I am simulating a wing with a winglet as Flat Plate panels stiched together as usual and coupled with the structural model. Nevertheless after running an analysis the result shows that the aerodynamic panels of the winglet are torn away from the main wing aerodynamic panels as shown at the...
I am analysing a glass fiber composite structure with PATRAN/NASTRAN. My F06 file contains results in terms of failure index as well, but when the results are attached the only options I have are constraints forces, displacements and stresses.
How to view the results for failure index?