A continuous-aligned composite lamina is to be designed to have Ec,L= 200 GPa, Ec,T = 10Q3.GPa and o*c,L = 500 MPa. The desired failure strength of the fiber and matrix are o*f = 1000 MPaand o'm = 20 MPa. Calculate the following to design a composite lamina of desired stiffness andstrength;(a) fiber and matrix volume fractions(b) fiber and matrix elastic modulus(c) load fractions of fiber-composite and matrix-composite(d) the calculated stiffness of fiber and matrix correspond closely to which type of fiber andmatrix materials

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A continuous-aligned composite lamina is to be designed to have Ec,L= 200 GPa, Ec,T = 10 Q3. GPa and o*cL = 500 MPa. The desired failure strength of the fiber and matrix are o*t = 1000 MPa and o'm = 20 MPa. Calculate the following to design a composite lamina of desired stiffness and strength; %3D %3D

A continuous-aligned composite lamina is to be designed to have Ec,L= 200 GPa, Ec,T = 10 Q3. GPa and ocL = 500 MPa. The desired failure strength of the fiber and matrix are ot = 1000 MPa and o'm = 20 MPa. Calculate the following to design a composite lamina of desired stiffness and strength; %3D %3D

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Concept explainers

Processing of Polymer Matrix Composites

The polymer matrix composite is described as a composite material that contains some polymer in the form of either fibers or powder. Polymer matrix composites are also known in short as PMC's.

Question

A continuous-aligned composite lamina is to be designed to have Ec,L= 200 GPa, Ec,T = 10
Q3.
GPa and o*c,L = 500 MPa. The desired failure strength of the fiber and matrix are o*f = 1000 MPa
and o'm = 20 MPa. Calculate the following to design a composite lamina of desired stiffness and
strength;
(a) fiber and matrix volume fractions
(b) fiber and matrix elastic modulus
(c) load fractions of fiber-composite and matrix-composite
(d) the calculated stiffness of fiber and matrix correspond closely to which type of fiber and
matrix materials

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