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                 Brown˙C07
                                          CHAPTER 7
                          FATIGUE AND DYNAMIC
                                            DESIGN








                    7.1 INTRODUCTION


                    A machine element may have been designed to be safe under static conditions, only to
                    fail under repeated dynamic loading, called a fatigue failure. This repeated loading could
                    be a complete reversal of the load, be a fluctuating load, or be due to a combination of
                    loadings. The loading may produce either normal stresses or shear stresses, or the loading
                    can produce a combination of both normal and shear stresses so that either by Mohr’s circle
                    or by the appropriate equations the principal stresses are found. All of these types of loading
                    conditions will be discussed in this section.
                      If the design of a machine element becomes unsafe under dynamic conditions, it usually
                    fails suddenly and below the static strengths of the material, either the yield strength (S y ) for
                    ductile materials or the ultimate tensile strength (S ut ) for brittle materials. It is interesting,
                    although not unexpected, that a brittle material would fail suddenly under either static or
                    dynamic conditions. Ductile materials fail as if they were brittle from excessive repeated
                    loading at a stress level below the yield strength (S y ). The most accepted method of deter-
                    mining this critical stress level will be presented shortly.
                      The mode of failure under dynamic conditions appears to be a result of a very small
                    crack, too small to see with the naked eye, developing at a point where the geometry of
                    the machine element changes, usually on the surface. A crack can even develop at a part
                    identification stamp, or at a surface scratch accidentally put on the part during assembly or
                    repair. Under repeated loading, this crack grows due to stress concentrations until the area
                    over which the load must be carried is reduced rapidly, causing the stress to increase just as
                    rapidly. Sudden failure, without any warning, occurs when the stress level exceeds a critical
                    value for a specified number of cycles. Therefore, a fatigue failure can be differentiated
                    visually from a static failure by the appearance of two regions on the failed part. The first
                    region is due to the propagation of the crack, and the second region is due to the sudden
                    fracture, not unlike what would be seen in the static failure of a brittle material, such as
                    cast iron. This is in contrast to what would be seen in the static failure of a ductile material,
                    where considerable yielding would be visible.
                      Some materials, like steel, have a critical stress value, which if never exceeded, ensure
                    the machine element has an infinite life. For other materials, like aluminum, there is no such
                    value at any number of cycles so the machine element will fail at some point no matter how
                    low the stress level is kept.
                      Thestudyoffatigueisrelativelyrecentandcommencedonlypost-WorldWarII.However,
                    some machines designed even in the middle-to-late nineteenth century have been operating



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