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What is Blade Discharge Angle Impact on Turbo Machines about?
The document analyzes the theoretical effect of blade discharge angle on the degree of reaction for a radial outward flow turbo machine. It derives an expression for degree of reaction in terms of blade discharge angle and establishes the following results: 1) For blade discharge angles less than 26.5°, the machine acts like a turbine with a degree of reaction greater than 1. 2) At 26.5°, there is no change in static pressure head and the degree of reaction is 1. 3) Between 26.5° and 153.5°, the machine is
- Author
- Muthuraju NP
- Language
- EN