
Structural Analysis
6th Edition
ISBN: 9781337630931
Author: KASSIMALI, Aslam.
Publisher: Cengage,
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Transcribed Image Text:stage
Q2. At a stage of reaction turbine, the mean rotor diameter is 1.4 m.
The speed ratio is 0.7. Determine the blade inlet angle if the blade
outlet angle is 20°. The rotor speed is 3000 rpm. Also find the stage
efficiency. Find the stage efficiency and rotor speed if the rotor is
designed to run at the best theoretical speed ratio. Assume Parsons
turbine and expansion losses as 10 % of heat drop. (50°, 90%, 90%)
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