METHODOLOGY FOR DETERMINING SPEED COEFFICIENTS IN THE DESIGN OF RADIAL-AXIAL TURBINE
Author(s) -
А.В. Пассар,
Д.В. Тимошенко,
E.V. Faleeva
Publication year - 2020
Publication title -
informatika i sistemy upravleniya
Language(s) - English
Resource type - Journals
eISSN - 1814-2419
pISSN - 1814-2400
DOI - 10.22250/isu.2020.66.25-36
Subject(s) - range (aeronautics) , turbine , axial compressor , mechanics , specific speed , flow (mathematics) , gas turbines , mathematics , control theory (sociology) , physics , computer science , mechanical engineering , engineering , aerospace engineering , centrifugal pump , control (management) , artificial intelligence , impeller , gas compressor
The article proposes a method for the interrelated determination of the speed coefficients and optimal geometry of a radial-axial centripetal turbine flow range. The method is based on a model of gas flow at an average diameter in a one-dimensional quasi-stationary approximation, supplemented with ratios to determine the optimal operating parameters of the turbine.
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