Page 314 - Marks Calculation for Machine Design
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P1: Shashi
                          January 4, 2005
                                      15:4
        Brown.cls
                 Brown˙C07
                                           STRENGTH OF MACHINES
                  296
                  solution
                  Step 1. Using Eq. (7.8) and values for the coefficient (a) and exponent (b) from Table 7.1,
                  calculate the surface finish factor (k a ) as
                                b                   −0.085
                          k a = aS ut  = (1.58 MPa)(595 MPa)  = (1.58)(0.5810) = 0.92
                  Step 2. Using Eq. (7.12) calculate the effective diameter (d e ) as


                                                                             2
                       d e = 0.808 (bh) 1/2  = 0.808 (0.16 cm)(1.25 cm) = (0.808) (0.20 cm )
                         = (0.808)(0.4472 cm) = 0.361 cm = 3.61 mm
                  Step 3. Using Eq. (7.10) calculate the size factor (k b ) as
                                    −0.1133      −0.1133

                                d e         3.61              −0.1133
                                                                         ∼
                         k b =           =             = (0.474)   = 1.09 = 1
                               7.62         7.62
                   Step 4. As the beam is in bending the load type factor (k c ) from Eq. (7.14) is
                                                k c = 1
                  Step 5. As the beam is operating at room temperature, the temperature factor (k d ) from
                  Eq. (7.15) and Table 7.2 is
                                                k d = 1
                  Step 6. Using the given reduced stress concentration factor (K f ), calculate the miscella-
                  neous effect factor (k e ) using Eq. (7.16) as
                                               1    1
                                          k e =  =    = 0.83
                                              K f  1.2
                  Step 7. Using the given ultimate tensile stress (S ut ) and the guidelines in Eq. (7.1), calculate
                  the test specimen endurance limit (S ) as

                                            e

                                 S = 0.504 S ut = (0.504)(595 MPa) = 300 MPa
                                  e
                  Step 8. Using the test specimen endurance limit (S ) found in Step 7 and the modifying

                                                        e
                  factors found in Steps 1 through 6, calculate the endurance limit (S e ) for the cantilevered
                  beam using the Marin equation in Eq. (7.7) as

                              S e = k a k b k c k d k e S = (0.92)(1)(1)(1)(0.83)(300 MPa)
                                            e
                                = (0.764)(300 MPa) = 229.1MPa
                  Step 9. Calculate the mean force (F m ) and the alternating force (F a ) as
                                F max + F min  (25.2N) + (10.8N)  36 N
                           F m =          =                 =      = 18 N
                                    2              2            2
                                F max − F min  (25.2N) − (10.8N)  14.4N
                            F a =         =                 =       = 7.2N
                                    2              2            2
                  Step 10. Calculate the mean bending moment (M m ) and the alternating bending moment
                  (M a ) as
                             M m = F m L = (18 N)(6cm) = 108 N · cm = 1.08 N · m
                              M a = F a L = (7.2N)(6cm) = 43.2N · cm = 0.43 N · m
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