Radial-inflow Gas Turbine

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Radial-inflow Gas Turbine

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► Rotor | Main dimensions

The Main Dimensions menu item is used to define main dimensions of the rotor. Main Dimensions are forming the most important basis for all following design steps.

The real flow in a turbine rotor is turbulent and  three-dimensional. Secondary flows, separation and reattachment in boundary layers, transient recirculation areas and other features may occur. Nevertheless it is useful - and it is common practice in the turbine design theory - to simplify the realistic flow applying representative streamlines for the first design approach.

Employing 1D-streamline theory the following cross sections are significant in particular: area just before leading edge (index 0), at the beginning (index 1) and at the end of the blade (index 2) and finally behind the trailing edge (index 3).

The cross section (S) is situated at the suction side in the connection flange of the component following the turbine.



¢ Setup

¢ Parameters

¢ Dimensions

The design of the main dimensions has to be made in a strict order. This will be secured by the following:One step within the design has to be finished completely before the next can be accomplished. That is to say, the changeability of a tab sheet will be disabled by CFturbo until all necessary parameters have been specified.