Page 184 - Marks Calculation for Machine Design
P. 184

P1: Shibu
                          January 4, 2005
                 Brown˙C04
        Brown.cls
                  166
                            U.S. Customary 14:25  STRENGTH OF MACHINES  SI/Metric
                  Step 2. Calculate the axial stress (σ axial ) using  Step 2. Calculate the axial stress (σ axial ) using
                  Eq. (4.1) as                       Eq. (4.1) as
                      σ axial = Eε axial               σ axial = Eε axial
                                                                       2
                                     2
                                                                   9
                                 6
                         = (30 × 10 lb/in )(0.00087)      = (207 × 10 N/m )(0.0008)
                                   2
                                                                        2
                         = 26,100 lb/in = 26.1 kpsi       = 165,600,000 N/m = 165.6MPa
                  Step 3. Calculate the thermal stress (σ thermal )  Step 3. Calculate the thermal stress (σ thermal )
                  from Eq. (4.2) as                  from Eq. (4.2) as
                      σ thermal = Eε T = Eα( T )        σ thermal = Eε T = Eα( T )
                                      2
                                  6
                                                                         2
                                                                      9
                           = (30 × 10 lb/in )                = (207 × 10 N/m )
                             ×(6.5 × 10 −06  in/in · F)        ×(12 × 10 −6  cm/cm · C)
                                                                             ◦
                                           ◦
                                                                   ◦
                                ◦
                             ×(80 F)                           ×(45 C)
                           = 15,600 lb/in 2                  = 111,800, 000 N/m 2
                           = 15.6 kpsi                       = 111.8MPa
                  Step 4. Combine the axial stress (σ axial ) from  Step 4. Combine the axial stress (σ axial ) from
                  step 2 and the thermal stress (σ thermal ) from  step 2 and the thermal stress (σ thermal ) from
                  step 3 using Eq. (4.3) to give the maximum  step 3 using Eq. (4.3) to give the maximum
                  stress (σ xx ) as                  stress (σ xx ) as
                       σ xx = σ axial + σ thermal        σ xx = σ axial + σ thermal
                          = (26.1 kpsi) + (15.6 kpsi)      = (165.6MPa) + (111.8MPa)
                          = 41.7 kpsi                      = 277.4MPa
                  Step 5. Display the answer for the maximum  Step 5. Display the answer for the maximum
                  stress (σ xx ) found in step 4, in kpsi, on a plane  stress (σ xx ) found in step 4, in MPa, on a plane
                  stress element.                    stress element.
                                   0                               0
                            0                                0
                       41.7                41.7        277.4               277.4


                                       0                                0

                                   0                               0
                    The above diagram will be a starting point  The above diagram will be a starting point
                  for the discussions in Chap. 5.    for the discussions in Chap. 5.
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