Ans) We know,
Longitudinal stiffness () = +
where, = Modulus of elasticity of fiber = 72.5 GPa
= Modulus of elastisity of matrix = 3 GPa
= Volume fraction of fiber = 42% or 0.42
= Volume fraction of matrix = 1 - 0.42 = 0.58
=> = 72.5(0.42) + 3(0.58)
=> = 32.19 GPa
Hence, longitudinal stiffness of composite is 32.19 GPa
QUESTION 23 The data in the table below is for glass fibre-reinforced nylon 6,6 composites. The...
Question 1. A continuous and aligned fibre-reinforced composite material is to be produced consisting of 40 vol % glass fibres and 60 vol % of an epoxy matrix. The mechanical characteristics of these two materials are as follows: MaterialModulus of Elasticity rcture Strength (GPa) (MPa) 2500 Glass Fibre 76 Epoxy 3.35 58 For this composite material, estimate by calculation the following parameters: i. The longitudinal tensile strength ii. The longitudinal modulus of elasticity
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. Modulus of Elasticity [GPa(psi)] Tensile Strength [MPa(psi)] Carbon fiber 260 (37 ×106) 4000 (5.8 ×105) Nylon 6,6 2.8 (4.0 ×105) 76 (11,000) (a) Using the data provided, determine the volume fraction of fibers that will be required. (b) What will be the tensile strength of this composite? Assume that the matrix stress at fiber failure...
Problem 8 10 pts) A continuous and aligned fiber-reinforced composite part has cross sectional area of 300 mm2 and consists of35 vol% glass fibers and 65 vol% of a nylon 6,6 matrix. If a longitudinal tensile load of 50kN is applied to the composite, determine (a) the longitudinal modulus of elasticity of the composite, (b) the longitudinal strain in the composite, (c) the stress in each phase (fiber and matrix), and (d) the magnitude of the load carried by each...
2. Consider unidirectionally reinforced glass/epoxy composites. The fibers are continuous and 60% by volume. The tensile strength of glass fibers is 1 GPa and the Young's modulus is 70 GPa. The tensile strength of the epoxy matrixis 60 MPa and its Young's modulus is 3GPa. Compute the Young's modulus and the tensile strength of the composite in the longitudinal direction.
Question B4 Carbon fibres typically have a modulus of 230 GPA, a tensile strength of 3.8 GPa and a density of 1.78 g cm3. In making composites, carbon fibres are often used with epoxy matrices that have a modulus of 3.0 GPa, a tensile strength of 60 MPa and a density of 1.3 g cm3. Which of the following is incorrect? (a) A carbon fibre/epoxy composite containing randomly oriented carbon fibres will have a lower modulus than one containing a...
A unidirectional continuous fibre reinforced composite is to be manufactured so that the fibres carry 90% of a load in the longitudinal direction. The moduli of elasticity of the fibre and matrix materials are 125 GPa and 2.6 GPa respectively. Determine: i) The volume fraction of fibres that will be required ii) The longitudinal and transverse elastic moduli of the resulting composite.
Please Answer this in full detailed as I am unable to get the full grasp of this topic a) Calculate the modulus of a cross-ply HS-carbon/epoxy laminate. Longitudinal fibre modulus (En)-230 GPa; transverse fibre modulus (E122)-20 GPa; matrix modulus (En)-3 GPa; fibre volume fraction (V) : 60%. [5 marks] b)(1) Explain the difference in failure of a single fibre in air and a single fibre embedded [5 marks] in a matrix. (2) How can a test that involves the fracture...
(b) For a unidirectional composite lamina with a 60% fibre volume fraction, the fibres are circular and are packed in a square array. Assume there is no void. The Young's modulus of the fibre is 180 GPa, the shear modulus of the fibre is 20 GPa. The Young's modulus of the matrix is 30 GPa, the shear modulus of the matrix is 4 GPa. The tensile strengths of fibre and matrix are 2000 MPa and 100 MPa separately. (1) Find...
A3. For polymer composites reinforced polymer composites, the resultant tensile strength is largely determined by the volume contents of fibers (as shown in the figure). If glass fibers are used for reinforcing (a) detemine the minimum volume content, Fmin, which will not cause multiple-fracture. [0.5 Marks] (b) detemine the minimum volume content, OFari, which will ensure that the strength of the composites is not less than that of neat epoxy. [0.5 Marks] an epoxy 60 GPa and tensile strenght a...
It is desired to produce an aligned carbon fibre-epoxy matrix composite having a longitudinal tensile strength of 462 MPa. Calculate the necessary volume fraction of fibres- Assume the following: (1) the average fibre diameter and length are 9.03 x 10 mm and 0.434 mm, respectively (2) the fibre fracture strength is 4.0 GPa (3) the fibre-matrix bond strength is 25 MPa (4) the matrix stress at composite failure is 70 MPa Express answers with three significant figures