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Section 1.2  Types of Material Failure                                       27





























            Figure 1.9 Fatigue failure of a garage door spring that occurred after 15 years of service.
            (Photo by R. A. Simonds; sample contributed by R. S. Alvarez, Blacksburg, VA.)


               Cracks may be initially present in a component from manufacture, or they may start early in
            the service life. Emphasis must then be placed on the possible growth of these cracks by fatigue, as
            this can lead to a brittle or ductile fracture once the cracks are sufficiently large. Such situations are
            identified by the term fatigue crack growth and may also be analyzed by the previously mentioned
            technology of fracture mechanics. For example, analysis of fatigue crack growth is used to schedule
            inspection and repair of large aircraft, in which cracks are commonly present.
               Such analysis is useful in preventing problems similar to the fuselage (main body) failure in
            1988 of a passenger jet, as shown in Fig. 1.11. The problem in this case started with fatigue cracks
            at rivet holes in the aluminum structure. These cracks gradually grew during use of the airplane,
            joining together and forming a large crack that caused a major fracture, resulting in separation of a
            large section of the structure. The failure could have been avoided by more frequent inspection and
            repair of cracks before they grew to a dangerous extent.


            1.2.5 Combined Effects
            Two or more of the previously described types of failure may act together to cause effects greater
            than would be expected by their separate action; that is, there is a synergistic effect. Creep and
            fatigue may produce such an enhanced effect where there is cyclic loading at high temperature. This
            may occur in steam turbines in electric power plants and in gas-turbine aircraft engines.
               Wear due to small motions between fitted parts may combine with cyclic loading to produce
            surface damage followed by cracking, which is called fretting fatigue. This may cause failure at
            surprisingly low stress levels for certain combinations of materials. For example, fretting fatigue
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