Page 370 - Biomedical Engineering and Design Handbook Volume 1, Fundamentals
P. 370

BIOMEDICAL COMPOSITES  347

                            The rule of mixtures equations have several drawbacks. The isostrain assumption in the Voight
                          model implies strain compatibility between the phases, which is very unlikely because of different
                          Poisson’s contractions of the phases. The isostress assumption in the Reuss model is also unrealistic
                          since the fibers cannot be treated as a sheet. Despite this, these equations are often adequate to
                          predict experimental results in unidirectional composites. A basic limitation of the rule of mixtures
                          occurs when the matrix material yields, and the stress becomes constant in the matrix while continuing
                          to increase in the fiber.
                                                                     ∗
                            The ultimate tensile strength of a fibrous composite s depends on whether failure is fiber-
                                                                     c
                          dominated or matrix-dominated. The latter is common when V is small. One result of such treatment is
                                                                     f
                                                         σ *
                                                                   *
                                                       *
                                                     σ =  m  EV + σ V                        (14.6)
                                                       c
                                                              f 1
                                                                   m m
                                                               f
                                                         E
                                                          m
                                ∗
                          where s is the fracture strength of the matrix.
                                m
                            Other results from this simple analytical approach for orthotropic composites are
                                                                   α V
                                                         E 1f α V +  E m m m
                                                            1f
                                                              f
                                                    α =                                      (14.7)
                                                     1c
                                                           EV +  E V
                                                              f
                                                                  m m
                                                            1 f
                                                        1
                                                   C =    ρ (  f C V + ρ m m m               (14.8)
                                                                   C V )
                                                    c
                                                               f
                                                             f
                                                       ρ
                                                        c
                                                       K =  K V +  K V                       (14.9)
                                                        c 1
                                                                  m m
                                                            f
                                                              f
                          where a is the coefficient of thermal expansion, C is the specific heat, and K is the thermal conduc-
                          tivity. The coefficient of hygroscopic expansion b can be found by substituting a with b above.
                          These results are for the longitudinal directions only.
              14.5.2  Theory of Elasticity Models
                          In this approach, no assumptions are made about the stress and strain distributions per unit volume.
                          The specific fiber-packing geometry is taken into account, as is the difference in Poisson’s ratio
                          between the fiber and matrix phases. The equations of elasticity are to be satisfied at every point in
                          the composite, and numerical solutions generally are required for the complex geometries of the
                          representative volume elements. Such a treatment provides for tighter upper and lower bounds on
                          the elastic properties than estimated by the rule of mixtures, as is described in the references used in
                          this section.
                            One illustrative result for the longitudinal Young’s modulus is
                                           2 [( v −  v ) 2 EVE V ]
                                                    f
                                                m
                                             f
                                                      f
                                                        m m
                          E =                                          + E m  + E (  f  − E V )  f  (14.10)
                              { EV 1− (  v −  v 2 ) + E ⎡ V 1− ( 1 v m  − v m 2  1− v ) ⎤ ⎦ }
                            c 1
                                                                                  m
                                            2
                                                           2 ) + (
                                                f ⎣
                                 mm
                                                                    m
                                        f
                                                   f
                                            f
                          where v and v are the Poisson’s ratios of the fiber and matrix, respectively. Very small differences
                               f    m
                          in the Poisson’s ratios of the phases cause such equations to be simplified to the rule of mixtures.
              14.5.3  Semiempirical Models
                          Curve-fitting parameters are used in semiempirical and generalized equations to predict experimen-
                          tal results. The most common model was developed by Halpin and Tsai, and it has been modified for
                          aligned discontinuous fiber composites to produce such results as the following for the longitudinal
                          modulus:
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