In an axial turbine stage, the absolute velocity entering and leaving the stage are in the axial
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Question:
In an axial turbine stage, the absolute velocity entering and leaving the stage are in the axial direction. The degree of reaction is 0.55 and nozzle angle is 22º.
Calculate the flow coefficient, loading coefficient and relative flow angle?
Related Book For
Thermodynamics An Interactive Approach
ISBN: 978-0130351173
1st edition
Authors: Subrata Bhattacharjee
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