A composite composed of graphite fibers in an epoxy matrix has a cross sectional area of 1.61 cm2, of which 63 percent is graphite fibers. The composite supports a total load of 15 402 kg in the direction of fiber alignment. Calculate the portion of the load in kg supported by the graphite fibers. For graphite fibers, E=400 GPa; For epoxy matrix, E=4.14 GPa.
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A composite composed of graphite fibers in an epoxy matrix has a cross sectional area of...
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...
A Graphite fiber-Polyester matrix composite has 20 % volume。 lume of the polyester matrix. The followi of fiber, and 80 % ing are the mechanical properties. Composite Graphite Fibers Polyester Matrix 100 % Volume Percent 80% 20 % 1.0 Volume Fraction E-34x 10 E 3 x 10 Elastic Moduļus (lb/ in a) In the Table above, fill in the volume fraction of the Graphite fibers and the Polyester matrix. Use the rule of mixtures, to calculate the Elastic Modulus of...
Q4
Acomposite consists of 65% polyester resin is reinforced by continuous and aligned glass fibers. The modulus elasticity of hardened resin is 4 0 GPa and the modulus elasticity of the ibers la 52.0 GPa. Compute: a. The overall modulus elasticity of composite in the longitudinal direction parallel 04. to fiber direction b. The load carried by each matrix and iber phase, If uniaxial srss of 50 MPa is applied in longitudinal direction on the 250 mm2 cross-sectional area. c....
5.30 La composite material, an epoxy matrix is reinforced with GY-70 Cype graphite fibers. The volumne percentage of fibers is 70%, and all are oriented in the same direction. For a sheet of this material in the X-Y planc, with fibers in the X-direction, strains $x = 0.005 and $y = 0.001 are measured. Estimate the applied stresses Ox and Oy
Continuous and aligned fiber-reinforced composite with cross-sectional area of 340 mm2 (0.53 in.2) is subjected to a longitudinal load of 50000 N (11200 Ibf). Assume Vf 0.3, Vm-0.7,Ef-131 GPa and Em 2.4 GPa (a) Calculate the fiber-matrix load ratio. (b) Calculate the actual load carried by fiber phase (c) Calculate the actual load carried by matrix phase (d) Compute the magnitude of the stress on the fiber phase (e) Compute the magnitude of the stress on the matrix phase (f)...
Q1: A fiberglass composite is composed of a matrix of vinyl ester and reinforcing fibers of E-glass. The volume fraction of E-glass is 31%. The remainder is vinyl ester. The density of the vinyl ester is 0.651 g/cm3, and its modulus of elasticity is 4.89 GPa. The density of E-glass is 2.685 g/cm3, and its modulus of elasticity is 71 GPa. A section of composite 1.00 cm by 25.00 cm by 200.00 cm is fabricated with the E-glass fibers running...
A continuous and aligned fiber-reinforced composite is to be produced consisting of 41 vol% aramid fibers and 59 vol% of a polycarbonate matrix; mechanical characteristics of these two materials are as follows: Modulus of Elasticity [GPa (psi)] Tensile Strength [MPa (psi)] Aramid fiber 131 (19 × 106) 3600 (520,000) Polycarbonate 2.4 (3.5 × 105) 65 (9425) Assume that this composite has a cross-sectional area of 320 mm2 (0.50 in.2) and is subjected to a longitudinal load of 49700 N (11200...
3. A [0/90]s graphite/epoxy laminate is subjected to a tensile normal load of 1N/m in the x- direction (the direction parallel to the fibers in the 0° ply). Assume the thickness of each ply is 5 mm and use properties of unidirectional graphite/epoxy lamina from the table. a) Calculate the resultant strains of the laminate b) Calculate the global stresses in the laminate c) Calculate the principal stresses (stresses in material directions) of the top layer. Typical Mechanical Properties of...
A unidirectional fiber reinforced composite is made from fibers and matrix with the following properties; (Ef= 400 GPa, Em = 4 GPa, modulus of elasticity of fiber and matrix respectively), (G12f= 170 GPa, Gm = 1.43 shear modulus of fiber and matrix), (V12f = 0.2, Vm = 0.4 for Poisson ratios of fiber and matrix respectively). a) Estimate the modulus of elasticity of a unidirectional lamina loaded along the fiber direction. b) Estimate the modulus of elasticity of a unidirectional...
2. For a graphite/epoxy unidirectional lamina (un-oriented lamina), find the following: ,--3 MPa 1) Compliance matrix 2) Stiffness matrix 3) Resultant strain under the applied stresses 12-4 MP 2 MPa τ12 Typical Mechanical Properties of a Unidirectional Lamina (SI System of Units) Glass Boron/ Graphitel epoxy epoxy Property Symbol Units epoxy Fiber volume fraction Longitudinal elastic modulus E Transverse elastic modulus E, Major Poisson's ratio Shear modulus Ultimate longitudinal tensile (σ1he 0.45 0.70 10.30 7.17 GPa GPa 38.6 8.27 18.50...