Analysis of the Three-Dimensional Accelerating Flow in A Mixed Turbine Rotor

An investigation on new rotor blade designs conceived to produce higher exit relative kinetic energy of a mixed flow turbine is undertaken. Accelerating the through in frame reference improves transfer shaft, which only produced rotating rotor. A three-dimensional converging channel might respond analysis requirements subsonic regimes. Effectively, machine experiences 3.71 % and 3.67 increase work output efficiency, respectively, representing this study’s primary intent. This has been accomplished by varying shroud profile lesser eye tip diameter, then hub larger root diameter. At last, both profiles are varied. It appears possible enhance performance terms optimum done efficiency devising suitable geometry designs. ANSYS CFX 15 code all simulation works.