Section

Section#

This command configures a Section, which represents a constitutive model between stress and strain resultants.

Model.section(type, tag, *args)#
Parameters:
  • type (string) – section type

  • tag (integer) – unique section tag

  • args – additional arguments dependent on section type

Library#

The following section types are valid for Frame elements:

For Plane elements, the following section types are available:

The following section types are valid for Shells: