Chapter 16: Problem 28
Briefly describe pultrusion, filament winding, and prepreg production fabrication processes; cite the advantages and disadvantages of each.
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Chapter 16: Problem 28
Briefly describe pultrusion, filament winding, and prepreg production fabrication processes; cite the advantages and disadvantages of each.
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(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 \(V_{f}\) ?
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 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
Briefly describe laminar composites. What is the prime reason for fabricating these materials?
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).
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