Invariant based approaches in the design of composite laminates

Invariant based approaches have been proposed to simplify the design and analysis of composite materials, in particular, for generating design allowables. Of these invariants, Trace, more recently referred to as Tsai's Modulus, a material property derived from the plane stress stiffness matrix, can be used to help with preliminary design. However, in literature this has mainly focused on unidirectional composites. The present work extends the application of invariants to woven and hybrid composites, i.e. the latter made with both unidirectional and woven laminae, and provides appropriate validation for the use of invariants in design. A novel approach to implement Tsai's Modulus and determine the three-dimensional stiffness matrix of a woven specimen is proposed. Omni failure envelopes have been proposed in literature and these have been extended to accommodate hybrid specimens with both unidirectional and woven laminae. This work shows that Tsai's Modulus and invariants can be used as an initial design tool in order to establish the likely properties of a given layup and material combination for use in preliminary design. Property predictions at the laminate level, E-x, E-y, nu(xy) and G(xy), were within +/- 10% of experimental values for highly complex laminate stacking sequences and material combinations.

Automated summary

Invariant based approaches have been extended to woven and hybrid composites, with a novel method proposed for Tsai's Modulus implementation and determination of the three-dimensional stiffness matrix of woven specimens, showing their potential as initial design tools.