In an aligned and continuous carbon fiber-reinforced nylon 6,6 composite, the fibers are to carry 94 % of a load applied in the longitudinal direction. i Carbon fiber Nylon 6,6 (a) Using the data provided, determine the volume fraction of fibers that will be required. i Modulus of Elasticity [GPa(psi)] 260 (37 ×106) 2.8 (4.0×105) Tensile Strength [MPa(psi)] 4000 (5.8×105) 76 (11,000) (b) What will be the tensile strength of this composite? Assume that the matrix stress at fiber failure is 50 MPa (7250 psi). MPa

In an aligned and continuous carbon fiber-reinforced nylon 6,6 composite, the fibers are to carry 94 % of a load applied in the longitudinal direction. i Carbon fiber Nylon 6,6 (a) Using the data provided, determine the volume fraction of fibers that will be required. i Modulus of Elasticity [GPa(psi)] 260 (37 ×106) 2.8 (4.0×105) Tensile Strength [MPa(psi)] 4000 (5.8×105) 76 (11,000) (b) What will be the tensile strength of this composite? Assume that the matrix stress at fiber failure is 50 MPa (7250 psi). MPa

Elements Of Electromagnetics

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ISBN:9780190698614

Author:Sadiku, Matthew N. O.

Publisher:Sadiku, Matthew N. O.

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Concept explainers

The Space Lattice and Unit Cells

Every matter consists of atoms, molecules, and ions. If these atoms, molecules, and ions (micro-particles) are represented in a three-dimensional space-occupying certain specific points in space, then these arrangements are termed as space lattices and the specific points which are being occupied by atoms, molecules and ions are termed as lattice points. The atoms, molecules, and ions at the lattice points are generally grouped in a regular fashion and repeat periodically at the three-dimensional space.

Question

In an aligned and continuous carbon fiber-reinforced nylon 6,6 composite, the fibers are to carry 94 % of a load applied in the
longitudinal direction.
i
Carbon fiber
Nylon 6,6
(a) Using the data provided, determine the volume fraction of fibers that will be required.
i
Modulus of Elasticity [GPa(psi)]
260 (37 ×106)
2.8 (4.0×105)
Tensile Strength [MPa(psi)]
4000 (5.8×105)
76 (11,000)
(b) What will be the tensile strength of this composite? Assume that the matrix stress at fiber failure is 50 MPa (7250 psi).
MPa

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