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136                                Chapter 8  Failure Analysis



                                         The distortion energy theory is another popular theory.
                              With the von-Mises criterion, the theory states that,
                                                      max     yield

                              where  max  is the maximum von-Mises stress.
                                         It is noted that the maximum stresses above are reduced
                              by the safety factor  n  for problems in application.


                              8.1   Buckling

                                  8.1.1  Fundamentals

                                         Buckling is a common failure of frame structure caused
                              by too high compressive loading.  Beam buckling is an academic
                              example often shown in undergraduate class because it is easy to
                              understand.  A beam with the length of L and moment of inertia of
                              I is made from material that has the Young’s modulus of E.  The
                              beam is constrained at the left end while the right end is subjected
                              to a compressive load of P as shown in the figure.


                                                          E,  I
                                                                                     P

                                                           L


                                         The  critical bucking load  P  according  to  the  Euler’s
                                                                  cr
                              formula is,
                                                                    2
                                                     P     2  EI kL
                                                      cr
                              where  k  is  the  factor  depending  on  the  end  boundary  conditions.
                              For  examples,  k  1 when  both  ends  are  pinned or hinged,  and
                               k  0.7071 when the left end is clamped.
                                         The lowest critical buckling load, sometimes called the
                              Euler’s  critical load,  causes  the  beam  to  bend  in  one  direction  as
                              shown in the preceding figure.  The lowest critical bucking load is,
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