Page 225 - Mechanics Analysis Composite Materials
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210                 Mechanics and analysis of composite materials
             directions.  Much more possibilities for such shaping are provided  by implementa-
             tion  of  knitted  fabrics whose strain to failure exceeds  100%. Moreover,  knitting
             allows us to shape the fibrous preform  in accordance with the shape of the future
             composite part. There exist different knitting patterns, some of which are shown in
             Fig. 4.83. Relatively high curvature of the yarns in knitted fabrics and possible fiber
             breakage in the process of knitting result in materials whose strength and stiffness
             are less than those of woven fabric composites, but whose processability is higher,
             and the cost is lower. Typical stress-strain  diagrams for composites reinforced by
             knitted fabrics are presented in Fig. 4.84.
               Material  properties  close  to  those  of  woven  composites  are  provided  by
             braided  structures which, being usually tubular in  form  are fabricated  by  mutual
             intertwining,  or  twisting  of  yarns  about  each  other.  Typical  braided  structures
             are  shown  in  Fig. 4.85.  Biaxial  braided  fabrics  in  Fig. 4.85  can  incorporate
             longitudinal yarns forming a triaxial braid whose structure is similar to that shown
            in  Fig. 4.81d.  Braided  preforms  are  characterized  with  very  high  processability
            providing  near  net-shape  manufacturing of tubes, and profiles with various cross-
             sectional shapes.
              Although microstructural models of the type shown in Fig. 4.80 and leading to
            equations  similar to Eq. (4.167) have been developed to predict  stiffness and even



                               c, MPa
                               400

                               300

                               200
                                                           45"

                               100

                                                              E,%
                                0                          2
                                  0    I     2    3     4    5
            Fig. 4.82.  Stress-strain  curves for fiber glass fabric composite loaded in tension at different angles with
                                      respect to the warp direction.












                                    Fig. 4.83.  Typical knitted structures.
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