Abstract

Octet lattice structures were designed with carbon fiber reinforced polymer (CFRP) composite hollow cylindrical struts to improve the specific compressive strength and stiffness of these lightweight structures. A joint connector was designed and manufactured from balanced [0/90] CFRP laminates to assemble the designed octet lattice structures. The compressive modulus and strength of CFRP cylindrical tube-based octet lattice structures were measured under quasi-static compression. Two competing failure mechanisms were observed. The fiber fracture of CFRP hollow struts dominated the failure of lattice structures with a relative density (ρ-) of 2.17%. In contrast, lattice structures with lower relative densities (ρ-= 1.33% and 0.85%) failed by Euler buckling of the CFRP hollow struts. To gain further insight of the compressive behavior of the lattice structures, an analytical model and a series of finite element (FE) models were developed. The predictions showed good agreement with experimental observations of both the compressive properties and failure behaviors. The results demonstrate that CFRP tube-based octet lattice structures exhibited significantly higher relative strength and stiffness than CFRP laminated strut-based counterparts. These superior properties of CFRP tube-based octet lattice structure show a strong potential in high performance lightweight load-bearing application.

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