Dear all,
I am working with a tapered cylindrical shell featuring the following layup: [45, -45, Aramid honeycomb, -45, 45]. The face sheets are made of CFRC. For the honeycomb core, I have the values for E1, E2, E3, ν12, ν13, G12, G23, G13, as well as the compression and shear strengths in...