Radial Turbine - Components of Radial Turbines

Components of Radial Turbines

  • Ninety degree inward-flow radial turbine stage

  • Velocity triangles for an inward-flow radial (IFR) turbine stage with cantilever blade

The radial and tangential components of the absolute velocity c2 are cr2 and cq2, respectively. The relative velocity of the flow and the peripheral speed of the rotor are w2 and u2 respectively. The air angle at the rotor blade entry is given by

tanβ2 = cr2/(cθ2-u2)= c2 sinα2 /( c2cosα2-u2)

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