1. Given a graphite/epoxy lamina with fiber orientation angle = 60 degrees, with the strength properties listed below and subjected to a state of stress {σ x, σ y, T xy}
= {2B, -3B, 4B} where B is some variable to be determined.
a. Draw a complete and correct FBD for this lamina.
b. Using Tsai-Wu Failure criterion, find the value of B that causes failure of this lamina.
Material Properties: Xt = 1500 MPa, Xc = 1500 MPa, Yt = 40 MPa, Yc
= 246 MPa, S = 68 MPa
Approximate answer: B = 21 +/- 10% (units you figure out)
1. Given a graphite/epoxy lamina with fiber orientation angle = 60 degrees, with the strength properties...
235 Find the off-axis shear strength and mode of failure of a 60 boron/ epoxy lamina. Use the properties of a unidirectional boron/epoxy lamina from Table 2.1. Apply the maximum stress failure, maximum strain, Tsai-Hill, and Tsai-Wu failure theories. TABLE 2.1 Tvpical Mechanical Properties of a Unidirectional Lamina (SI System of Units) Glass Boron/ Graphite/ Property SymbolUnits epoxy epoxy epoxy Fiber volume fraction Longitudinal elastic modulus Transverse elastic modulus Major Poisson's ratio Shear modulus Ultimate longitudinal tensile strength Ultimate longitudinal...
Consider a single lamina of unidirectional kevlar-epoxy with a
fiber orientation angle of 55 degress . You may use a computer or
do the calculations by hand but must show your work. Use the lamina
properties provided in Lesson 3, Slide 19 in SI units. The lamina
is loaded with stresses {x, y,
xy} = {125, -10,
20} MPa. a. Sketch a complete and useful figure for this problem,
including all relevant coordinate systems. b. Calculate the strains
in the...
We have a filament-wound pressure vessel fabricated from E-glass/epoxy with the strength properties as listed below. The diameter d 1 m, and wall thickness 20 mm. The vessel is subjected to an internal pressure, p. The fiber orientation囝囝= 53 degree. Determine the maximum internal pressure p, which would cause failure of the vessel according to (a) the maximum stress criterion and (b) the Tsai-Hill criterion (no need to solve "b" - we will learn Tsai-Hill failure criterion from Chapter #...
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...
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...
Composite Structures Tutorial 7 (week 8) 7.1 Find the five strength parameters of a unidirectional glass/epoxy lamina with 40% fiber volume fraction. Use the properties of glass and epoxy from Table 3.1 and Table 3.2. Assume the fibers have circular cross-section and are in a square array packing. 1-52.0-$01674870 225 47 Find 208 Mechanics of Composite Materials, Second Edi Convert PO or Excel Orl Select PDF I TABLE 3.1 Typical Properties of Fibers (SI System of Units) Units Graphite Glass...