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composite materials   •   23








                             Figure 2.4.  Illustrates the shear load applied to a composite body.


















                             Figure 2.5.  Illustrates the loading due to flexure on a composite body.


                           a composite is often used to indicate this property in a multi-layer
                           composite (“laminate”).
                        Flexure:  Flexural  loads are really  a  combination of  tensile,  com-
                           pression,  and  shear  loads. When loaded as shown in Figure 2.5,
                           the upper face is put into compression, the lower face into tension,
                           and the central portion of the laminate experiences shear.



                      2.1.1.2  Comparison With other Structural Materials

                      Owing to the factors described previously, there is a very large range
                      of mechanical properties that can be achieved with composite materi-
                      als. Even when considering one fiber type on its own, the composite
                      properties can vary by a factor of 10 with the range of fiber contents
                      and orientations that are commonly achieved. The comparisons that fol-
                      low therefore show a range of mechanical properties for the composite
                      materials. The lowest properties for each material are associated with
                      simple manufacturing processes and material forms (e.g., spray lay-up
                      glass fiber), and the higher properties are associated with higher technol-
                      ogy manufacture (e.g., autoclave molding of unidirectional glass fiber
                      prepreg), such as would be found in the aerospace industry. For the other
                      materials shown, a range of strength and stiffness (modulus) figures are
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