Page 176 - Marks Calculation for Machine Design
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P1: Shibu
                          January 4, 2005
                                      14:25
        Brown.cls
                 Brown˙C04
                  158
                                           STRENGTH OF MACHINES
                                    Stress element  T
                                                          R
                                                       r = 0
                                    FIGURE 4.9  Element for maximum stress.


                    Figure 4.9 is a view down the axis of the shaft, showing the torque (T ) acting counter-
                  clockwise. The darkened rectangle is at a radius (R) and the dimension of the element in
                  the radial direction is assumed to be much smaller than the other two dimensions, which is
                  the primary requirement of plane stress analysis.
                    For many of the other load combinations, locating the plane stress element of greatest
                  interest will be more difficult, and in fact there may be several elements from which to
                  choose a worse case senario for your design.
                    Although it will be a review on the stress equations, consider the following example to
                  show how combinations of loadings will result in actual quantitative information.



                            U.S. Customary                       SI/Metric
                  Example 1. Determine the maximum stresses  Example 1. Determine the maximum stresses
                  due to a combination of axial and torsion loads  due to a combination of axial and torsion loads
                  on a solid shaft, where            on a solid shaft, where
                    P = 10 kip = 10,000 lbs            P = 45 kN = 45,000 N
                    T = 5,000 ft · lb = 60,000 in · lb  T = 7,500 N · m
                    D = 4.0 in = 2 R                   D = 10.0 cm = 0.1 m = 2 R
                  solution                           solution
                  Step 1. Calculate the cross-sectional area (A)  Step 1. Calculate the cross-sectional area (A)
                  of the shaft.                      of the shaft.
                                                              2
                           2
                                                                       2
                                    2
                      A = π R = π(2.0in) = 12.57 in 2   A = π R = π(0.05m) = 0.008 m 2
                  Step 2. Substitute this cross-sectional area and  Step 2. Substitute this cross-sectional area and
                  the force (P) in the equation for axial stress to  the force (P) in the equation for axial stress to
                  give                               give
                             P  10,000 lb                    P   45,000 N
                         σ =  =                          σ =   =
                             A  12.57 in 2                   A   0.008 m 2
                                                                       2
                                  2
                          = 796 lb/in = 0.8 kpsi           = 5,625,000 N/m = 5.6MPa
                  Step 3. Calculate the polar moment of inertia  Step 3. Calculate the polar moment of inertia
                  (J) for the shaft.                 (J) for the shaft.
                            1  4  1       4                   1   4  1       4
                        J =  π R =  π(2.0in)              J =  π R =  π(0.05 m)
                            2     2                           2      2
                          = 25.13 in 4                      = 0.0000098 m 4
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