CBAR

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 , from GA, in the displacement coordinate system at GA (see Figure 1). 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 iA and iB, respectively, in displacement coordinate systems at points GA and GB, respectively (see Figure 1). Real or blank 0.0
F0 Preload. Real or blank 0.0

Remarks:

  1. Element identification numbers must be unique with respect to all other element identification numbers.
  2. If field 6 is an integer, then G0 is used. If field 6 is blank or real, then X1, X2, X3 is used.
  3. G0 cannot be located at GA or GB.
  4. If there are no pin flags or offsets, the continuation may be omitted.
  5. 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)