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Исследование зависимости аэродинамических характеристик вращающихся цилиндров от угла скоса воздушного потока
Author(s) -
Н.К. Танашева,
Н.Н. Шуюшбаева,
Э.К. Мусенова
Publication year - 2018
Publication title -
pisʹma v žurnal tehničeskoj fiziki
Language(s) - English
Resource type - Journals
eISSN - 1726-7471
pISSN - 0320-0116
DOI - 10.21883/pjtf.2018.17.46572.17240
Subject(s) - lift coefficient , rake angle , lift (data mining) , rake , aerodynamics , mechanics , cylinder , physics , engineering , mechanical engineering , turbulence , computer science , reynolds number , data mining , machining
The results of experimental studies on estimating the lift force and lift coefficient of a rotating cylinder of constant cross section are presented. The data on the effect of the flow rake angle on the aerodynamic characteristics of rotating cylinders within a range of angles from 0° to 90° are analyzed. It has been established that a decrease in the lift coefficient is observed at flow rake angles above 30°, so the wind engine element shows a positive result within a range of rake angles from–30 ° ≤ α ≤ 30°. The data of these experimental studies can be used for the development of wind engines with blades designed as rotating cylinders with a smooth surface.

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