Chapter 16: Problem 29
Briefly describe laminar composites. What is the prime reason for fabricating these materials?
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Chapter 16: Problem 29
Briefly describe laminar composites. What is the prime reason for fabricating these materials?
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(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?
(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?
(a) What is the distinction between matrix and lispersed phases in a composite material? b) Contrast the mechanical characteristics of natrix and dispersed phases for fiber-reinforced composites.
A continuous and aligned fibrous reinforced composite having a cross-sectional area of \(970 \mathrm{~mm}^{2}\) (1.5 in. \(\left.^{2}\right)\) is subjected to an external tensile load. If the stresses sustained by the fiber and matrix phases are 215 MPa (31,300 psi) and \(5.38\) MPa (780 psi), respectively, the force sustained by the fiber phase is \(76,800 \mathrm{~N}\left(17,265 \mathrm{lb}_{\mathrm{f}}\right)\), and the total longitudinal composite strain is \(1.56 \times 10^{-3}\), determine the following: (a) The force sustained by the matrix phase (b) The modulus of elasticity of the composite material in the longitudinal direction (c) The moduli of elasticity for fiber and matrix phases
(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.
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