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                                                                               Fatigue Failure Resulting from Variable Loading  327
                                                  Collins said it well: “In spite of all the problems cited, the Palmgren linear damage
                                               rule is frequently used because of its simplicity and the experimental fact that other
                                               more complex damage theories do not always yield a significant improvement in fail-
                                               ure prediction reliability.” 26

                                     6–16      Surface Fatigue Strength
                                               The surface fatigue mechanism is not definitively understood. The contact-affected
                                               zone, in the absence of surface shearing tractions, entertains compressive principal
                                               stresses. Rotary fatigue has its cracks grown at or near the surface in the presence of
                                               tensile stresses that are associated with crack propagation, to catastrophic failure. There
                                               are shear stresses in the zone, which are largest just below the surface. Cracks seem to
                                               grow from this stratum until small pieces of material are expelled, leaving pits on the sur-
                                               face. Because engineers had to design durable machinery before the surface fatigue phe-
                                               nomenon was understood in detail, they had taken the posture of conducting tests,
                                               observing pits on the surface, and declaring failure at an arbitrary projected area of hole,
                                               and they related this to the Hertzian contact pressure. This compressive stress did
                                               not produce the failure directly, but whatever the failure mechanism, whatever the
                                               stress type that was instrumental in the failure, the contact stress was an index to its
                                               magnitude.
                                                                                                           8
                                                  Buckingham 27  conducted a number of tests relating the fatigue at  10 cycles to
                                               endurance strength (Hertzian contact pressure). While there is evidence of an endurance
                                                             7
                                               limit at about 3(10 ) cycles for cast materials, hardened steel rollers showed no endurance
                                                            8
                                               limit up to 4(10 ) cycles. Subsequent testing on hard steel shows no endurance limit.
                                               Hardened steel exhibits such high fatigue strengths that its use in resisting surface fatigue
                                               is widespread.
                                                  Our studies thus far have dealt with the failure of a machine element by yielding,
                                               by fracture, and by fatigue. The endurance limit obtained by the rotating-beam test is
                                               frequently called the flexural endurance limit, because it is a test of a rotating beam. In
                                               this section we shall study a property of mating materials called the surface endurance
                                               shear. The design engineer must frequently solve problems in which two machine ele-
                                               ments mate with one another by rolling, sliding, or a combination of rolling and sliding
                                               contact. Obvious examples of such combinations are the mating teeth of a pair of gears,
                                               a cam and follower, a wheel and rail, and a chain and sprocket. A knowledge of the sur-
                                               face strength of materials is necessary if the designer is to create machines having a
                                               long and satisfactory life.
                                                  When two surfaces roll or roll and slide against one another with sufficient force,
                                               a pitting failure will occur after a certain number of cycles of operation. Authorities are
                                               not in complete agreement on the exact mechanism of the pitting; although the subject
                                               is quite complicated, they do agree that the Hertz stresses, the number of cycles, the sur-
                                               face finish, the hardness, the degree of lubrication, and the temperature all influence the
                                               strength. In Sec. 3–19 it was learned that, when two surfaces are pressed together, a
                                               maximum shear stress is developed slightly below the contacting surface. It is postulated
                                               by some authorities that a surface fatigue failure is initiated by this maximum shear
                                               stress and then is propagated rapidly to the surface. The lubricant then enters the crack
                                               that is formed and, under pressure, eventually wedges the chip loose.


                                               26 J. A. Collins, Failure of Materials in Mechanical Design, John Wiley & Sons, New York, 1981, p. 243.
                                               27 Earle Buckingham, Analytical Mechanics of Gears, McGraw-Hill, New York, 1949.
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