Page 172 - Marks Calculation for Machine Design
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P1: Shibu
                                      14:25
                          January 4, 2005
        Brown.cls
                 Brown˙C04
                                           STRENGTH OF MACHINES
                  154
                        TABLE 4.2
                        Element  Summary of the Pressure Loadings  Shear stress (τ)
                                             Normal stress (σ)
                                                p i r m
                        Thin-wall sphere   σ sph =                     —
                                                2 t
                        Thin-wall cylinder:
                                                p i r m
                         Axial             σ axial =                   —
                                                 2 t
                                                p i r m
                         Hoop              σ hoop =                    —
                                                  t
                        Thick-wall cylinder: (p o = 0)
                                               p i r 2          2
                         Tangential        σ t =  i  1 +  r o          —
                                              r − r 2 i  r
                                               2
                                               o
                                               p i r  2        r o    2
                         Radial            σ r =  i  1 −               —
                                               2
                                              r − r i 2  r
                                               o
                                                p i r  2
                         Axial             σ a =  i                    —
                                               2
                                               r − r 2 i
                                               o
                  of the element, meaning ( x z) or ( y z). The dimension ( z) is very much smaller
                  than either ( x) or ( y) so that it can be assumed that there is no variation in the stresses
                  perpendicular to the plane of the stress element, meaning in the z direction.
                                         y               y
                                                    ∆y         z
                                                 x
                                                         ∆z
                                          ∆x
                                   FIGURE 4.1  Geometry of a plane stress element.
                    The standard nomenclature and sign conventions for both normal stress (σ) and shear
                  stress (τ) for a plane stress element are shown in Fig. 4.2, where positive normal stress (σ)
                  is directed outward from the element. Therefore, pressure (p i ) is a negative stress.
                                             s yy              s yy
                                               t xy
                                                            t xy •
                                                   t yx         t yx
                                  s xx
                                                           s xx  •
                                                     s xx         p i
                                     t yx
                                                            t xy  ×
                                        t xy
                                             s yy               s yy

                                  FIGURE 4.2  Plane stress element.
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