Hello!
I'm in the middle of comparing aluminum and composite wing structure using Patran/Nastran. I already have the results for the aluminum one, but unfortunately I can't access failure indices results for a composite simulation. I've seen numerous of tutorials for failure indices, but there...
Hey guys!
I'm facing quite strange problem with my model. I'm in the middle of stress analysis of the aeroplane wing. Actually, I'm stuck on the model before meshing and computing... First something about my model. It is a surface model extracted from solid model drawn in NX (using parasolid...