hi, I am doing a risk analysis of a cylindrical fuselage with windows. I have applied contact interactions between the different parts, and I have applied a unit value load to a reference point, joining the displacements of that point to my figure. however, the lpf comes out constant, and does not come out as it should, as I understand that it should come out a maximum and then decrease.
attached is my load proporcionality factor plot
does anyone know what this is due to?