13. Determine the total-to-total efficiency of a low speed axial turbine stage that at the design condition has a stator exit flow angle of 70°, zero swirl at inlet and exit, constant axial velocity, and 50% reaction. Assume that the kinetic energy loss coefficient of both the stator blades and the rotor blades is 0.09.

Elements Of Electromagnetics
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ISBN:9780190698614
Author:Sadiku, Matthew N. O.
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13. Determine the total-to-total efficiency of a low speed axial turbine stage that at the design
condition has a stator exit flow angle of 70°, zero swirl at inlet and exit, constant axial
velocity, and 50% reaction. Assume that the kinetic energy loss coefficient of both the stator
blades and the rotor blades is 0.09.
Transcribed Image Text:13. Determine the total-to-total efficiency of a low speed axial turbine stage that at the design condition has a stator exit flow angle of 70°, zero swirl at inlet and exit, constant axial velocity, and 50% reaction. Assume that the kinetic energy loss coefficient of both the stator blades and the rotor blades is 0.09.
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