Analysis of Aerodynamic Characteristics of Two Parallel Rotating Cylinders

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dc.contributor.authorTanasheva, N. K.
dc.contributor.authorNusupbekov, B. R.
dc.contributor.authorDyusembaeva, A. N.
dc.contributor.authorShuyushbayeva, N. N.
dc.date.accessioned2022-04-12T05:58:45Z
dc.date.available2022-04-12T05:58:45Z
dc.date.issued2019
dc.description.abstractWe report on the results of experimental investigations on determining drag and lift coefficients for a system of two parallel rotating cylinders. The results show that with increasing the distance between rotating cylinders, drag and lift coefficients decrease. It has been established experimentally that the distance beginning with which cylinders almost stop acting on each other is 0.4 of the diameter of these cylinders.ru_RU
dc.identifier.citationTanasheva N. K. Analysis of Aerodynamic Characteristics of Two Parallel Rotating Cylinders/N. K. Tanasheva [et all]//Technical Physics.-2019.-Vol 64(7).-pp.947-949ru_RU
dc.identifier.issn1063-7842
dc.identifier.urihttps://rep.buketov.edu.kz//handle/data/12177
dc.language.isoenru_RU
dc.publisherTechnical Physicsru_RU
dc.relation.ispartofseriesTechnical Physics;Vol 64(7)
dc.titleAnalysis of Aerodynamic Characteristics of Two Parallel Rotating Cylindersru_RU
dc.typeArticleru_RU

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