Page 173 - Marks Calculation for Machine Design
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                                      14:25
                          January 4, 2005
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                 Brown˙C04
                                            COMBINED LOADINGS
                                                                                  155
                      The first subscript on the stresses shown in Fig. 4.2 indicates the direction of the stress,
                    and the second subscript indicates the direction of the perpendicular to the surface area on
                    which the stress acts. For the shear stresses shown, (τ xy ) and (τ yx ) are interchangeable, so
                    only (τ xy ) will be used in the remainder of this book. As mentioned earlier, and as shown in
                    Fig. 4.2, the internal pressure (p i ) acts perpendicular to the plane stress element; however,
                    it is directed toward the surface of the element and so it is considered a negative normal
                    stress. More about the effect of an internal pressure on the overall stress distribution on an
                    element is presented in Chap. 5.
                      Although Fig. 4.2 shows the worst case senario for a stress element, and as mentioned ear-
                    lier a very rare occurrence in actual engineering practice, there are three special plane stress
                    elements. These three elements are called uniaxial stress element, biaxial stress element,
                    and pure shear stress element. These three elements have special significance that will be
                    discussed in Chap. 5.
                    Uniaxial Stress Element. For the fundamental loadings of axial, thermal, and bending, a
                    uniaxial stress element is produced and shown in Fig. 4.3,
                                     0
                                       0
                                          0
                         s xx                            s
                                                                               s
                                             s xx
                                                     ←
                             0
                               0                                  Uniaxial
                                     0
                        FIGURE 4.3  Uniaxial stress element.
                    where there is only normal stress (σ) along the axis of interest; and the other stresses, the
                    normal stress (σ yy ) and the four shear stresses (τ xy ), are zero.

                    Biaxial Stress Element. For the pressure loadings on thin-walled vessels, both spherical
                    and cylindrical, and thick-walled cylinders, a biaxial stress element is produced and shown
                    in Fig. 4.4,
                                    s yy                           s hoop  or s t
                                      0
                                         0
                        s xx
                                                Æ
                                            s xx    s axial  or s a      s axial  or s a
                             0
                              0
                                                         Biaxial
                                    s yy                           s hoop  or s t
                        FIGURE 4.4  Biaxial stress element.
                    where there are the normal stresses (σ axial ) or (σ a ) in the x-direction, along the axis of
                    interest, and the normal stresses (σ hoop ) or (σ t ) in the y-direction, perpendicular to the axis of
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