16.29 Briefly describe laminar composites. What is the prime reason for fabricating these materials?

Short Answer

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Answer: The prime reason for fabricating laminar composites is to obtain a combination of properties that cannot be achieved with a single material, allowing for the creation of a material that is specifically tailored for a particular application or performance requirement.

Step by step solution

01

Define laminar composites

Laminar composites are materials that are formed by bonding layers of different materials together. These layers, or laminae, are often bonded using an adhesive or with heat and pressure. Laminar composites can have a variety of different layered structures, but they generally consist of two or more materials in parallel orientation.
02

Describe the properties of laminar composites

Laminar composites typically have improved properties compared to their individual components. This is achieved by combining the desirable properties of each layer or material in the composite. For example, one layer might contribute strength or stiffness, while another layer provides flexibility or reduces weight. The overall properties of the composite depend on the properties of its individual layers as well as the bonding method used to join them.
03

Explain the prime reason for fabricating laminar composites

The prime reason for fabricating laminar composites is to obtain a combination of properties that cannot be achieved with a single material. By combining different materials with individual desirable properties, laminar composites allow for the creation of a material that is specifically tailored for a particular application or performance requirement. This customization can lead to improved performance, reduced weight, or increased durability compared to using a single material alone.
04

Provide examples of laminar composites

Some common examples of laminar composites include: 1. Fiberglass: A composite made from layers of woven glass fibers bonded together with a resin, often used in the aerospace industry for its lightweight and high strength properties. 2. Carbon fiber composites: Layers of carbon fibers embedded in a polymer matrix, used in various industries due to their excellent strength-to-weight ratio. 3. Plywood: Made from layers of wood veneers bonded together, with alternating grain directions to increase strength and resistance to warping. 4. Sandwich panels: Layers of lightweight core materials, such as foam, sandwiched between layers of stiffer, stronger skin materials like metal or fiber-reinforced composites, often used in construction or transportation applications due to their lightweight and high-strength properties.

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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 by combining two or more constituent materials with significantly different physical or chemical properties. The constituents retain their identities in the composite, meaning they do not dissolve or merge completely but interact at a microscopic level to enhance overall performance. One familiar example you might recognize is concrete, which combines cement with gravel and sand. Each constituent, such as the stiff fibers and the matrix in carbon fiber composites, offers a specific attribute that, when integrated, allows the composite material to achieve performance levels unattainable by any single material.

Imagine a superhero team where each member has unique powers—when they combine forces, they can tackle challenges that none of them could handle alone. This is similar to how composite materials work; each ingredient brings its 'superpower' to create a final product that is strong, durable, lightweight, or even flexible. Designers and engineers choose composites for the precise mix of properties they provide, making them essential in a range of fields, from aeronautics to sporting equipment.
Properties of Laminar Composites
Laminar composites possess a set of key characteristics that elevate their application in various industries. Primarily, the directional arrangement of layers can be tailored to achieve desired mechanical properties such as enhanced strength, stiffness, or resistance to impact along specific axes. This can be comparable to the grain in wood, which is stronger along one direction than the other.

Anisotropy

In the case of laminar composites, this property is called anisotropy. It gives designers the freedom to engineer materials that align with the load-bearing patterns expected in their applications. For example, a skateboarding ramp may require different structural support along the length versus the width. The composite material could be designed with layers oriented accordingly to match these needs.

Thermal and Acoustic Insulation

Additionally, laminar composites can provide superior thermal and acoustic insulation, thanks in part to the presence of air or foam layers within their structure. These layers disrupt heat transfer and sound waves, making such composites ideal for building applications or automotive components.

Furthermore, the customized combination of materials often leads to an overall structure that is lightweight but durable—a balance that is particularly advantageous in transportation and mobile equipment. The unique fusion of layered materials, paired with bonding methods such as adhesives, heat, or pressure, result in composites with a versatility that single-material counterparts simply cannot match.
Applications of Laminar Composites
The versatility of laminar composites sees them employed in a vast array of sectors. Their ability to be lightweight yet strong makes them ideal for the aerospace industry, where every kilogram saved can contribute significantly to fuel savings and overall efficiency. Airplanes and spacecraft benefit greatly from materials like carbon fiber composites, which combine strength and reduced weight.

Sports Equipment

Athletics sees widespread use of laminar composites as well. High-performance sports equipment such as tennis rackets, bicycles, and golf clubs often utilize these materials to deliver enhanced durability and power while minimizing weight. The specific layering patterns can be engineered to optimize energy transfer during a swing or shot, providing athletes with an edge in competition.

The unique properties of laminar composites, like those found in sandwich panels, make them particularly useful in the construction industry. These panels can serve as an integral part of walls or flooring systems—offering strength, insulation, and durability without the burden of excessive weight. In transportation, the attributes of laminar composites contribute to lighter, more fuel-efficient vehicles, contributing to reduced emissions and operating costs over time.

These applications are just a snapshot of where laminar composites make an impact. Their tailored properties and performance make them essential in the pursuit of technological advancements across various fields, proving that the prime reason for their fabrication—to create materials with custom characteristics—is not only met but exceeded.

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Most popular questions from this chapter

16.30 (a) Briefly describe sandwich panels. (b) What is the prime reason for fabricating these structural composites? (c) What are the functions of the faces and the core? to be aligned parallel to the tube axis. The applied load, maximum fiber volume fracuser is allowed to input values for the foltion, elastic moduli of matrix and all fiber lowing parameters: inside and outside tube materials, densities of matrix and fiber diameters, tube length, maximum deflecmaterials, and cost per unit mass for the tion at the axial midpoint for some given matrix and all fiber materials.

\(16.16\) It is desired to produce an aligned carbon fiber-epoxy matrix composite having a longitudinal tensile strength of 750 MPa (109,000 psi). Calculate the volume fraction of fibers necessary if (1) the average fiber diameter and length are \(1.2 \times 10^{-2} \mathrm{~mm}\) (4.7 \(\times 10^{-4}\) in. \()\) and \(1 \mathrm{~mm}(0.04\) in. \()\), respectively; (2) the fiber fracture strength is \(5000 \mathrm{MPa}\) \((725,000 \mathrm{psi}) ;\) (3) the fiber-matrix bond strength is 25 MPa (3625 psi); and (4) the matrix stress at fiber failure is \(10 \mathrm{MPa}\) \((1450 \mathrm{psi})\)

(a) What is the distinction between cement, and concrete? (b) Cite three important limitations that restrict the use of concrete as a structural material. (c) Briefly explain three techniques that, are used to strengthen concrete by reinforcement.

16.12 In an aligned and continuous glass fiberreinforced nylon 6,6 composite, the fibers are to carry \(94 \%\) of a load applied in the longitudinal direction. (a) Using the data provided, determine the volume fraction of fibers that will be required. (b) What will be the tensile strength of this composite? Assume that the matrix stress at fiber failure is 30 MPa (4350 psi). \begin{tabular}{lcc} \hline & Modulus of Elasticity ofensile [GPa (psi)] & Strength [MPa(psi)] \\ \hline Glass fiber & \(72.5\left(10.5 \times 10^{6}\right)\) & \(3400(490,000)\) \\\ Nylon 6,6 & \(3.0\left(4.35 \times 10^{5}\right)\) & \(76(11,000)\) \\ \hline \end{tabular}

.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 \(\left[E_{m}=2.5 \mathrm{GPa}\left(3.6 \times 10^{5} \mathrm{psi}\right)\right]\)

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