Open AccessOptimal values of the angle of exit of the flow from the nozzle apparatus radial-axial turbine, depending on the mode of its operation
Author(s) -
А.В. Пассар,
Д.В. Тимошенко,
Ю.Я. Фершалов
Publication year - 2022
Publication title -
морские интеллектуальные технологии
Language(s) - English
Resource type - Journals
eISSN - 2588-0233
pISSN - 2073-7173
DOI - 10.37220/mit.2022.57.3.017
Subject(s) - nozzle , mechanics , turbine , flow (mathematics) , radius , axial compressor , internal flow , physics , thermodynamics , computer science , gas compressor , computer security
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