Page 31 - Mechanical Engineer's Data Handbook
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20                                                  MECHANICAL  ENGINEER’S DATA  HANDBOOK


               Incomplete
               penetration






                                                  n
                                      I
                                      Incomplete penetration
                                                                          Cracking     Slag inclusions
                                                                      (due to poor weldability)

                                                                          Porosity
                         Bad profile              Improved profile
                                                                            Incomplete weld
               1.3.4   Stress concentration factors
              Stress  concentration  factors  are  given  for  various
              common discontinuities; for example, it can be seen   dJw   0.00  0.10  0.20  0.30  0.40  0.50  0.55
              that for a ‘wide plate’ with a hole the highest stress is 3
              times the nominal stress. General values are also given   K   3.00  3.03  3.14  3.36  3.74  4.32  4.70
              for keyways, gear teeth, screw threads and welds.
                                                          Note: In this case the area of maximum cross-section is
              Stress concentration  factor is defined as:   used.
                   Highest  value  of  stress  at  a  discontinuity
              K=
                 Nominal  stress  at  the  minimum  cross-section
              Plate with hole at centre of  width

              K = u,,$o;   a = PJwh
              a,,,   occurs at A and B.





                                                          Semi-injinite  plate with hole near  edge

                                                          a, = stress at A
                                                          nb = stress at B
                                                          n = stress away from hole
                                                          K,=aJa;  K,=oda


              r/c    0.00    0.10    0.20   0.30    0.40    0.50   0.60    0.70    0.80   0.85

              K,     3.00    3.05    3.15   3.25    3.40    3.70   4.12    4.85    6.12    7.15
              K,     3.00    3.03    3.07   3.10    3.15    3.18   3.25    3.32    3.42    3.50
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