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Procedia engineering, v.10, 2011년, pp.3220 - 3225
Montoro, S.R. , Shiino, M.Y. , Cruz, T.G.d. , Cioffi, M.O.H. , Woorwald, H.J.C.
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A major difficulty to achieve maximum weight savings in the manufacture of composite structural components, is the tendency of these materials have the formation of voids and cracks in the interior and surface components. In aeronautical applications, controlling the volume fraction of fibers, resin...
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