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Abstract
The efficiency of the stators of centripetal radial turbine expansion engines, characterized by the small dimensions of the flow section have been studied. The study is extended to obtain data on the variation of the losses in relation to the relative geometrical parameters. Investigations have been carried out into the level of the total losses in the wing-shaped small vane stator and its geometrical parameters are optimized. The processing method accepted for the calculations is based on the equations of the unidimensional theory of the gas flows which gives sufficiently reliable results.
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