Page 189 - Marks Calculation for Machine Design
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P1: Shibu
                                      14:25
                          January 4, 2005
        Brown.cls
                 Brown˙C04
                              U.S. Customary  COMBINED LOADINGS   SI/Metric       171
                    Step 5. Display the answers for the normal  Step 5. Display the answers for the normal
                    stress (σ xx ) found in step 3 and the shear stress  stress (σ xx ) found in step 3 and the shear stress
                    (τ xy ) found in step 4, in kpsi, on the top stress  (τ xy ) found in step 4, in MPa, on the top stress
                    element of Fig. 4.18.              element of Fig. 4.18.
                                    0                               0
                            3.8                            36.7
                         15.3               15.3        146.7                146.7


                                         3.8                             36.7

                                    0                               0
                      Again, this stress element diagram will be a  Again, this stress element diagram will be a
                    starting point for the discussions in Chap. 5.  starting point for the discussions in Chap. 5.

                    Example 6. Determine the maximum stresses  Example 6. Determine the maximum stresses
                    on the left element of a solid circular crank arm,  on the left element of a solid circular crank arm,
                    using Fig. 4.16 and the given information from  using Fig. 4.16 and the given information from
                    Example 5, where                   Example 5, where
                       P = 500 lb                         P = 2,250 N
                      L AB = 2ft = 24 in                L AB = 0.8 m
                      L BC = 1ft = 12 in                L BC = 0.4 m
                       R = 1.0 in                         R = 2.5 cm = 0.025 m
                    solution                           solution
                    Step 1. In step 4 of Example 5, the shear stress  Step 1. In step 4 of Example 5, the shear stress
                    (τ xy ) due to the torque (T AB ) was found to be  (τ xy ) due to the torque (T AB ) was found to be
                                                                        2
                                    2
                         τ xy = 3,820 lb/in = 3.8 kpsi    τ xy = 36,670,000 N/m = 36.7MPa
                    Step 2.  From Eq. (4.7), the shear force (V ) is  Step 2.  From Eq. (4.7), the shear force (V ) is
                    equal to the applied force (P)     equal to the applied force (P)
                              V = P = 500 lb                    V = P = 2,250 N
                    Step 3. Substitute the shear force (V ) and the  Step 3. Substitute the shear force (V ) and the
                    radius (R) in the second term on the third line  radius (R) in the second term of the third line
                    of Eq. (4.13) to give              of Eq. (4.13) to give
                              4 V    4 (500 lb)                4 V     4 (2,250 N)
                         τ xy =  2  =      2              τ xy =  3 πR 2  =  3 π(0.025 m) 2
                              3 πR   3 π(1.0in)
                              2,000 lb                          9,000 N
                            =      2                         =  0.00589 m 2
                              9.425 in
                                                                         2
                                   2
                            = 212 lb/in = 0.2 kpsi           = 1,528,000 N/m = 1.5MPa
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