Figure 332 shows an example of a stress line defined for an axisymmetric model of a pressure vessel.
The stress line Section_A_B is defined through the vessel wall. Figure 333 and Figure 334 show the basic settings and computations, respectively, that you use to linearize the S22 stress component for the undeformed model shape. When you click OK or Apply in the Stress Linearization dialog box, ABAQUS/CAE creates an X–Y plot of the S22 stress component (oriented normal to the stress line) and of the resulting linearized stresses, as shown in Figure 335. The following output is also written to a file called linearStress.rpt:******************************************************************************** Statically Equivalent Linear Stress Distribution across a Section, written on Wed Mar 24 15:05:47 2004 Source ------- ODB: Job-1.odb Step: Step-1 Frame: Increment 1: Step Time = 1.000 Linearized Stresses for stress line 'Section_A_B' X Y Z XY Shear Stress Stress Stress Stress Membrane (Average) Stress -388.19 1493.14 1497.67 74.0502 Membrane plus Bending, Point 1 -737.581 1889.06 1770.23 74.0502 Membrane plus Bending, Point 2 -98.2912 1124.3 1245.32 74.0502 -------------------------------- INVARIANT RESULTS -------------------------- Bending components in equation for computing membrane plus bending stress invariants are: S22 Max. Mid. Min. Tresca Mises Prin. Prin. Prin. Stress Stress Membrane (Average) Stress 1497.67 1496.05 -391.101 1888.77 1887.96 Membrane plus Bending, Point 1 1891.47 1497.67 -390.596 2282.06 2112.87 Membrane plus Bending, Point 2 1497.67 1127.92 -391.807 1889.47 1734.41The Y Stress corresponds to the S22 stress shown in Figure 335. The actual stress values plotted in the curve Section_A_B_S22 do not appear in the report. The linearized membrane and membrane-plus-bending stress curves are generated from the values shown for Y Stress. The reported invariants are calculated from the selected linearized components.