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Centrifugal Pumps, Fans and Compressors  217































                          FIG. 7.11. Head correction factors for centrifugal impellers (adapted from Csanady
                                                         (1960)).


                          For radial vaned impellers this becomes   s D 1  0.63 /Z but is often written for
                          convenience and initial approximate calculations as   s D 1  2/Z.
                            Ferguson (1963) has usefully compiled values of slip factor found from several
                          theories for a number of blade angles and blade numbers and compared them with
                                                                             0
                          known experimental values. He found that for pumps, with ˇ between 60 deg and
                                                                             2
                          70 deg, the Busemann or Stodola slip factors gave fairly good agreement with
                          experimental results. For radial vaned impellers on the other hand, the Stanitz
                          expression, eqn. (7.18a) agreed very well with experimental observations. For inter-
                                          0
                          mediate values of ˇ the Busemann slip factor gave the most consistent agreement
                                          2
                          with experiment.
                            Wiesner (1967) reviewed all the available methods for calculating values of slip
                          factor and compared them with values obtained from tests. He concluded from
                          all the material presented that Busemann’s procedure was still the most generally
                          applicable predictor for determining the basic slip factor of centripetal impellers.
                          Wiesner obtained the following simple empirical expression for the slip velocity:
                                      p
                                   U 2 cosˇ 0 2
                              c  s D        .                                            (7.19a/
                                      Z 0.7
                          and the corresponding slip factor
                                       p     0  0.7
                                         cosˇ /Z
                                             2
                                w D 1              ,                                     (7.19b/
                                                 0
                                       .1    2 tan ˇ /
                                                 2
                          which, according to Wiesner, fitted the Busemann results “extremely well over the
                          whole range of practical blade angles and number of blades”.
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