摘要: In recent years, large composite structures have been used increasingly in the aerospace and naval industries. Such a structure is mostly fabricated using scarf joining technique so that multiple substructures can be connected together. Figure 1 shows three commonly joint configuration. Among three, step/overlap considered as strongest because it has largest surface area. As result, this chapter addresses joint. The typically constructed sketched Fig. 2. Vacuum Assisted Resin Transfer Molding (VARTM) frequently for fabrication process applied to size of structure. Furthermore, also repair damaged section.