Calculation Reactivity Degree for Axial Low-Account Turbines with Small Emergence Angles of Nozzle Devices

Abstract

This paper presents the possibility of constructing a mathematical regression model for the reactivity degree of turbine stages (with the nozzle exit angles 5 ° ... 9 ° and a diameter of 0.17 m) depending on the constructed and model factors that have the greatest impact on the function value.