martin555
Aerospace
- Nov 30, 2018
- 17
I am looking to compare my hand calculations from my classical laminate theory tool to a FEM model.
I am using FEMAP and want to apply a Nx load of 100lb.in.
How does this convert into the FEMAP load definition.
If I use point load the unit would be lbf correct ?
I am using FEMAP and want to apply a Nx load of 100lb.in.
How does this convert into the FEMAP load definition.
If I use point load the unit would be lbf correct ?