Hello,
I hope you are doing well.
I am doing a dummy model to validate shear stresses on a beam (actually it is a fastener in a larger model).
The model is really simple, a cantilever beam, fixed at left and a 100 [N] vertical force on the other end. It has a length of 100 [mm] and thus, 100 elements. The beam has a circular section of r = 5 [mm]. The solver is Nastran MSC.

Questions/Problems :
1) I found one thing that I do not understand. The force is applied in the vertical Y direction, and the bar follows the X direction. Then, I should have the whole shear in the plane normal to the bar axis, i.e., the YZ plane. However, I found the shear decomposed in two planes (named 1 & 2). The so-called Web Shear Plane1 is 32.444 and the Web Shear Plane2 is 94.591. In the modulus I found the 100 [N] in Shear, but I do not understand why it is split in two planes. The same happens with the bending moment, which should only be present in the Z direction given the loading.

2) The problem that I found is that by no means I can get neither VM stresses nor shear stresses output for the CBEAM elements.
I've tried with the global output request STRESS(VM), STRESS(SHEAR) but I do not have these results later in HyperView.
For 1D Stress the results available are : CBEAM Long Stress at Point C1/D1/E1/F1, CBEAM Maximum Stress1 & CBEAM Minimum Stress1 and some others like these.
For CBEAM Maximum Stress1, I found 96.349 [MPa] which I imagine is a normal stress given by Sigma= M * y / I, being M = 10000 [N.mm], y = r & I = 490.87385, which manually calculated gives 101.85 [MPa].
Thank you in advance !
Sincerely,
EC