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Friction, lubrication and wear in higher kinematic pairs  239

                                 Eliminating Q gives





                                 This is Reynolds equation for a steady two-dimensional flow in a thin
                                 lubricating film. Given the variation in thickness of the film h(x), it can be
                                 integrated to give pressure p(x) developed by hydrodynamic action. For a
                                 more complete discussion of the Reynolds equation the reader is referred to
                                 the books on lubrication listed at the end of Chapter 5.
                                   Now, eqn (6.18) will be used to find the pressure developed in a film
                                 between two rotating cylinders.



                                 The geometry of two rotating rigid cylinders in contact is schematically
                                 shown in Fig. 6.4. An ample supply of lubricant is provided on the entry
                                 side. Within the region of interest the thickness of the film can be expressed
                                 by



                                 where l/R = 1/Rt + l/R 2 and h is the thickness at x=0. Substituting eqn
                                 (6.19) into (6.18) gives






     Figure 6.4
                                                                 l
                                 By making the substitution c=tan [x/(2Rh)*] eqn (6.20) can be in-
                                 tegrated to give an expression for the pressure distribution







                                              i
                                 where ^=tan [xi/(2Rh 0)*'] and x t is the value of x where h = h v and
                                 dp/dx=0. The values of ^ and A are found from the end conditions.
                                   At the start it is assumed that the pressure is zero at distant points at entry
                                 and exit, i.e. p=0atx=±oo. The resulting pressure distribution is shown
                                 by the dotted line in Fig. 6.4. It is positive in the converging zone at entry
                                 and equally negative in the diverging zone at exit. The total force W
                                 supported by the film is clearly zero in this case. However this solution is
                                 unrealistic since a region of large negative pressure cannot exist in normal
                                 ambient conditions. In practice the flow at the exit breaks down into
                                 streamers separated by fingers of air penetrating from the rear. The pressure
                                 is approximately ambient in this region. The precise point of film
                                 breakdown is determined by consideration of the three-dimensional flow in
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