Answer:
Part (a)
Eₓ = 142.1 GPa
Part (b)
Load carried by carbon fiber = 98.5%
Part (c)
F (fiber) = 14776.1 N
F (matrix) = 221.63 N
Step-by-step explanation:
Given data:
Carbon-Epoxy composite
Carbon fibers = 40%
Epoxy fibers = 60%
Modulus of elasticity of carbon fibers = 350 GPa
Modulus of elasticity of Epoxy fibers = 3.5 GPa
Longitudinal stress = 60 MPa
Cross-sectional area = 250 mm^2
Solution:
Part (a)
Modulus of Elasticity of composite material = Eₓ = E₁V₁ + E₂V₂
Eₓ = Modulus of Elasticity of composite material
E₁ = Modulus of Elasticity of carbon fibers
V₁ = % of carbon fibers
E₂ = Modulus of Elasticity of epoxy fibers
V₂ = % of epoxy fibers
Eₓ = 350*0.4 + 3.5*0.6
Eₓ = 142.1 GPa
Part (b)
Load carried by carbon fiber
Put,
V composite = 1
E composite = 142.1 GPa
E carbon = 350 GPa
V carbon = 0.4
= (350*0.4) / (142.1*1)
= 0.985
Load carried by carbon fiber = 98.5%
Part (c)
First calculate ratio of fiber load to matrix load
= (350*0.4) / (3.5*0.6) (F represents force or load)
= 66.67 ................... Eq (1)
Total force sustained by composite material
= Applied stress * Cross-sectional area
Fₓ = 60 MPa * 250 mm^2
Fₓ = 15,000 N
This total load is carried by both fibers and matrix phases. So,
Fₓ = F (fiber) + F (matrix)
Put values in above equation
15,000 = (66.67 * F (matrix)) + F (matrix)
15,000 = 67.67 F (matrix)
F (matrix) = 221.63 N
Put F (matrix) = 221.63 N in equation (1)
F (fiber) = 221.63 * 66.67
F (fiber) = 14776.1 N