Page 295 - Fluid Mechanics and Thermodynamics of Turbomachinery
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276 Fluid Mechanics, Thermodynamics of Turbomachinery
                          (3) the gas exit velocity and mass flow rate;
                          (4) the shroud radius at rotor exit;
                          (5) the relative flow angle at rotor inlet;
                          (6) the specific speed.

                          NB. The volume flow rate to be used in the definition of the specific speed is based on the
                          rotor exit conditions.
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