Page 208 - Marks Calculation for Machine Design
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                          January 4, 2005
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                                           STRENGTH OF MACHINES
                  190
                       PRINCIPAL STRESSES
                  5.2
                  Suppose the element in Fig. 5.1 that is assumed to be aligned along some natural direction
                  of a machine, such as the center of a shaft, or thick-walled cylinder, or along the axis of
                  a beam that is modeling the machine, is rotated counterclockwise an angle (θ). A new set
                  of normal and shear stresses will act on the plane stress element. This rotated element is
                  shown in Fig. 5.2, where the new coordinate axes and stresses are denoted by primes and
                  labeled (σ x x ),(σ y y ), and (τ x y ).



                                                          y¢
                                                                y
                                    s yy                s
                                      t xy              y¢y¢   t x¢y¢   t x¢y¢
                                                                     s x¢x¢   x¢
                                         t xy
                        s xx                                            q
                                                                           x
                                            s xx    s
                           t xy                      x¢x¢
                                                         t
                              t xy                        x¢y¢
                                                             t x¢y¢
                                                                    s y¢y¢
                                    s yy
                        FIGURE 5.2  Rotated plane stress element.
                    If the all the stresses in Fig. 5.2 are multiplied by the appropriate area over which each
                  acts, a set of forces acting on the rotated and unrotated elements will result. Furthermore,
                  if equilibrium is to be satisfied for both the rotated and unrotated elements, then a set of
                  relationships can be established between the rotated and unrotated stresses. Leaving out the
                  development with its bzillion algebra and trig steps, these relationships between the rotated
                  and unrotated stresses are given in the following three equations:
                                      σ xx + σ yy  σ xx − σ yy
                                σ x x =       +         cos 2θ + τ xy sin 2θ   (5.1)

                                         2         2
                                      σ xx + σ yy  σ xx − σ yy
                                σ y y =       −         cos 2θ − τ xy sin 2θ   (5.2)

                                         2         2
                                       σ xx − σ yy
                                τ x y =−       sin 2θ + τ xy cos 2θ            (5.3)

                                           2
                    Consider the following manufacturing process to see how these relationships provide
                  important design information.
                    One of the ways thin-walled cylindrical pressure vessels are manufactured is by passing
                  steel plate through a set of compression rollers creating a circular piece of steel that can
                  then be welded along the resulting seams. Such a vessel is shown in Fig. 5.3.
                                          Weld seams
                                                  q
                                                       Weld angle
                        FIGURE 5.3  Welded cylindrical pressure vessel.
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