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Chapter 2 Macromechanical Analysis of a Lamina Review of Definitions Dr. Autar Kaw Department of Mechanical Engineering University of South Florida, Tampa, FL 33620 Courtesy of the Textbook Mechanics of Composite Materials by Kaw
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FIGURE 2.5 Stresses on infinitesimal area on an arbitrary plane
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FIGURE 2.6 Forces on an infinitesimal area on the y-z plane
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FIGURE 2.7 Stresses on an infinitesimal cuboid
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FIGURE 2.8 Normal and shearing strains on an infinitesimal area in the x-y plane
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u = u(x,y,z) = displacement in x-direction at point (x,y,z), v = v(x,y,z) = displacement in y-direction at point (x,y,z), w = w(x,y,z) = displacement in z-direction at point (x,y,z) Where:
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Substituting
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u = u(x,y,z) = displacement in x-direction at point (x,y,z), v = v(x,y,z) = displacement in y-direction at point (x,y,z), w = w(x,y,z) = displacement in z-direction at point (x,y,z) Where:
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Substituting
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Where:
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Substituting
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FIGURE 2.9 Cartesian coordinates in 3-D
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Where:
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