dc.contributor.author |
Tanasheva, N.K. |
|
dc.contributor.author |
Sakipova, S.E. |
|
dc.contributor.author |
Minkov, L.L. |
|
dc.contributor.author |
Bakhtybekova, A.R. |
|
dc.contributor.author |
Shuyushbaeva, N.N. |
|
dc.contributor.author |
Burkov, M.A. |
|
dc.date.accessioned |
2021-11-24T11:06:10Z |
|
dc.date.available |
2021-11-24T11:06:10Z |
|
dc.date.issued |
2021-06-11 |
|
dc.identifier.citation |
Tanasheva N.K. STUDY OF AERODYNAMIC CHARACTERISTICS OF A CYLINDRICAL BLADE WITH DEFLECTOR/N.K. Tanasheva [et al]//Eurasian Physical Technical Journal. -2021.-Vol.18. №3(37). Р.48-52. |
ru_RU |
dc.identifier.uri |
https://rep.ksu.kz//handle/data/11430 |
|
dc.description.abstract |
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. |
ru_RU |
dc.language.iso |
en |
ru_RU |
dc.publisher |
KU Publ. |
ru_RU |
dc.relation.ispartofseries |
Eurasian Physical Technical Journal;№3(37)/2021 |
|
dc.subject |
cylindrical blade with deflector |
ru_RU |
dc.subject |
wind turbines |
ru_RU |
dc.subject |
aerodynamic coefficients |
ru_RU |
dc.subject |
drag force |
ru_RU |
dc.subject |
lift force |
ru_RU |
dc.subject |
angle of attack |
ru_RU |
dc.subject |
Reynolds number |
ru_RU |
dc.title |
STUDY OF AERODYNAMIC CHARACTERISTICS OF A CYLINDRICAL BLADE WITH DEFLECTOR |
ru_RU |
dc.type |
Article |
ru_RU |