetrahedral Thermal Solid Config 210, Type 5 
SOLID90 

3D 20Node Thermal Solid

SOLID92  Tetra10  3D 10Node Tetrahedral Structural Solid Config 210, Type 3 
SOLID95 

3D 20Node Structural Solid

SOLID96 

3D Magnetic Scalar Solid

SOLID97 

3D Magnetic Solid

SOLID98  Tetra10  Tetrahedral CoupledField Solid Config 210, Type 4 
SOLID117 

3D 20Node Magnetic Solid

SOLID147 

3D Brick Structural Solid pElement 
SOLID148 

3D Tetrahedral Structural Solid pElement

SOLID164 

Explicit 3D Structural Solid

SOLID168  Tetra10  Explicit 3D 10Node Tetrahedral Structural Solid 
SOLID185 

3D 8Node Structural Solid

SOLID186 

3D 20Node Structural Solid

SOLID187  Tetra10  3D 10Node Tetrahedral Structural Solid Config 210, Type 6 
SOLID191 

3D 20Node Layered Structural Solid

SOLID226 

3D 20Node CoupledField Solid 
SOLID227  Tetra10  3D 10Node CoupledField Solid 
SOLID236 

3D 20Node element capable of modeling electromagnetic fields. The element has magnetic and electric degrees of freedom. 
SOLID278 


SOLID279 


SOLID285  Tetra4  
SOLSH190 

3D 8Node Layered Solid Shell

SURF151  Bar2  2D Thermal Surface Effect Config 60, Type 12 
SURF152 

3D Thermal Surface Effect

SURF153 

2D Structural Surface Effect

SURF154 

3D Structural Surface Effect

SURF156  Bar3  3D Structural Surface Line Load Effect 
SURF251  Rod  2D Radiosity Surface Config 61, Type 25 
SURF252 

3D Radiosity Surface

TARGE169 

2D Target Segment

TARGE170 

3D Target Segment

VISCO88 

2D 8Node Viscoelastic Solid 
VISCO107 

3D 8Node Viscoplastic Solid

EXODUS Cards
Card  Supported Element Configurations  Description 

BEAM  bar2  
BEAM2  bar2  
BEAM3  bar3  
CIRCLE  mass  
HEX20  hex20  
HEX8  hex8  
PYRAMID13  pyramid13  
PYRAMID5  pyramid5  
QUAD4  quad4  
QUAD8  quad8  
RBAR  weld  
RJOINT  rigid  
RROD  rigid  
SHELL3  tria3  
SHELL4  quad4  
SHELL6  tria6  
SHELL8  quad8  
SPHERE  mass  
SPRING  spring  
TETRA10  tetra10  
TETRA4  tetra4  
TRI3  tria3  
TRI6  tria6  
TRIANGLE3  tria3  
TRIANGLE6  tria6  
TRUSS  rod  
WEDGE15  penta15  
WEDGE6  penta6 
LSDYNA Cards
Card  Supported Element Configurations  Description 

*CONSTRAINED_GENERALIZED_WELD_BUTT_(ID)  Rigid  Define butt welds. Spot(default)/type 1, Fillet/type 2, and Butt/type 3 failure modes are supported. Failure information is based on weld type selected. Coordinate System ID can be selected. No Failure/Type 0 Card 36 entities are defined as *CONSTRAINED_NODAL_RIGID_BODIES in Keyword. They are a separate element type. 
*CONSTRAINED_GENERALIZED_WELD_COMBINED_(ID)  Rigid  Define combined welds. 
*CONSTRAINED_GENERALIZED_WELD_CROSS_FILLET_(ID)  Rigid  Define cross fillet welds. 
*CONSTRAINED_GENERALIZED_WELD_FILLET_(ID)  Rigid  Define fillet welds. 
*CONSTRAINED_GENERALIZED_WELD_SPOT_(ID)  Rigid  Define spot welds. 
*CONSTRAINED_INTERPOLATION  RBE3  Define an interpolation constrain. 
*CONSTRAINED_JOINT_CONSTANT_VELOCITY  Joint  
*CONSTRAINED_JOINT_CYLINDRICAL  Joint  Define a joint between two rigid bodies. 
*CONSTRAINED_JOINT_CYLINDRICAL_FAILURE(ID)  Joint  
*CONSTRAINED_JOINT_CYLINDRICAL_LOCAL(ID)  Joint  
*CONSTRAINED_JOINT_CYLINDRICAL_LOCAL_FAILURE(ID)  Joint  
*CONSTRAINED_JOINT_GEARS  Joint  
*CONSTRAINED_JOINT_LOCKING(ID)  Joint  
*CONSTRAINED_JOINT_LOCKING_FAILURE(ID)  Joint  
*CONSTRAINED_JOINT_LOCKING_LOCAL(ID)  Joint  
*CONSTRAINED_JOINT_LOCKING_LOCAL_FAILURE(ID)  Joint  
*CONSTRAINED_JOINT_PLANAR(ID)  Joint  
*CONSTRAINED_JOINT_PLANAR_FAILURE(ID)  Joint  
*CONSTRAINED_JOINT_PLANAR_LOCAL(ID)  Joint  
*CONSTRAINED_JOINT_PLANAR_FAILURE_LOCAL(ID)  Joint  
*CONSTRAINED_JOINT_PULLY  Joint  
*CONSTRAINED_JOINT_RACK_AND_PINION_ID  Joint  
*CONSTRAINED_JOINT_REVOLUTE  Joint  
*CONSTRAINED_JOINT_REVOLUTE_LOCAL(ID)  Joint  
*CONSTRAINED_JOINT_REVOLUTE_FAILURE(ID)  Joint  
*CONSTRAINED_JOINT_REVOLUTE_LOCAL_FAILURE(ID)  Joint  
*CONSTRAINED_JOINT_ROTATIONAL_MOTOR  Joint  
*CONSTRAINED_JOINT_SCREW  
*CONSTRAINED_JOINT_SPHERICAL(ID)  Joint  
*CONSTRAINED_JOINT_SPHERICAL_LOCAL(ID)  Joint  
*CONSTRAINED_JOINT_SPHERICAL_FAILURE(ID)  Joint  
*CONSTRAINED_JOINT_SPHERICAL_LOCAL_FAILURE(ID)  Joint  
*CONSTRAINED_JOINT_STIFFNESS_TRANSLATIONAL  Joint  Define optional rotational and translational joint stiffness for joints defined by *CONSTRAINED_JOINT_OPTION. 
*CONSTRAINED_JOINT_TRANSLATIONAL(ID)  Joint  
*CONSTRAINED_JOINT_TRANSLATIONAL_FAILURE(ID)  Joint  
*CONSTRAINED_JOINT_TRANSLATIONAL_LOCAL(ID)  Joint  
*CONSTRAINED_JOINT_TRANSLATIONAL_LOCAL_FAILURE(ID)  Joint  
*CONSTRAINED_JOINT_TRANSLATIONAL_MOTOR  Joint  
*CONSTRAINED_JOINT_UNIVERSAL(ID)  Joint  
*CONSTRAINED_JOINT_UNIVERSAL_FAILURE(ID)  Joint  
*CONSTRAINED_JOINT_UNIVERSAL_LOCAL(ID)  Joint  
*CONSTRAINED_JOINT_UNIVERSAL_LOCAL_FAILURE(ID)  Joint  
*CONSTRAINED_NODAL_RIGID_BODY  Rigid  Define a nodal rigid body. 
*CONSTRAINED_NODAL_RIGID_BODY (2Noded)  Rigid  
*CONSTRAINED_NODAL_RIGID_BODY_INERTIA  Rigid  Used when inertial properties are defined rather than computed. 
*CONSTRAINED_NODAL_RIGID_BODY_INERTIA (2Noded)  Rigid  
*CONSTRAINED_NODAL_RIGID_BODY_INERTIA _SPC  Rigid  
*CONSTRAINED_NODAL_RIGID_BODY_INERTIA _SPC (2Noded)  Rigid  
*CONSTRAINED_NODAL_RIGID_BODY_SPC  Rigid  
*CONSTRAINED_NODAL_RIGID_BODY_SPC (2Noded)  Rigid  
*CONSTRAINED_NODE_SET  Rigid  Define nodal constraint sets for translational motion in global coordinates. 
*CONSTRAINED_NODE_SET (2Noded)  Rigid  
*CONSTRAINED_NODE_SET_ID  Rigid  
*CONSTRAINED_RIVET  Weld  Define massless rivets between noncontiguous nodal pairs. 
*CONSTRAINED_SHELL_TO_SOLID  Rigid  Define a tie between a shell edge and solid elements. 
*CONSTRAINED_SPOTWELD_ID  Weld  Define massless spot welds between noncontiguous nodal
pairs. Normal and shear failure values can be edited. 
*CONSTRAINED_SPOTWELD_FILTERED_FORCE_ID  Weld  
*ELEMENT_BEAM  Bar  Define two node elements including 3D beams, trusses, 2D
axisymmetric shells and 2D plane strain beam
elements. Thickness option can be added. This allows you to edit the parameters based on the element formulation in the property to which the beam points. 
*ELEMENT_BEAM_OFFSET  Bar  
*ELEMENT_BEAM_OFFSET_PID  Bar  
*ELEMENT_BEAM_OFFSET_THICKNESS  Bar  
*ELEMENT_BEAM_ORIENTATION  Bar  
*ELEMENT_BEAM_PID  Bar  
*ELEMENT_BEAM_PID_ORIENTATION  Bar  
*ELEMENT_BEAM_PID_SCALAR  Bar  
*ELEMENT_BEAM_SCALAR  Bar  
*ELEMENT_BEAM_SCALAR_ORIENTATION  Bar  
*ELEMENT_BEAM_SECTION  Bar  
*ELEMENT_BEAM_SECTION_ORIENTATION  Bar  
*ELEMENT_BEAM_SECTION_PID  Bar  
*ELEMENT_BEAM_THICKNESS  Bar  
*ELEMENT_BEAM_THICKNESS_ORIENTATION  Bar  
*ELEMENT_BEAM_THICKNESS_PID  Bar  
*ELEMENT_BEAM_THICKNESS_SCALAR  Bar  
*ELEMENT_DISCRETE  Spring  Define a discrete (spring or damper) element between two
nodes or a node and ground. Scale factor, printing flags, and offset values can be edited. 
*ELEMENT_INERTIA  Mass  Define a lumped inertia element assigned to a nodal point. 
*ELEMENT_INERTIA_OFFSET  Mass  
*ELEMENT_MASS  Mass  Define a lumped mass element assigned to a nodal point or equally distributed to the nodes of a node set. 
*ELEMENT_MASS_NODE_SET  Mass  Mass elements defined on node set 
*ELEMENT_MASS_PART  Mass  Define additional nonstructural mass to be distributed by an area weighted distribution to all nodes of a given part ID. 
*ELEMENT_MASS_PART_SET  Mass  Mass elements defined on part set. 
*ELEMENT_PLOTEL  Plot  Define a null beam element for visualization. 
*ELEMENT_SEATBELT  Rod  Define a seat belt element. 
*ELEMENT_SEATBELT_SENSOR  Sensors  Define seat belt sensor. 
*ELEMENT_SHELL 

Define three, four, six and eight node elements including 3D
shells, membranes, 2D plane stress, plane strain, and
axisymmetric solids. Thickness and beta options can be added singularly or together. This allows you to edit the thickness and material angles to override the SECTION card. 
*ELEMENT_SHELL_BETA 


*ELEMENT_SHELL_BETA_OFFSET 


*ELEMENT_SHELL_COMPOSITE 


*ELEMENT_SHELL_DOF 


*ELEMENT_SHELL_MCID 


*ELEMENT_SHELL_MCID_OFFSET 


*ELEMENT_SHELL_OFFSET 


*ELEMENT_SHELL_THICKNESS 


*ELEMENT_SHELL_THICKNESS_BETA 


*ELEMENT_SHELL_THICKNESS_BETA_OFFSET 


*ELEMENT_SHELL_THICKNESS_MCID 


*ELEMENT_SHELL_THICKNESS_MCID_OFFSET 


*ELEMENT_SHELL_THICKNESS_OFFSET 


*ELEMENT_SOLID 

Define threedimensional solid elements including 4 noded tetrahedrons and 8noded hexahedrons. 
*ELEMENT_SOLID_ORTHO 

Define a local coordinate system for orthotropic and anisotropic materials. 
*ELEMENT_SOLID_TET4TOTET10  Tetra4  Converts 4 node tetrahedron solids to 10 node quadratic tetrahedron solids. 
*ELEMENT_SPH  Mass  Define a lumped mass element assigned to a nodal point 
*ELEMENT_TSHELL 

Define an eight node thick shell element which is available with either fully reduced or selectively reduced integration rules. 
*INITIAL_MOMENTUM 

Defines initial momentum in the solid element at the start of
analysis. This momentum could be from previous analysis/step
carried forward to next analysis/step. This is supported as an attribute to an element to maintain its associativity with element inside HM. 
*INITIAL_STRAIN_SHELL 

Defines stress in the shell element at the start of analysis.
This stress could be from previous analysis/step carried forward
to next analysis/step. This is supported as an attribute to an element to maintain its associativity with element inside HM. 
*INITIAL_STRAIN_SOLID 

Defines stress in the solid element at the start of analysis.
This stress could be from previous analysis/step carried forward
to next analysis/step. This is supported as an attribute to an element to maintain its associativity with element inside HM. 
*INITIAL_STRESS_BEAM  Bar  Defines stress in the beam element at the start of analysis.
This stress could be from previous analysis/step carried forward
to next analysis/step. This is supported as an attribute to an element to maintain its associativity with element inside HM. 
*INITIAL_STRESS_SHELL 

Defines stress in the shell element at the start of analysis.
This stress could be from previous analysis/step carried forward
to next analysis/step. This is supported as an attribute to an element to maintain its associativity with element inside HM. 
*INITIAL_STRESS_SOLID 

Defines stress in the solid element at the start of analysis.
This stress could be from previous analysis/step carried forward
to next analysis/step. This is supported as an attribute to an element to maintain its associativity with element inside HM. 
Nastran Cards
Card  Supported Element Configurations  Description 

CAABSF 

Defines a frequencydependent acoustic absorber element in coupled fluidstructural analysis. 
CACINF3  Tria3  Defines an acoustic conjugate infinite element with triangular base. 
CACINF4  Quad4  Defines an acoustic conjugate infinite element with quadrilateral base. 
CAERO1  Quad4  Defines an aerodynamic macro element (panel) in terms of two leading edge locations and side chords. This is used for DoubletLattice theory for subsonic aerodynamics and the ZONA51 theory for supersonic aerodynamics. 
CAERO2  Rod  Defines aerodynamic slender body and interference elements for DoubletLattice aerodynamics. 
CBAR  Bar  Defines a simple beam element. 
CBEAM  Bar  Defines a beam element. 
CBEND  Bar  Defines a curved beam, curved pipe, or elbow element. 
CBUSH 

Defines a generalized springanddamper structural element
that may be nonlinear or frequency dependent. Both elements with grounded terminals are supported. 
CBUSH1D 

Defines the connectivity of a onedimensional spring and
viscous damper element. Both elements with grounded terminals are supported. 
CDAMP1 

Defines a scalar damper element. Elements CDAMP1 and CDAMP2 with grounded terminals are not supported. 
CDAMP2 

Defines a scalar damper element without reference to a
material or property entry. Elements CDAMP1 and CDAMP2 with grounded terminals are not supported. 
CDAMP3 

Defines a scalar damper element that is connected only to
scalar points. Elements CDAMP1 and CDAMP2 with grounded terminals are not supported. 
CDAMP4 

Defines a scalar damper element that connected only to scalar
points and without reference to a material or property
entry. Elements CDAMP1 and CDAMP2 with grounded terminals are not supported. 
CELAS1 

Defines a scalar spring element. Elements CDAMP1 and CDAMP2 with grounded terminals are not supported. 
CELAS2 

Defines a scalar spring element without reference to a
property entry. Elements CDAMP1 and CDAMP2 with grounded terminals are not supported. 
CELAS3 

Defines a scalar spring element that connects only to scalar
points. Elements CDAMP1 and CDAMP2 with grounded terminals are not supported. 
CELAS4 

Defines a scalar spring element that is connected only to
scalar points, without reference to a property entry. Elements CDAMP1 and CDAMP2 with grounded terminals are not supported. 
CFAST 

Defines a fastener with material orientation connecting two surface patches. 
CGAP  Gap  Defines a gap or friction element. 
CHACAB  Hex8  Defines the acoustic absorber element in coupled fluidstructural analysis. 
CHBDYE 

Defines a boundary condition surface element with reference
to a heat conduction element. This element is supported as GROUP. 
CHBDYG 

Defines a boundary condition surface element without
reference to a property entry. This element is supported as GROUP. Creation from scratch is not yet supported. 
CHBDYP 

Defines a boundary condition surface element with reference
to a PHBDY entry. CONVM is supported as a continuation card inside CHBDYP. 
CHEXA (20noded)  Hex20  Defines a second order solid element, composed of 6
quadrilateral faces. In Nastran, you can define a second order element with missing midside nodes. Input data decks containing such elements are read by the translator as a firstorder element. A message is written to the nastran.msg file indicating the corresponding element ID. 
CHEXA (8noded)  Hex8  Defines a first order solid element, composed of 6 quadrilateral faces. 
CMASS1 

Defines a scalar mass element. 
CMASS2 

Defines a scalar mass element without reference to a property entry. 
CMASS3 

Defines a scalar mass element that is connected only to scalar points. 
CMASS4 

Defines a scalar mass element that is connected only to scalar points, without reference to a property entry. 
CONM1  Mass  Defines a 6 x 6 symmetric mass matrix at a geometric grid point. 
CONM2  Mass  Defines a concentrated mass at a grid point. 
CONROD  Rod  Defines a rod element without reference to a property entry. 
CPENTA (6noded)  Penta6  Defines the connections of a fivesided solid element with six to fifteen grid points. 
CPENTA (15noded)  Penta15  Defines the connections of a fivesided solid element with
six to fifteen grid points. In Nastran, you can define a second order element with missing midside nodes. Input data decks containing such elements are read by the translator as a firstorder element. A message is written to the nastran.msg file indicating the corresponding element ID. 
CQUAD4  Quad4  Defines an isoparametric membranebending or plane strain quadrilateral plate element. 
CQUAD8  Quad8  Defines a curved quadrilateral shell or plane strain element
with eight grid points. In Nastran, you can define a second order element with missing midside nodes. Input data decks containing such elements are read by the translator as a firstorder element. A message is written to the nastran.msg file indicating the corresponding element ID. 
CQUADR  Quad4  Defines an isoparametric membrane and bending quadrilateral plate element. However, this element does not include membranebending coupling. This element is less sensitive to initial distortion and extreme values of Poisson’s ratio than the CQUAD4 element. It is a companion to the CTRIAR element. 
CROD  Rod  Defines a tensioncompressiontorsion element. 
CSHEAR  Quad4  Defines a shear panel element. 
CSEAM  Rod  
CTETRA (4noded)  Tetra4  Defines the connections of the foursided solid element with four grid points. 
CTETRA (10noded)  Tetra10  Defines the connections of the foursided solid element with
ten grid points. In Nastran, you can define a second order element with missing midside nodes. Input data decks containing such elements are read by the translator as a firstorder element. A message is written to the nastran.msg file indicating the corresponding element ID. 
CTRIA3  Tria3  Defines an isoparametric membranebending or plane strain triangular plate element. 
CTRIA6  Tria6  Defines a curved triangular shell element or plane strain
with six grid points. In Nastran, you can define a second order element with missing midside nodes. Input data decks containing such elements are read by the translator as a firstorder element. A message is written to the nastran.msg file indicating the corresponding element ID. 
CTRIAR  Tria3  Defines an isoparametric membranebending triangular plate element. However, this element does not include membranebending coupling. It is a companion to the CQUADR element. 
CTRIAX 

Defines an axisymmetric triangular element with up to 6 grid points for use in fully nonlinear (i.e., large strain and large rotations) hyperelastic analysis 
CTRIAX6 

Defines an isoparametric and axisymmetric triangular cross section ring element with midside grid points. 
CTUBE  Rod  Defines a tensioncompressiontorsion tube element. 
CQUADX 

Defines an axisymmetric quadrilateral element with up to nine
grid points for use in fully nonlinear (i.e. large strain and
large rotations) analysis or a linear harmonic or rotor dynamic
analysis. The element has between four and eight grid
points. Ninth grid selected in card edit of the element. 
CVISC  Spring  Defines a viscous damper element. Elements CDAMP1 and CDAMP2 with grounded terminals are not supported. 
CWELD 

Defines a weld or fastener connecting two surface patches or
points. NodeNode, NodePatch, or PatchPatch weld elements can be read. CWELD element is stored as an element of the rod configuration. CWELD elements using the ELEMID option not created in HyperMesh will be displayed as zero length. Currently, the Spotweld panel can only create NodeNode and PatchPatch CWELD elements. HyperMesh always calculates the location of GA and GB by projecting GS in the normal direction of surface patch A and surface patch B, respectively. 
GENEL  RBE3  Defines a general element. 
HM_SPRING  Spring  Defines a spring element, which is converted to Nastran entities on export, in a manner similar to that explained in Using HM_ELAS. 
MBOLT  Mass  Defines a bolt for use in SOL 600 in countries outside the USA. 
MBOLTUS  Mass  Defines a bolt for use only in SOL 600 and only in the USA. 
PLOTEL  Plot  Defines a onedimensional dummy element for use in plotting. 
RBAR  Weld  Defines a rigid bar with six degreesoffreedom at each
end. RBAR CNA field defaults to 123456. To edit the CNA, CNB, CMA, or CMB fields, you must view the card image for the RBAR element. 
RBE2 

Defines a rigid body with independent degreesoffreedom that
are specified at a single grid point and with dependent
degreesoffreedom that are specified at an arbitrary number of
grid points. An RBE2 element with one dependent node is identified as a rigid element, while an element with multiple dependent nodes is identified as a rigid link element. 
RBE3  RBE3  Defines the motion at a reference grid point as the weighted
average of the motions at a set of other grid
points. Individual weight factors can be created on the independent nodes of RBE3 using the update functionality in the RBE3 panel. See the online help for the RBE3 panel for more information. 
RJOINT  Defines a rigid joint element connecting two coinciding grid
points. RBE2 

RROD  Defines a rigid pinended element connection. 
OptiStruct Cards
Card  Supported Element Configurations  Description 

BMFACE 

Defines quad or tria faces that are in turn used to define a barrier to limit the total deformation for freeshape design regions. 
CAABSF 

Defines the frequencydependent fluid acoustic absorber element in coupled fluidstructural analysis. 
CBAR  Bar2  Defines a simple beam element (BAR) of the structural model. 
CBEAM  Bar2  Defines a beam element (BEAM) of the structural model. 
CBUSH  Spring  Defines a generalized springdamper structural element. 
CBUSH1D 

Defines a onedimensional springdamper structural element. 
CDAMP1 

Defines a scalar damper element. Represented as a spring element type or as a mass element type (grounded CDAMP1). 
CDAMP2 

Defines a scalar damper element without reference to a
property entry. Represented as a spring element type or as a mass element type (grounded CDAMP2). 
CDAMP3 

Defines a scalar damper element that is connected only to
scalar points. Represented as a spring element type or as a mass element type (when a coordinate is constrained). 
CDAMP4 

Defines a scalar damper element that is connected only to
scalar points and is without reference to a material or property entry. Represented as a spring element type or as a mass element type (when a coordinate is constrained). 
CELAS1 

Defines a scalar spring element of the structural
model. Represented as a spring element type or as a mass element type (grounded CELAS1). 
CELAS2 

Defines a scalar spring element of the structural model
without reference to a property entry. Represented as a spring element type or as a mass element type (grounded CELAS2). Exported in large field format by optistructlf template. 
CELAS3 

Defines a scalar spring element that connects only to
scalar points. Represented as a spring element type or as a mass element type (when a coordinate is constrained). 
CELAS4 

Defines a scalar spring element that is connected only to
scalar points without reference to a property entry. Represented as a spring element type or as a mass element type (when a coordinate is constrained). 
CFAST 

Define a fastener with material orientation connecting two
shell surfaces. Represented as a mass or rod element type, depending on fastener configuration. 
CGAP  Gap  Defines a gap or friction element. The type of gap elements (either CGAP or CGAPG) is automatically determined based on whether the element is nodetonode or nodetoelem. 
CGAPG 

Defines a nodetoobstacle gap element. The obstacle may be
an element face or a patch of nodes. The type of gap elements (either CGAP or CGAPG) is automatically determined based on whether the element is nodetonode or nodetoelem. 
CGASK6  Penta6  Defining the connections of the GASK6 solid gasket element. 
CGASK8  Hex8  Defining the connections of the GASK8 solid gasket element. 
CGASK12  Penta15  Defining the connections of the GASK12 solid gasket element. 
CGASK16  Hex20  Defining the connections of the GASK16 solid gasket element. 
CHACAB  Hex8  Defines the acoustic absorber element in coupled fluidstructural analysis. 
CHBDYE  Slave1  Defines a surface element for application of thermal
boundary condition. Defined using the Interfacespanel with the CONDUCTION or CONVECTION type. 
CHEXA (8noded)  Hex8  Defines a first order solid element, composed of 6 quadrilateral faces. 
CHEXA (20noded)  Hex20  Defines a second order solid element, composed of 6
quadrilateral faces. A second order element with missing midside nodes can be defined in OptiStruct. Input data decks containing such elements are read by the translator as a firstorder element. A message is written to the OptiStruct.msg file indicating the corresponding element ID. 
CMASS1 

Defines a scalar mass element. Represented as a spring element type or as a mass element type (grounded CMASS1). 
CMASS2 

Defines a scalar mass element without reference to a
property entry. Represented as a spring element type or as a mass element type (grounded CMASS2). 
CMASS3 

Defines a scalar mass element that is connected only to
scalar points. Represented as a spring element type or as a mass element type (when a coordinate is constrained). 
CMASS4 

Defines a scalar mass element that is connected only to
scalar points, without reference to a property entry. Represented as a spring element type or as a mass element type (when a coordinate is constrained). 
CMBEAM  Bar2  Defines a beam element for multibody dynamics solution sequence without reference to a property entry. 
CMBUSH  Spring  Defines a bushing element without reference to a property entry. 
CMBUSHC  Spring  
CMBUSHE  Spring  
CMBUSHT  Spring  
CMSPDP  Spring  Defines a spring damper element without reference to a property entry for multibody solution sequence. 
CMSPDPC  Spring  Defines a spring damper element without reference to a property entry for multibody solution sequence. 
CMSPDPE  Spring  Defines a spring damper element without reference to a property entry for multibody solution sequence. 
CMSPDPT  Spring  Defines a spring damper element without reference to a property entry for multibody solution sequence. 
CONM1  Mass  Defines a 6x6 mass matrix at a geometric grid point. 
CONM2  Mass  Defines a concentrated mass at a grid point of the
structural model. Exported in large field format by optistructlf template. 
CONROD  Rod  Defines a rod element without reference to a property entry. 
CONV  Slave1  Defines a free convection boundary condition for heat
transfer analysis through connection to a surface element (CHBDYE
card). Represented as a continuation to CHBDYE secondary element card. 
CPENTA (6noded)  Penta6  Defines a first order solid element, composed of 3 quadrilateral and 2 triangular faces. 
CPENTA (15noded)  Penta15  Defines a second order solid element, composed of 3
quadrilateral and 2 triangular faces.
A second order element with missing midside nodes can be defined in OptiStruct. Input data decks containing such elements are read by the translator as a firstorder element. A message is written to the OptiStruct.msg file indicating the corresponding element ID. 
CPYRA (5noded)  Pyramid5  Defines a first order solid element, composed of 1 quadrilateral and 4 triangular faces. 
CPYRA (13noded)  Pyramid13  Defines a second order solid element, composed of 1
quadrilateral and 4 triangular faces. A second order element with missing midside nodes can be defined in OptiStruct. Input data decks containing such elements are read by the translator as a firstorder element. A message is written to the OptiStruct.msg file indicating the corresponding element ID. 
CQUADR  Quad4  Equivalent to CQUAD4. Unlike other Nastran codes, a 6 degreeoffreedom per node formulation is used for all shell elements. 
CQUAD4  Quad4  Defines a quadrilateral plate element (QUAD4) of the structural model. This element uses a 6 degreeoffreedom per node formulation. 
CQUAD8  Quad8  Defines a curved quadrilateral shell element with eight grid points. 
CROD  Rod  Defines a tensioncompressiontorsion element (ROD) of the structural model. 
CSHEAR  Quad4  Defines a shear panel element. 
CTAXI  Tria3  Defines an axisymmetric triangular crosssection ring element for use in linear analysis. 
CTETRA (4noded)  Tetra4  Defines a first order solid element, composed of 4 triangular faces. 
CTETRA (10noded)  Tetra10  Defines a second order solid element, composed of 4
triangular faces. A second order element with missing midside nodes can be defined in OptiStruct. Input data decks containing such elements are read by the translator as a firstorder element. A message is written to the OptiStruct.msg file indicating the corresponding element ID. 
CTRIAR  Tria3  CTRIAR entry is equivalent to CTRIA3. Unlike other Nastran codes, a 6 degreesoffreedom per node formulation is used for all shell elements. 
CTRIAX6  Tria6  Defines an axisymmetric triangular crosssection ring element for use in Linear Analysis. 
CTRIA3  Tria3  Defines a triangular plate element (TRIA3) of the structural model. This element uses a 6 degreeoffreedom per node formulation. 
CTRIA6  Tria6  Defines a curved triangular shell element with six grid points. 
CTUBE  Rod  Defines a tensioncompressiontorsion element (TUBE) of the structural model. 
CVISC  Spring  Defines a viscous damper element. Represented as a spring element type. 
CWELD 

Defines a weld or fastener connecting two surface patches
or points. Represented as a rod element type. 
DHEXA8  Hex8  
DQUAD4  Quad4  
DPENTA6  
DTETRAA4  Tetra4  
DTRIA3  Tria3  
HMSPRING  Spring  Defines a spring element, which is converted to OptiStruct entities on export, in a manner similar to that explained in Using HM_ELAS. 
JOINT  Joint  Defines a joint. 
PLOTEL  Plot  Defines a onedimensional dummy element for use in plotting. 
PLOTEL3 

Defines a threenoded, twodimensional dummy element for use in plotting. 
PLOTEL4 

Defines a fournoded, twodimensional dummy element for use in plotting. 
QBDY1  Flux  Defines a uniform heat flux for CHBDYE elements. 
RBAR  Weld  Defines a rigid bar with six degreesoffreedom at each end. 
RBE2 

Defines a rigid body whose independent degreesoffreedom
are specified at a single grid point and whose dependent degreesoffreedom are
specified at an arbitrary number of grid points. An RBE2 element with one dependent node is represented as a rigid element type, while an element with multiple dependent nodes is represented as a rigid link element type. 
RBE3  Rbe3  Defines the motion at a "reference" grid point as the weighted average of the motions at a set of other grid points. 
RROD  Rod  Defines a pinended rod that is rigid in extension. 
PAMCRASH Cards
The component of the element refers to a material, which contains the material definition for PAMCRASH.
Card  Supported Element Configurations  Description 

ASSOCIATE  Rigids  Defines entities to be converted from deformable to rigid. 
BAR /  Rod  Bar element. 
BASE_BODY  Rigid  Rigid bodies on which the boundary conditions are defined, used in Multibody systems. 
BEAM /  Bar2  Beam element. If the orientation vector is defined via vectors, the string VECTOR is displayed in the N3 field, and a zero is written in the exported deck. If the ydirection node is directly specified, its ID is displayed in the N3 field. 
BSHEL /  Hex8  8noded brick shell element. 
EDG  Rod  
ELINK /  Rod  Link element. The element must be edited in the card previewer to define the connections. 
JOINT /  Rod  Joint element. The element must be edited in the card previewer to define element orientation. 
KJOIN /  Rod  Kinematic joint element. The element must be edited in the card previewer to define element orientation. 
LLINK /  Rod  Link element. The element must be edited in the card previewer to define the connections. 
MASS  Mass  Added mass. 
MEMBR / 

Membrane element. 
MTJOIN /  FE Joint  Multiple node to one node Kinematic joint element. 
MTOCO /  Rigid  Rigid element. 
NODCO /  Rigid  Nodal constraint definition. This configuration allows you to create nodal constraints via entity sets. The element must be edited in the card previewer. Degrees of freedom are ignored. 
OTMCO /  RBE3  One node to multiple node constraints. 
PLINK /  Mass  Plink element. The element must be edited in the card
previewer. Mass value is ignored. Use the following
templates to handle the welds:

PLINK_VI  Rod  These elements are created during connector realization to show the actual connections. They are not exported. 
RETRA /  Mass  The element must be edited in the card previewer. Mass value is ignored. 
RBODY /  Weld  Rigid body with 2 nodes. When created, the default value for rigid body type is 1. 
RBODY /  Rigid  This configuration allows you to create rigid bodies via entity sets. The element must be edited in the card previewer. Degrees of freedom are ignored. 
SEG 

The elements are used in entity selection. With this keyword, only nodes of these elements are output along with SEG keyword. 
SENPT /  Mass  
SHELL /  Mass  Shell element. Mass value is ignored. Mass defined with a keyword other than NOD is not supported. The reader creates one mass element for each NOD definition in the MASS card, therefore the exported deck will contain the same number of MASS/cards as many NOD definitions. 
SHELL /  Tria3  The default behavior for tria3 elements is Coo
triangles. To output standard triangles (N3 = N4). 
SHELL /  Quad4  
SLINK / 

The element must be edited in the card previewer to define the connections. 
SLIPR /  Mass  The element must be edited in the card previewer. Mass value is ignored. 
SOLID / 

8noded brick element. 
SPH /  Mass  
SPRING /  Spring  Spring element. The element must be edited in the card previewer to define element orientation. 
SPRGBM /  Spring  Spring beam element. The element must be edited in the card previewer to define element orientation. 
TETRA /  Tetra10  10noded tetra element. Local frame definition. 
TETR4 /  Tetra4  4noded tetra element. 
TSHEL /  Quad4  4noded thick shell element. The element must be edited in the card previewer to define the connections. 
Permas Cards
Card  Supported Element Configurations  Description 

BEAM2  Bar2  2 noded straight general beam 
BECOC  Bar2  2 noded straight thinwalled tube 
BECOP  Bar2  2 noded straight thinwalled tube 
BECOS  Bar2  2 noded straight solid beam 
BETAC  Bar2  2 noded straight tapered thinwalled tube 
BETOP  Bar2  2 noded straight thinwalled open beam 
CA1ZERF3  Spring  Zero Force Element with 1 Node and Three Translational Stiffnesses 
CA2ZERF1  Spring  Translational Zero Force Element with 2 Nodes 
CA2ZERF3  Spring  Zero Force Element with 2 Nodes and Three Translational Stiffnesses 
CONAX2  Bar2  
CONAX3  Bar3  
CONA3  Tria3  3 noded triangular surface convection and radiation element. 
CONA4  Quad4  4 noded quadrilateral surface convection and radiation element. 
CONA6  Tria6  6 noded triangular surface convection and radiation element. 
CONA8  Quad8  8 noded quadrilateral surface convection and radiation element. 
CONS3  Tria3  3 noded triangular shell surface convection and radiation element. 
CONS4  Quad4  4 noded quadrilateral shell surface convection and radiation element. 
CONS6  Tria6  6 noded triangular shell surface convection and radiation element. 
CONS8  Quad8  8 noded quadrilateral shell surface convection and radiation element. 
DAMP1  Spring  Translational viscous damper. 
DAMP3  Spring  Viscous damper for three degrees of freedom. 
DAMP6  Spring  Viscous damper for six degrees of freedom. 
FLA2  Rod  2 noded straight flange (rod). 
FLA3  Bar3  3 noded straight flange (rod). 
FLHEX8  Hex8  8 noded fluid hexahedron. 
FLHEX20  Hex20  20 noded fluid hexahedron. 
FLPENT6  Penta6  6 noded fluid pentahedron. 
FLPENT15  Penta15  15 noded fluid pentahedron. 
FLPYR5  Pyramid5  5 noded fluid pyramid. 
FLTET4  Tetra4  4 noded fluid tetrahedron. 
FLTET10  Tetra10  10 noded fluid tetrahedron. 
FSINTA3  Tria3  3 noded triangular fluid structure interface element. 
FSINTA4  Quad4  4 noded quadrilateral fluid structure interface element. 
FSINTA6  Tria6  6 noded triangular fluid structure interface element. 
FSINTA8  Quad8  8 noded quadrilateral fluid structure interface element. 
GKHEX8  Hex8  8 noded solid hexahedron. 
GKHEX20  Hex20  20 noded solid hexahedron. 
GKPNT6  Penta6  6 noded solid pentahedron. 
GKPNT15  Penta15  15 noded solid pentahedron. 
HEXE8  Hex8  8 noded solid hexahedron. 
HEXE20  Hex20  20 noded solid hexahedron. 
LOADA3  Tria3  3 node triangular load carrying membrane element. 
LOADA4  Quad4  4 node quadrilateral load carrying membrane element. 
LOADA6  Tria6  6 node triangular load carrying membrane element. 
LOADA8  Quad8  8 node quadrilateral load carrying membrane element. 
MASS3  Mass  Point mass. 
MASS6  Mass  Rigid mass. 
$MPC ASSIGN  Rigid  Dependent nodes are forced to have the same displacement as an independent node. User can specify degrees of freedom for dependent and independent nodes. 
$MPC JOIN  Rigid  Pairwise identical displacements. 
$MPC RIGID  Rigid  Rigid regions. 
$MPC SAME  Rigid  Identical corresponding displacements. 
$MPC WLSCON  RBE3  Weighted averaged connection. 
MPC_IQUAD4  RBE3 
Quadrilateral Interpolation Surface 
MPC_IQUAD8  RBE3 
Quadrilateral Interpolation Surface 
MPC_IQUAD9  RBE3 
Quadrilateral Interpolation Surface 
MPC_ITRIA3  RBE3 
Triangular Interpolation Surface 
MPC_ITRIA6  RBE3 
Triangular Interpolation Surface 
NLDAMP  Spring  Nonlinear translational viscous damper. 
NLDAMPR  Spring  Nonlinear rotational viscous damper. 
NLSTIFF  Spring  Nonlinear translational spring. 
NLSTIFFR  Spring  Nonlinear rotational spring. 
PENTA6  Penta6  6 noded solid pentahedron. 
PENTA15  Penta15  15 noded solid pentahedron. 
PLOTA3  Tria3  3 noded triangular plot element. 
PLOTA4  Quad4  4 noded quadrilateral plot element. 
PLOTA6  Tria6  6 noded triangular plot element. 
PLOTA8  Quad8  8 noded quadrilateral plot element. 
PLOTL2  Plot  2 noded straight line plot element. 
PLOTL3  Bar3  3 noded straight line plot element. 
PYRA5  Pyramid5  5 noded solid pyramid. 
QUAD4  Quad4  4 noded quadrilateral shell element. 
QUAD4S  Quad4  
QUAM4  Quad4  4 noded quadrilateral plane membrane element. 
QUAM8  Quad8  8 noded quadrilateral plane membrane element 
QUAMS4  Quad4  4 noded quadrilateral solid shell element 
QUAMS8  Quad8  8 noded quadrilateral solid shell element 
QUAX4  Quad4  4 noded quadrilateral axisymmetric solid element 
QUAX8  Quad8  8 noded quadrilateral axisymmetric solid element 
SHEAR4  Quad4  4 noded quadrilateral plane shear panel element. 
SHELL3  Tria3  3 noded triangular shell element for laminates. 
SHELL4  Quad4  4 noded quadrilateral shell element for laminates. 
SPRINGX1  Spring  
SPRINGX2  Spring  
SPRINGX3  Spring  
SPRING1  Spring  Translational spring. 
SPRING3  Spring  Spring with three translational stiffnesses 
SPRING6  Spring  Spring with three translational and three rotational stiffnesses. 
TET4  Tetra4  4 noded solid tetrahedron. 
TET10  Tetra10  10 noded solid tetrahedron. 
TRIA3  Tria3  3 noded triangular shell element. 
TRIA3K  Tria3  3 noded triangular thin shell element. 
TRIA3S  Tria3 
Axisymmetric Solid Element, 3 Noded Triangular Sandwich Shell Element 
TRIAX3  Tria3 
Axisymmetric Solid Element 
TRIAX6  Tria6 
Axisymmetric Solid Element 
TRIM3  Tria3  3 noded triangular plane membrane element. 
TRIM6  Tria6  6 noded triangular plane membrane element. 
TRIMS3  Tria3  3 noded triangular solid shell element 
TRIMS6  Tria6  6 noded triangular solid shell element. 
X1DAMP3  Mass  Scalar viscous damper at one node with three degrees of freedom. 
X1DAMP6  Mass  Scalar viscous damper at one node with six degrees of freedom. 
X1GEN6  Mass  General element at one node with six degrees of freedom. 
X1MASS3  Mass  Scalar mass at two nodes with three degrees of freedom. 
X1MASS6  Mass  Scalar mass at one node with six degrees of freedom. 
X1STIFF3  Mass  Scalar spring at one node with three degrees of freedom. 
X1STIFF6  Mass  Scalar spring at one node with six degrees of freedom. 
X2DAMP3  Spring  Scalar viscous damper at two nodes with three degrees of freedom. 
X2DAMP6  Spring  Scalar viscous damper at two nodes with six degrees of freedom. 
X2GEN6  Mass  General element at two nodes with six degrees of freedom. 
X2STIFF3  Spring  Scalar spring at two nodes with three degrees of freedom. 
X2STIFF6  Spring  Scalar spring at two nodes with six degrees of freedom. 
Radioss Cards
 Shell thickness is included with the connectivity data. The default value is contained in the property set.
 The time history is provided for the elements.
 3D elements are supported.
 Degenerated 3D solid elements (from Hexa), such as Tetra and Penta, are included with the present 3D elements.
Card  Supported Element Configurations  Description 

/ADMAS  Mass  Assign additional nonstructural mass to nodes or a group of nodes. Optionally the total additional nonstructural mass of a part or a group of parts can be defined (applied to shells and solids only) or a surface mass can be assigned to a surface and Radioss would then compute the added node based mass value using area (volume)  weighted distribution. 
/BEAM  Bar  Describes the beam elements. Two properties (/PROP/TYPE3 (BEAM) and /PROP/TYPE18 (INT_BEAM)) are available for this beam element. The properties describing a beam element are all defined in a local beam coordinate system. 
/BRIC20  Hex20  Describes 3D solid elements (20 Node Brick Elements). This quadratic element should be used with the property /PROP/SOLID. 
/BRICK 

Defines a hexahedral solid element and thick shell element with 8 nodes. 
/CYL_JOINT  Rigid  Defines cylindrical joints. 
/QUAD  Quad4  Describes the 2D solid elements. QUAD elements must be defined in the global YZ plane. 
/RBE2  Rigid  Defines a rigid body whose independent degrees of freedom are specified at a single main node and whose dependent degrees of freedom are specified at an arbitrary number of secondary nodes. 
/RBE3  RBE3  Defines the motion of a reference (secondary) node as the weighted average of the motions of sets of main nodes. 
/RBODY  Rigid  Defines rigid bodies. 
/RLINK  Rigid  Defines a rigid link. The rigid link imposes the same velocity on all the secondary nodes in one or more directions. 
/SHELL  Quad4  Describes input for 4node shell elements. 
/SH3N  Tria3  Describes the triangular 3node shell elements. 
/SPHCEL  Mass  Describes the SPH cells. 
/SPRING2N  Spring2N  Describes the 2noded spring elements. 
/SPRING3N  Spring3N  Describes the 3noded spring elements. 
/SRPING4N  Spring4N  Describes the 4noded spring elements. 
/TETRA4  Tetra4  Describes a tetrahedral solid element with 4 nodes. 
/TETRA10  Tetra10  Describes a tetrahedral solid element with 10 nodes. 
/TRUSS  Rod  Describes one dimension truss elements, which could be used with property /PROP/TYPE2 (TRUSS). Truss could only carry axial load (like for bar). 
/XELEM  Xelem  Describes the multistrand elements. 
Samcef Cards
Card  Supported Element Configurations  Description 

AXISYM 


BUSH  Spring  
COMP AXISYM 


COMP DEFO PLAN 


COMP MEMB BIDIM 


COMP PLAN GENE 


COMP VOLU 


COMP VOLU COQUE 


COQU DEFO PLAN 


DEFO GENE 


DEFO PLAN 


FLUX THERMIQUE 


FOUR MULT HARM 


FOURIER 


HETEROSIS 


HYBR VOLU 


HYBRID VOLU COQUE 


MEMB AXISYM  Bar2  
MEMB BIDIM 


MEMB FLEXION 


MEMB FOURIER  Bar2  
MEMB MULT HARM  Bar2  
MINDLIN 


RBE3  RBE3  
SAND VOLU 


SOLID SHELL 


THER AXISYM 


THER COQU 


THERMIQU 


TUYAU  Rod  
TUYAU THERMIQUE  Rod  
VOLU COQUE 


VOLUMIC 
