.16.26 (a) Write an expression for the modulus of elasticity for a hybrid composite in which all fibers of both types are oriented in the same direction. (b) Using this expression, compute the longitudinal modulus of elasticity of a hybrid composite consisting of aramid and glass fibers in volume fractions of \(0.30\) and \(0.40\), respectively, within a polyester resin matrix \(\left[E_{m}=2.5 \mathrm{GPa}\left(3.6 \times 10^{5} \mathrm{psi}\right)\right]\)

Short Answer

Expert verified
Answer: The longitudinal modulus of elasticity for the hybrid composite is approximately 69.01 GPa.

Step by step solution

01

Definition of Modulus of Elasticity for a Hybrid Composite

The modulus of elasticity for a hybrid composite material refers to its ability to resist deformation under an applied force. For a composite material with fibers oriented in the same direction, the modulus of elasticity can be calculated as the sum of the individual moduli for each type of fiber, weighted by their respective volume fractions.
02

Expression for Modulus of Elasticity

To derive the expression for the modulus of elasticity for a hybrid composite, let's consider a composite material with two types of fibers (fiber 1 and fiber 2) and a matrix (m). Let \(E_1\), \(E_2\), and \(E_m\) represent the moduli of elasticity for fiber 1, fiber 2, and the matrix, respectively. Similarly, let \(V_1\), \(V_2\), and \(V_m\) represent the volume fractions for fiber 1, fiber 2, and the matrix, respectively. Then, the modulus of elasticity for the hybrid composite (\(E_c\)) can be expressed as: \(E_{c} = V_{1}E_{1} + V_{2}E_{2} + V_{m}E_{m}\)
03

Calculation of Longitudinal Modulus of Elasticity

Now that we have the expression for the modulus of elasticity for the hybrid composite, we'll calculate the longitudinal modulus of elasticity for the given composite material consisting of aramid and glass fibers within a polyester resin matrix. Given the volume fractions of aramid (\(V_{1} = 0.30\)) and glass fibers (\(V_{2} = 0.40\)), with the modulus of elasticity for polyester resin matrix provided as \(E_{m} = 2.5 \; \text{GPa}\). If we refer to appropriate material property tables, we can find the values for the moduli of elasticity for aramid and glass fibers: \(E_{1} = 131 \; \text{GPa}\) (for aramid fibers) \(E_{2} = 72.4 \; \text{GPa}\) (for glass fibers) Since the volume fractions must add up to 1, we can find the volume fraction for the matrix: \(V_{m} = 1 - V_{1} - V_{2} = 1 - 0.30 - 0.40 = 0.30\) Now we can substitute this information back into our expression for the modulus of elasticity for the hybrid composite: \(E_{c} = (0.30)(131) + (0.40)(72.4) + (0.30)(2.5) = 39.3 + 28.96 + 0.75 = 69.01 \; \text{GPa}\) So the longitudinal modulus of elasticity of the hybrid composite is approximately \(69.01 \; \text{GPa}\).

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Key Concepts

These are the key concepts you need to understand to accurately answer the question.

Composite Materials
Composite materials are engineered or naturally occurring materials made from two or more constituent materials with significantly different physical or chemical properties that remain separate and distinct within the finished structure. The main advantage of composite materials is their ability to combine the best characteristics of their components to create a substance with superior properties to traditional materials. For instance, composite materials can be designed to be lightweight yet incredibly strong, or they can be made to conduct heat while withstanding high temperatures.

Commonly, a composite is made up of a reinforcement material (such as fibers or particles), which provides strength and stiffness, and a matrix (such as polymer, metal, or ceramic), which supports the reinforcement and distributes the load evenly. The success of a composite material depends heavily on how well these two constituents work together, which is often determined by the bonding quality and the compatibility between the reinforcement and the matrix.

In solving problems involving composites, understanding the role of each constituent material as well as how they interact is vital. It is this intrinsic understanding that allows engineers to tailor composites to meet specific design needs.
Fiber Reinforcement
Fiber reinforcement refers to the technique of incorporating fiber materials into a matrix to create a composite material. Fibers are typically chosen for their high tensile strength and modulus of elasticity, enabling the composite to sustain heavy loads without deforming. The alignment, length, and distribution of these fibers within the matrix play a crucial role in determining the mechanical properties of the final composite.

Fiber reinforcement can be broadly classified into continuous and discontinuous (short) fiber reinforcement. When fibers are aligned in the direction of the applied force, as in the case of the exercise, the composite is said to have a unidirectional structure, which maximizes strength and stiffness in that particular direction.

Incorporating high-strength fibers like aramid or carbon into polymers can significantly enhance the material's performance. For instance, aramid fibers, known for their exceptional strength-to-weight ratio and resistance to impact, are often used in ballistic protective gear. Similarly, glass fibers are used to provide stiffness and strength while being cost-effective. The selection of fiber types and their properties is crucial for designing composites with desired characteristics.
Volume Fraction
Volume fraction is a measure used to describe the proportion of each component within a composite material. It is defined as the volume of a particular constituent divided by the total volume of the composite. Volume fractions are crucial as they influence the overall properties and performance of the composite material.

The volume fraction concept plays an integral role in tailoring the mechanical properties of composites. By adjusting the relative amounts of fiber and matrix materials, engineers can design composites with specific elasticity, strength, weight, and other properties. For instance, increasing the volume fraction of fibers usually increases the strength and stiffness of the composite, but there is an optimum beyond which additional fibers might not significantly improve performance, and could make the composite more brittle and less damage tolerant.

In the textbook exercise, the volume fractions of aramid and glass fibers within the polyester matrix are key parameters used to determine the composite's modulus of elasticity. The calculation involves summing the product of each material's modulus of elasticity and its respective volume fraction, emphasizing the central role volume fraction plays in composite material design. Understanding this relationship helps in predicting how changes in material composition might affect a composite's behavior under load.

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Most popular questions from this chapter

16.7 (a) For a fiber-reinforced composite, the efficiency of reinforcement \(\eta\) is dependent 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 \(l=40\) \(\mathrm{mm}\) (1.6 in.), assuming that \(x=0.75 \mathrm{~mm}\) \((0.03 \mathrm{in} .)\) (b) What length is required for a \(0.80\) efficiency of reinforcement?

\(16.14\) A continuous and aligned fiber-reinforced composite having a cross- sectional area of \(1130 \mathrm{~mm}^{2}\left(1.75 \mathrm{in} .^{2}\right)\) is subjected to an \(\mathrm{ex}\) ternal tensile load. If the stresses sustained by the fiber and matrix phases are \(156 \mathrm{MPa}\) \((22,600 \mathrm{psi})\) and \(2.75 \mathrm{MPa}(400 \mathrm{psi})\), respectively; the force sustained by the fiber phase is \(74,000 \mathrm{~N}\left(16,600 \mathrm{lb}_{6}\right)\); and the total longitudinal strain is \(1.25 \times 10^{-3}\), determine (a) the force sustained by the matrix phase, (b) the modulus of elasticity of the composite material in the longitudinal direction, and (c) the moduli of elasticity for fiber and matrix phases.

(a) List four reasons why glass fibers are most commonly used for reinforcement. (b) Why is the surface perfection of glass fibers so important? (c) What measures are taken to protect the surface of glass fibers?

16.8 A continuous and aligned fiber-reinforced composite is to be produced consisting of 30 vol \(\%\) aramid fibers and 70 vol\% of a polycarbonate matrix; mechanical characteristics of these two materials are as follows: \begin{tabular}{lcc} \hline & Modulus of Elasticity [GPa (psi)] & Tensile Strength \([\) MPa (psi)] \\\ \hline Aramid fiber & \(131\left(19 \times 10^{6}\right)\) & \(3600(520,000)\) \\ Polycarbonate & \(2.4\left(3.5 \times 10^{5}\right)\) & \(65(9425)\) \\ \hline \end{tabular} Also, the stress on the polycarbonate matrix when the aramid fibers fail is \(45 \mathrm{MPa}\) (6500 psi). For this composite, compute (a) the longitudinal tensile strength, and

16.25 (a) What is a hybrid composite? (b) List two important advantages of hybrid composites over normal fiber composites.

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