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Study of aerodynamic characteristics of a cylindrical blade with deflector N. K. Tanasheva, S. E. Sakipova, L. L. Minkov [et al.]

Contributor(s): Tanasheva, N. K | Sakipova, S. E | Minkov, Leonid L | Bakhtybekova, A. R | Shuyushbaeva, N. N | Burkov, M. AMaterial type: ArticleArticleContent type: Текст Media type: электронный Subject(s): ветродвигатели | аэродинамические коэффициенты | сила сопротивления | подъемная сила | угол атаки | Рейнольдса число | цилиндрические лопасти | дефлекторыGenre/Form: статьи в журналах Online resources: Click here to access online In: Eurasian physical technical journal Vol. 18, № 3. P. 48-52Abstract: The article discusses some aspects of the renewable energy sources use, in particular, the problem of small wind power. A brief analysis of the development rates of wind energy in the world and in Kazakhstan is presented. The study is devoted to finding ways to optimize the blade of a wind power plant based on the Magnus effect, designed to generate electrical energy at low wind speeds. A cylindrical blade with a turbo-deflector has been developed to ensure independent starting of the blade rotation without the use of additional trigger mechanism. Laboratory tests of a cylindrical blade with a turbo deflector were carried out on a T-I-M wind tunnel at various flow regimes. The obtained dependences of aerodynamic forces on the air flow velocity at different angles of attack are shown.
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The article discusses some aspects of the renewable energy sources use, in particular, the problem of small wind power. A brief analysis of the development rates of wind energy in the world and in Kazakhstan is presented. The study is devoted to finding ways to optimize the blade of a wind power plant based on the Magnus effect, designed to generate electrical energy at low wind speeds. A cylindrical blade with a turbo-deflector has been developed to ensure independent starting of the blade rotation without the use of additional trigger mechanism. Laboratory tests of a cylindrical blade with a turbo deflector were carried out on a T-I-M wind tunnel at various flow regimes. The obtained dependences of aerodynamic forces on the air flow velocity at different angles of attack are shown.

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