Von Mises Stress
CELAS Stress
CROD Axial Stress
CBAR Longitudinal Stress SAC
CBAR Longitudinal Stress SAD
CBAR Longitudinal Stress SAE
CBAR Longitudinal Stress SAF
CBAR Longitudinal Stress SAMIN
CBAR Longitudinal Stress SAMAX
CBAR Longitudinal Stress SBC
CBAR Longitudinal Stress SBD
CBAR Longitudinal Stress SBE
CBAR Longitudinal Stress SBF
CBAR Longitudinal Stress SBMIN
CBAR Longitudinal Stress SBMAX
CWELD Axial Stress
CWELD Maximum Stress A
CWELD Minimum Stress A
CWELD Maximum Stress B
CWELD Minimum Stress B
CWELD Maximum Shear Stress
CWELD Bearing Stress
Von Mises Stress
The following stress results are output for CBAR/CBEAM elements defined via PBARL/PBEAML property entries. The Result type: HyperView is CBAR/CBEAM Stresses (<TYPE>), where the <TYPE> entry is based on the selected cross-section (TYPE/NAME field) on the PBARL/PBEAML entries. The element stress results can be reviewed for each cross-section type, corresponding evaluation point, at element ends (A or B). The maximum normal/shear/von Mises stresses can also be reviewed.
- | CBAR/CBEAM Stresses (<Type>) |
<Stress Result Output> <evaluation point> (A/B)
Where,
<Type> = BAR, BOX, BOX1, CHAN, CHAN1, CHAN2, CROSS, H, HAT, I, I1, ROD, T, T1, T2, TUBE, Z.
<Stress Result Output> = normal, shear, and von Mises
<evaluation point> = evaluation point of the element
- | CBAR/CBEAM Stresses(BAR) |
Normal S1N(A)
Normal S1N(B)
Shear S4S(A)
Shear S4S(B)
von Mises S8V(A)
von Mises S8V(B)
Normal S3N(B): normal stress at the 3rd evaluation point of the beam element (end B);
Shear S6S(A): shear stress at the 6th evaluation point of the beam element (end A);
von Mises S5V(B): von Mises stress at the 5th evaluation point of the beam element (end B).
Review evaluation points via: DRESP1 - Static Stress Item Codes for Bar Elements using PBARL, PBEAML Properties
The von Mises stresses for all CBEAM/CBAR elements with PBARL/PBEAML properties at the same time can be output using the Result type: CBAR/CBEAM vonMises Stresses.
- | CBAR/CBEAM vonMises Stresses |
<Stress Result Output>
Where,
<Stress Result Output> = Von Mises
Results are calculated by HyperView.
Von Mises Stress
Maximum Principal Stress
Von Mises Stress (Z1)
Von Mises Stress (Z2)
Von Mises Stress (mid)
P1 (major) Stress (Z1)
P1 (major) Stress (Z2)
P1 (major) Stress (mid)
P3 (minor) Stress (Z1)
P3 (minor) Stress (Z2)
P3 (minor) Stress (mid)
Normal X Stress (Z1)
Normal X Stress (Z2)
Normal X Stress (mid)
Normal Y Stress (Z1)
Normal Y Stress (Z2)
Normal Y Stress (mid)
Shear XY Stress (Z1)
Shear XY Stress (Z2)
Shear XY Stress (mid)
Principal Stress Angle (Z1)
Principal Stress Angle (Z2)
Principal Stress Angle (mid)
Von Mises Stress
Maximum Principal Stress
Results are calculated by HyperView.
Von Mises Stress
Signed Von Mises Stress
P1 (major) Stress (solid)
P2 (mid) Stress (solid)
P3 (minor) Stress (solid)
Normal X Stress (solid)
Normal Y Stress (solid)
Normal Z Stress (solid)
Shear XY Stress (solid)
Shear YZ Stress (solid)
Shear XZ Stress (solid)
Von Mises Stress
Von Mises Stress
Maximum Principal Stress
1. | In the TENSOR mode, pass tensor components to HyperView, which then calculates derived results on-the-fly. |
2. | For frequency response loadcases, only the TENSOR mode is available. |