Part I (Salzar et al, 1996) of the paper presented an exact elastic-pl
astic analytical solution for an arbitrarily laminated metal matrix co
mposite tube subjected to axisymmetric thermo-mechanical and torsional
loading. In Part II, this solution strategy is first validated by com
parison with available closed-form solutions, as well as with results
obtained using the finite-element approach. Subsequently, examples are
presented that illustrate the utility of the developed solution metho
dology in predicting the elastic-plastic response of arbitrarily layer
ed metal matrix composite tubes. In particular, optimization of the th
e response of composite tubes under internal pressure is considered th
rough the use of functionally graded architectures.