Thursday - last edited Thursday
I'm having a problem analysing a torsion.
I have a hollow NACA 0012 wing profile with a small slot on the trailing edge. I fully constrained one side and applied a moment on the other. I'm looking for the rotation values on the Z axis (preferably with the referencial on the centroid). It's expected that the torsion grows from 0 on the constrained side and maximum on the other side.
I'm using 2D elements with 1 mm thickness.
What am I getting wrong?
Thanks in advance
When you run model - Nastran create many files in model directory: *.f06 - error log, *.op2 - results, *.dat - solver input that contain mesh, loads, constraints and analysis setting. This dat file can be imported to NX or Femap or other FEA sofrware or edited by hand in text editor. This file is more practical to inmpot - it can be imported to previous versions of NX.