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?

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