04/ An impulsive stage of a steam turbine is supplied with dry and saturated steam (15 Dar). The stage has a single row of moving blades running at (3600 rpm). The mean dameter of the blade disc is (0.9 m). the nozzle angle is ( 15) and the axial component of he absolute velocity leaving the nozzle is (94 m/sec). the height of the nozzles at their exit S(100 mm). The nozzle efficiency is (0.9) and the blade velocity Coefficient is (0.97). The t angle of the moving blades is (2°) greater than at the inlet. Determine, 1- the blade 4. theo the outlet angles. 2- the isentropic heat drop in the stage. 3- the stage efficiency. the power developed by the stage.

Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
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Q4/ An impulsive stage of a steam turbine is supplied with dry and saturated steam (15
da The stage has a single row of moving blades running at (3600 rpm). The mean
diameter of the blade disc is (0.9 m). the nozzle angle is ( 15) and the axial component of
absolute velocity leaving the nozzle is (94 m/sec). the height of the nozzles at their exit
o mm). The nozzle efficiency is (0.9) and the blade velocity Coefficient is (0.97). The
inles angie of the moving blades is (2°) greater than at the inlet. Determine, 1- the blade
4. thend the outlet angles. 2- the isentropic heat drop in the stage. 3- the stage efficiency.
the power developed by the stage.
th
Transcribed Image Text:Q4/ An impulsive stage of a steam turbine is supplied with dry and saturated steam (15 da The stage has a single row of moving blades running at (3600 rpm). The mean diameter of the blade disc is (0.9 m). the nozzle angle is ( 15) and the axial component of absolute velocity leaving the nozzle is (94 m/sec). the height of the nozzles at their exit o mm). The nozzle efficiency is (0.9) and the blade velocity Coefficient is (0.97). The inles angie of the moving blades is (2°) greater than at the inlet. Determine, 1- the blade 4. thend the outlet angles. 2- the isentropic heat drop in the stage. 3- the stage efficiency. the power developed by the stage. th
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