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               FIGURE 2.12  Effect of the diameter’s ratio on the contraction coeffi cient of
               a sharp-edged orifi ce, calculated.



                   Sharp-edged orifices are preferred because of their predictable
               characteristics. The pressure and power losses in these orifices are
               dominated by the fluid inertia. The fluid viscosity has no significant
               effect on their operation (C ≈ 1). Therefore, the flow rate through
                                       v
               sharp-edged orifices is viscosity-independent. On the other hand, for
               economy reasons, short tube orifices are widely used, especially as
               fixed restrictors in the flow passages. The fluid flow through a short
               tube orifice is subjected to the friction losses as well as the minor  losses
               at inlet and outlet. Therefore, these orifices are viscosity- dependent.
               The discharge coefficient of a short tube orifice depends on the Reyn-
               olds number and the orifice geometry. The following expressions are
               used to calculate the discharge coefficient for the turbulent and lami-
               nar regions [Merritt (1967)]:


                           ⎡               1 ⎤  −  1 2
                           ⎢         ⎛  L ⎞ ⎥        Red
                                           2
                              +
                                  .
                             .
                       C = 1 5 13 74 ⎜    ⎟ ⎥   For      > 50       (2.40)
                        d  ⎢         ⎝ Re d⎠          L
                           ⎢ ⎣              ⎥ ⎦
                                       1
                           ⎡     64 L⎤  −  2
                             .
                       C = 228  +    ⎥           For  Red           (2.41)
                           ⎢
                        d                                < 50
                           ⎣     Re d ⎦               L
                   The variation of the discharge coefficient with (Re d/L), calculated
               using these expressions, is plotted in Fig. 2.13.
               Local Losses  The local losses, also called minor losses, result from a
               rapid variation in the magnitude or direction of the velocity vector.
               The throttling elements, elbows, and T connections are typical local
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