(a) Verify that Equation 16.11, the expression for the ratio of fiber load to matrix load \(\left(F_{f} / F_{m}\right)\), is valid. (b) What is the \(F_{f} / F_{c}\) ratio in terms of \(E_{f}, E_{m}\), and \(V_{f}\) ?

Short Answer

Expert verified
Question: Verify the validity of given Equation 16.11 and find the fiber load-composite load ratio \((F_f/F_c)\) in terms of \(E_f, E_m,\) and \(V_f\). Answer: (a) Equation 16.11 has been successfully verified using the rule of mixtures. (b) The fiber load-composite load ratio \((F_f/F_c)\) in terms of \(E_f, E_m,\) and \(V_f\) is given by: \(\frac{F_f}{F_c} = \frac{V_f E_f}{(E_m - V_f E_m) + V_f E_f}\)

Step by step solution

01

(a) Verifying the validity of Equation 16.11

To verify the validity of Equation 16.11, we need to apply the rule of mixtures to find the relationship between fiber load and matrix load. The rule of mixtures states that the composite modulus \((E_c)\) can be given by the following equation: \(E_c = E_fV_f + E_m(1 - V_f)\) Let's denote the stress in the fiber as \(\sigma_f\) and in the matrix as \(\sigma_m\). Since we have the fiber load-matrix load ratio as \(F_f/F_m\), we need to find the relationship between the stresses which can be obtained from the applied strain. The applied strain is assumed to be the same in both the fiber and the matrix, denoted as \(\epsilon\): \(\epsilon = \frac{\sigma_f}{E_f} = \frac{\sigma_m}{E_m}\) Now the fiber and matrix loads can be found with the following relations: \(F_f = A_f \sigma_f = V_f A \sigma_f\) \(F_m = A_m \sigma_m = (1 - V_f) A \sigma_m\) Using the stress relations we found above, we can rewrite these expressions for loads as: \(F_f = V_f A \frac{E_f}{E_m} \sigma_m\) \(F_m = (1 - V_f) A \sigma_m\) Finally, let's find the ratio \(F_f / F_m\): \(\frac{F_f}{F_m} = \frac{V_f A \frac{E_f}{E_m} \sigma_m}{(1 - V_f) A \sigma_m} = \frac{V_f E_f}{E_m - V_f E_m}\) Thus, we have successfully verified Equation 16.11 using the rule of mixtures.
02

(b) Finding the \(F_f / F_c\) ratio

Now, we need to find the fiber load-composite load ratio \((F_f/F_c)\) in terms of \(E_f, E_m,\) and \(V_f\). To do this, let's first find the stress in the composite \((\sigma_c)\). We can use the rule of mixtures: \(E_c = E_fV_f + E_m(1 - V_f)\) Now, considering the overall strain \(\epsilon\): \(\epsilon = \frac{\sigma_f}{E_f} = \frac{\sigma_c}{E_c}\) We already know the relationship between fiber load and matrix load, so let's rewrite fiber load in terms of composite load: \(F_f = \frac{V_f E_f}{E_m - V_f E_m} F_m = \frac{V_f E_f}{E_m - V_f E_m} (F_c - F_f)\) Rearranging the equation to find \(F_f / F_c\): \(\frac{F_f}{F_c} = \frac{V_f E_f}{(E_m - V_f E_m) + V_f E_f}\) The fiber load-composite load ratio \((F_f/F_c)\) in terms of \(E_f, E_m,\) and \(V_f\) has been found.

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Most popular questions from this chapter

In an aligned and continuous carbon fiberreinforced nylon 6,6 composite, the fibers are to carry \(97 \%\) of a load applied in the longitudinal direction. (a) Using the data provided, determine the volume fraction of fibers required. (b) What is the tensile strength of this composite? Assume that the matrix stress at fiber failure is \(50 \mathrm{MPa}\) (7250 psi).

(a) For a fiber-reinforced composite, the efficiency of reinforcement \(\eta\) depends on fiber length \(l\) according to $$ \eta=\frac{l-2 x}{l} $$ where \(x\) represents the length of the fiber at each end that does not contribute to the load transfer. Make a plot of \(\eta\) versus \(l\) to \(l=50 \mathrm{~mm}\) (2.0 in.), assuming that \(x=1.25 \mathrm{~mm}(0.05 \mathrm{in} .)\). (b) What length is required for a \(0.90\) efficiency of reinforcement?

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