Propulsion and Power Plants
Аuthors
1*, 2, 1**1. Moscow Aviation Institute (National Research University), 4, Volokolamskoe shosse, Moscow, А-80, GSP-3, 125993, Russia
2. JSC «Gazprom», 16 Nametkina St., Moscow, GSP-7, 117997, Russian
*e-mail: agulnik@mai.ru
**e-mail: igor6fhsrby@yandex.ru
Abstract
Methods of calculation of losses of efficiency of a axial turbine stage with the driving wheel with a bandage and without a bandage are analyzed, settlement research is carried out them and known formulas for turbines with the driving wheel with a bandage are corrected.Keywords:
axial turbine stages, experiments, calculation, gaps, bandage, correction of formulas
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