Stress Linearization
Stress linearization is a procedure in which the stress distribution along a line through the thickness in a solid is approximated with an equivalent linear stress distribution, similar to what would be the result of an analysis using shell theory. The line is commonly referred to as a stress classification line, SCL.
First, the computed stresses are transformed into a local orthonormal coordinate system x1-x2-x3, where the x1 direction is oriented along the SCL. In 3D, you must specify the x2 direction, and thus implicitly the x3 direction. In 2D and 2D axial symmetry, the x3 direction is in the out-of-plane direction — that is, the Z and azimuthal directions, respectively.
The length of the SCL, which is assumed to be straight, start on one boundary, and end on the opposite boundary, is denoted L.
The membrane stress tensor is the average of each local stress component along the SCL:
Each component of the bending stress tensor is assumed to have a linear variation along the SCL, with the value being zero at the midpoint.
The maximum bending stress is defined so that the linear stress distribution has the same moment as the true stress distribution.
The linearized stress distribution is the sum of the membrane and bending stresses,
Finally, the peak stress tensor is defined at the two endpoints of the SCL. It is the difference between the actual stress tensor, and the linearized stress representation.
The stress intensity, also known as the Tresca equivalent stress, is often the ultimate goal of a stress linearization. It is computed as a worst case of the equivalent stress at the two ends of the SCL. The stress intensity is computed from the principal stresses as
When computing the principal stresses at the endpoints of the SCL, it is customary to ignore the bending part of the through-thickness oriented stresses. The principal stresses and the stress intensity variables are the endpoints are thus computed using the following stress tensor:
Section forces, similar to what would be computed in a shell or plate analysis, is another type of result quantities available for each SCL. The in-plane forces are computed from the membrane stresses as
The bending moments are computed from the bending stresses as
The out-of-plane shear forces are computed from the membrane stresses as