Chapter 16: Problem 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?
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Chapter 16: Problem 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?
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A continuous and aligned fiber-reinforced composite is to be produced consisting of 45 vol\% aramid fibers and 55 vol \(\%\) polycarbonate matrix; the mechanical characteristics of these two materials are as follows: The stress on the polycarbonate matrix when the aramid fibers fail is \(35 \mathrm{MPa}\) (5075 psi). For this composite, compute the following: (a) The longitudinal tensile strength (b) The longitudinal modulus of elasticity
(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?
Estimate the maximum and minimum thermal conductivity values for a cermet that contains 90 vol titanium carbide (TiC) particles in a nickel matrix. Assume thermal conductivities of 27 and \(67 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\) for \(\mathrm{TiC}\) and Ni, respectively.
(a) From the moduli of elasticity data in Table \(16.2\) for glass fiber- reinforced polycarbonate com- posites, determine the value of the fiber efficiency parameter for each of 20,30 , and 40 vol\% fibers. (b) Estimate the modulus of elasticity for 50 vol \(\%\) glass fibers.
Compute the longitudinal tensile strength of an aligned glass fiber-epoxy matrix composite in which the average fiber diameter and length are \(0.015 \mathrm{~mm}\left(5.9 \times 10^{-4}\right.\) in. \()\) and \(2.0 \mathrm{~mm}(0.08\) in. \()\), respectively, and the volume fraction of fibers is \(0.25\). Assume that (1) the fiber-matrix bond strength is \(100 \mathrm{MPa}(14,500 \mathrm{psi}),(2)\) the fracture strength of the fibers is \(3500 \mathrm{MPa}\left(5 \times 10^{5} \mathrm{psi}\right)\), and (3) the matrix stress at composite failure is \(5.5 \mathrm{MPa}(800 \mathrm{psi})\).
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