Page 59 - Tribology in Machine Design
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46  Tribology in machine design


                                   A non-dimensional normal stress T can be defined as




                                 The shear stress acting at the same point is


                                 and the corresponding nondimensional stress is





                                 Figure 2.16 shows the distribution of shear stress along a plane parallel to
                                 the surface (y is constant). It is seen that that shear stress distribution is
                                 asymmetrical, with larger stresses being developed ahead of the contact line
                                 than behind it, and with the sense of the stress changing sign directly below
                                 the contact line. Thus any point below the surface will experience a cyclic
                                 stress history from negative to positive shear as the contact moves along the
                                 surface. The shear asymmetry becomes more pronounced the higher the
                                 coefficient of friction. However, Fig. 2.16 shows that the friction associated
                                 with the wear surface does not have a large effect on these stresses. The
                                 corresponding normal stress distribution is plotted in Fig. 2.17.
                                   This stress component is larger than the shear, and it peaks at a
                                 horizontal distance close to the origin where the shear stress is small. The
                                 normal stress also changes sign and becomes very slightly positive far
                                 behind the contact point. In front of the contact line the normal stress
                                 decreases monotonically and becomes of the same order as the shear stress
                                 in the region of peak shear stress. The maximum normal stress is found in a
                                 similar manner to the maximum shear stress; that is by differentiating eqn
                                 (2.104) with respect to 0 and setting the result equal to zero. In the case of
                                 shear stress, eqn (2.106) is involved. Thus, for shear stress


                                 where 0* corresponds to the position of largest shear. When eqn (2.108) is
                                evaluated numerically, 0* is found to be very insensitive to the friction
                                coefficient tan a, only varying between 30° and 45° as a varies from 0° to 90°.
                                   For normal stress, the critical angle is given by














     Figure 2.16                                     Figure 2.17
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