Page 368 - Marks Calculation for Machine Design
P. 368

P1: Sanjay
                          January 4, 2005
                 Brown˙C08
        Brown.cls
                  350
                            U.S. Customary 15:14  APPLICATION TO MACHINES  SI/Metric
                  determine the maximum shear stress (τ max ) as  determine the maximum shear stress (τ max ) as

                                     2                                2

                            σ xx − σ yy  2                   σ xx − σ yy  2
                    τ max =          + τ xy          τ max =          + τ xy
                               2                                2

                                      2                                 2

                            (1.6) − (0)                      (11.25) − (0)
                                           2
                                                                              2
                       =              + (1.2 ) kpsi      =               + (8.44 ) MPa
                               2                                 2

                       =   (0.64) + (1.44 ) kpsi         =  (31.64) + (71.23 ) MPa
                         √                                 √
                       =   2.08 kpsi = 1.44 kpsi         =  102.87 kpsi = 10.14 MPa
                  Step 5. Substitute the average stress (σ avg )  Step 5. Substitute the average stress (σ avg )
                  from step 3 and the maximum shear stress  from step 3 and the maximum shear stress
                  (τ max ) from step 4 in Eq. (5.15) to determine  (τ max ) from step 4 in Eq. (5.15) to determine
                  the principal stress (σ 1 ) as     the principal stress (σ 1 ) as
                       σ 1 = σ avg + τ max               σ 1 = σ avg + τ max
                          = (0.8 kpsi) + (1.44 kpsi)       = (5.63 MPa) + (10.14 MPa)
                          = 2.24 kpsi                      = 15.77 MPa
                  Fillet Welds.  For fillet welds, the two parts to be joined together are placed such that
                  right-angle corners are created as shown in Fig. 8.8, where (t) is the weld size and (H) is
                  the weld throat. Not shown is the weld length (L), which is a dimension perpendicular to
                  the page.
                                                  H
                                                           t
                              P
                                                        t
                                                                      P
                             FIGURE 8.8  Fillet welds for a lap joint.

                    The tensile force (P) is balanced by a shear stress (τ fillet ) acting over the effective areas
                  of both fillet welds, where each effective area is given by Eq. (8.70) as
                                                     ◦
                                    A fillet = HL = (t cos 45 ) L = 0.707 tL    (8.70)
                    Using the effective area of one weld given in Eq. (8.70), the shear stress (τ fillet ) for the
                  lap joint shown in Fig. 8.8 is given by Eq. (8.71) as
                                      P       P         P           P
                              τ fillet =   =      =             =               (8.71)
                                    2 A fillet  2 (HL)  2 (0.707 t)( L)  1.414 tL
                    If there had been only one weld, then the shear stress (τ fillet ) would be twice the value
                  calculated from Eq. (8.71).
                    Consider the fillet welds in Fig. 8.9 where the transverse load (P) is balanced by a shear
                  stress (τ fillet ) over the two weld strips of length (L) having a weld size (t).
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