Article ID Journal Published Year Pages File Type
6707132 Composite Structures 2015 10 Pages PDF
Abstract
In this work, smart cure cycle was developed to reduce the thermal residual stress of the co-cured E-glass/carbon/epoxy structure for VRFB. The deformations of structure fabricated using smart cure cycle were investigated with respect to the degree of cure and post-cure process using the viscoelastic properties of composite materials during post-cure process. In addition, the thermal residual stress and actual bonding temperature were calculated. Using the experimental results of degree of cure and actual bonding temperature, a finite element analysis was performed to verify the stress of the co-cured FF-BP structure as a function of the cure cycles.
Related Topics
Physical Sciences and Engineering Engineering Civil and Structural Engineering
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