Simple Beam Element Connection
Description: Defines a simple beam element.
Format:
Example:
Alternate Format and Example:
Field | Definition | Type | Default |
---|---|---|---|
EID | Element identification number. | Integer > 0 | Required |
PID | Property identification number of a PBAR entry. | Integer > 0 | Required |
GA, GB | Grid point identification numbers of connection points. | Integer > 0; GA ≠ GB | Required |
X1, X2, X3 | Components of vector
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Real or blank | |
G0 | Grid point identification number to optionally supply X1, X2, and X3. Direction of orientation vector is GA to G0. | Integer or blank | |
PA, PB | Pin flags for bar ends A and B, respectively (up to 5 of the unique digits 1-6 anywhere in the field with no embedded blanks). Used to remove connections between the grid point and selected degrees of freedom of the bar. The degrees of freedom are defined in the element's coordinate system (see Figure 1). The bar must have stiffness associated with the PA and PB degrees of freedom to be released by the pin flags. For example, if PA = 4 is specified, the PBAR entry must have a value for J, the torsional stiffness. | Integer > 0 or blank | None |
WiA, WiB | Components of offset vectors
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Real or blank | 0.0 |
F0 | Preload. | Real or blank | 0.0 |
Remarks:
- Element identification numbers must be unique with respect to all other element identification numbers.
- If field 6 is an integer, then G0 is used. If field 6 is blank or real, then X1, X2, X3 is used.
- G0 cannot be located at GA or GB.
- If there are no pin flags or offsets, the continuation may be omitted.
- Offset vectors are treated like rigid elements and are therefore subject to the same limitations.
- Offset vectors do not affect thermal loads.
- The specification of offset vectors is not recommended in solutions that compute differential stiffness because the offset vector remains parallel to its original orientation (differential stiffness is computed in buckling, prestress, and nonlinear analysis with PARAM, LGDISP, ON).
Figure 1. CBAR Element Geometry
Figure 2. CBAR Element Internal Forces and Moments (xy-Plane)
Figure 3. CBAR Element Internal Forces and Moments (xz-Plane)