Abstract
An effect of the Coriolis forces on the process of gas expansion in the turbine stage is considered. Expressions for efficiency with regard for the radial flow passage are derived. The calculation results and statistical data on the geometric parameters of diagonal stages are presented.
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Original Russian Text © E.N. Bogomolov, P.V. Kashcheeva, 2009, published in Izvestiya VUZ. Aviatsionnaya Tekhnika, 2009, No. 2, pp. 75–77.
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Bogomolov, E.N., Kashcheeva, P.V. Thermodynamic features of aircraft diagonal gas turbines. Russ. Aeronaut. 52, 250–254 (2009). https://doi.org/10.3103/S1068799809020196
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DOI: https://doi.org/10.3103/S1068799809020196