ProductsAbaqus/CAE Stress values are extracted at regular intervals along the defined section, and integration is performed numerically using the extracted stress values. Membrane, bending, and peak stress values are computed. These stresses are defined as follows:
For the best results, the endpoints of the section should be chosen so that the section is normal to the interior and exterior surfaces of the model. This orientation minimizes problems with shear stresses since they will be approximately zero at the ends of the line (Kroenke, 1973). Three-dimensional structuresThe membrane values of the stress components are computed using the following equation: where
The linear bending values of the stress components are computed using the following equations: where and are the bending values of the stress at point A and point B (the endpoints of the section; see Figure 1). Figure 1. Recommended stress paths.
The integration is performed numerically. Assuming the path between point A and point B is divided uniformly into n intervals, the integrals are evaluated as follows: and where is the stress at point j along the path. Axisymmetric structuresThe derivation of the above equations is similar for the axisymmetric case, except for the fact that the neutral axis is shifted radially outward. Separate expressions are obtained for the stresses in the thickness, meridional, and hoop directions. In Abaqus/CAE these are represented as local directions 1, 2, and 3, respectively (see Figure 2). Figure 2. Stress directions.
Meridional stressThe meridional stresses are computed using the following relations. The meridional force per unit circumferential length is where
The meridional membrane stress is obtained by dividing through the thickness: The numerical scheme used to compute the meridional membrane stress is where
To compute the meridional bending stresses, we first need to compute the distance from the center surface to the neutral surface for meridional bending. That distance, , is equal to where is the angle between the thickness direction and the radial direction. The meridional bending moment per unit circumferential length is defined as and the moment of inertia for meridional bending is given by Hence, the meridional bending stresses at the endpoints A and B are obtained with The numerical scheme used to compute the meridional bending moment is Hoop stressThe hoop membrane stress is obtained with where
The hoop bending stresses at the endpoints are obtained using the relations where is the distance from the center surface to the neutral surface for hoop bending, is the hoop bending moment per unit meridional length, and is the moment of inertia for circumferential bending. The numerical scheme to compute the circumferential membrane stress is and the bending moment is computed with the summation Thickness stressThe thickness stress does not transfer any forces or moments. Typically, the stress arises due to applied external pressures and thermal expansion effects, and there is no obvious preferred method for determining membrane and bending stresses. Hence, we choose the thickness membrane stress as the average thickness stress: We choose the thickness bending stress such that the sum of the thickness membrane and bending stresses at the endpoints A and B is equal to the total stress at these points: and interpolate the bending stress linearly between these values. This is a reasonable assumption, since the thickness surface stresses are determined by the applied pressure and should not have a strong peak stress contribution. Shear stressThe membrane shear stress in the meridional plane is computed in the same way as the meridional membrane stress: where is the shear stress along the path. The shear stress distribution is assumed to be parabolic and equal to zero at the ends. Hence, the bending shear stresses are set to 0.0. The numerical scheme used to compute the membrane shear stress is: |