Analysis of Aerodynamic Characteristics of Two Parallel Rotating Cylinders
- Authors: Tanasheva N.K.1, Nusupbekov B.R.2, Dyusembaeva A.N.2, Shuyushbayeva N.N.3
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Affiliations:
- Institute of Applied Mathematics
- Karaganda State University
- Ualikhanov Kokshetau State University
- Issue: Vol 64, No 7 (2019)
- Pages: 947-949
- Section: Gases and Liquids
- URL: https://journals.rcsi.science/1063-7842/article/view/203687
- DOI: https://doi.org/10.1134/S1063784219070247
- ID: 203687
Cite item
Abstract
We 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.
About the authors
N. K. Tanasheva
Institute of Applied Mathematics
Author for correspondence.
Email: nazgulya_tans@mail.ru
Kazakhstan, Karaganda, 100028
B. R. Nusupbekov
Karaganda State University
Email: nazgulya_tans@mail.ru
Kazakhstan, Karaganda, 100028
A. N. Dyusembaeva
Karaganda State University
Email: nazgulya_tans@mail.ru
Kazakhstan, Karaganda, 100028
N. N. Shuyushbayeva
Ualikhanov Kokshetau State University
Email: nazgulya_tans@mail.ru
Kazakhstan, Kokshetau, 020000