where
Nx = Axial resultant force
Ny = Resultant force in beam Y coordinate direction
Nz = Resultant force in beam Z coordinate direction
Mx = Torque about the beam axes
My = Torque about the beam Y coordinate direction
Mz = Torque about the beam Z coordinate direction
Ax = Axial acceleration
Ay = Acceleration in beam Y coordinate direction
Az = Acceleration in beam Z coordinate direction
Rx = Angular acceleration about beam axes
Ry = Angular acceleration about beam Y coordinate direction
Rz = Angular acceleration about beam Z coordinate direction Cij( T) (where i=1,7 and j = i,7) = mass
or moment of inertia terms in the upper triangle of the cross-section mass matrix as a function of
temperature
T = Current temperature
15.5.1. Defining a Composite Beam Section
Each of the following commands specifies a particular component quantity necessary for defining a
preintegrated composite beam section:
Table 15.3: Commands for Specifying Preintegrated Composite Beam Section Data
Command Quantity Defined and Data Specified
Cross-section stiffness matrix. Upper triangle
of 6 x 6 or 7 x 7 matrix. Row and column 7 are
used only when KEYOPT(1) = 1.
CBMX [ 1 ]
Cross-section mass matrix. Upper triangle of 6
x 6 matrix.
CBMD [ 1 ]
Temperature specification for a subsequent
matrix.
CBTMP [ 1 ]
T
CBTE [ 1 ] Thermal expansion coefficient
ALPHA
- Repeatable for six independent temperatures.
Temperature dependencies (T) You can define each of the preintegrated composite beam section
data components as temperature-dependent. It is possible to specify up to six temperatures (T ) by reis-
suing any command as necessary. If you issue a command for a temperature specified earlier, the most
recent data supersedes the previous value.
15.5.1.1. Matrix Input.
Each component (axial, bending, torque, transverse shear, and warping) of a preintegrated beam section
definition is input directly as a 7 x 7 matrix. The terms of the matrix are defined via the CBMX command.
Release 15.0 - © SAS IP, Inc. All rights reserved. - Contains proprietary and confidential information
Using Preintegrated Composite Beam Sections