document: On a general constitutive description for the inelastic and failure behavior of fibrous laminates . II . Laminate theory and applications For pt . I see ibid. , pp. 1159-76 . The two papers report systematically a constitutive description for the inelastic and strength behavior of laminated composites reinforced with various fiber preforms . The constitutive relationship is established micromechanically , through layer-by-layer analysis . Namely , only the properties of the constituent fiber and matrix materials of the composites are required as input data . In the previous part lamina theory was presented . Three fundamental quantities of the laminae , i.e. the internal stresses generated in the constituent fiber and matrix materials and the instantaneous compliance matrix , with different fiber preform -LRB- including woven , braided , and knitted fabric -RRB- reinforcements were explicitly obtained by virtue of the bridging micromechanics model . In this paper , the laminate stress analysis is shown . The purpose of this analysis is to determine the load shared by each lamina in the laminate , so that the lamina theory can be applied . Incorporation of the constitutive equations into an FEM software package is illustrated . A number of application examples are given to demonstrate the efficiency of the constitutive theory . The predictions made include : failure envelopes of multidirectional laminates subjected to biaxial in-plane loads , thermomechanical cycling stress-strain curves of a titanium metal matrix composite laminate , S-N curves of multilayer knitted fabric reinforced laminates under tensile fatigue , and bending load-deflection plots and ultimate bending strengths of laminated braided fabric reinforced beams subjected to lateral loads
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