Page 312 - Fluid Mechanics and Thermodynamics of Turbomachinery
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Hydraulic Turbines  293

                                            U 2                               U 2

                                                   W 2                               W 2
                                           C 2                               C 2



                                                             U 2                             U 2




                                                                       W 3
                                      W 3
                                                                                 C 3
                                                C 3
                                                                           U 3
                                         U 3
                             Design point - full load operation     Part load operation
                          FIG. 9.13. Comparison of velocity triangles for a Francis turbine for full load and at part
                                                       load operation.


                                            100
                                                   Kaplan


                                                                  Pelton
                                           Efficiency, per cent  60
                                             80
                                                          Francis











                                             40
                                               20     40      60     80     100
                                                      Load ratio, per cent
                          FIG. 9.14. Variation of hydraulic efficiency for various types of turbine over a range of
                                          loading, at constant speed and constant head.


                            It is of interest to note the effect that swirling flow has on the performance
                          of the following diffuser. The results of an extensive experimental investigation
                          made by McDonald et al. (1971), showed that swirling inlet flow does not affect
                          the performance of conical diffusers which are well designed and give unsepa-
                          rated or only slightly separated flow when the flow through them is entirely axial.
                          Accordingly, part load operation of the turbine is unlikely to give adverse diffuser
                          performance.
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