Analysis of Aerodynamic Characteristics of Two Parallel Rotating Cylinders
- Авторлар: Tanasheva N.K.1, Nusupbekov B.R.2, Dyusembaeva A.N.2, Shuyushbayeva N.N.3
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Мекемелер:
- Institute of Applied Mathematics
- Karaganda State University
- Ualikhanov Kokshetau State University
- Шығарылым: Том 64, № 7 (2019)
- Беттер: 947-949
- Бөлім: Gases and Liquids
- URL: https://ogarev-online.ru/1063-7842/article/view/203687
- DOI: https://doi.org/10.1134/S1063784219070247
- ID: 203687
Дәйексөз келтіру
Аннотация
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.
Авторлар туралы
N. Tanasheva
Institute of Applied Mathematics
Хат алмасуға жауапты Автор.
Email: nazgulya_tans@mail.ru
Қазақстан, Karaganda, 100028
B. Nusupbekov
Karaganda State University
Email: nazgulya_tans@mail.ru
Қазақстан, Karaganda, 100028
A. Dyusembaeva
Karaganda State University
Email: nazgulya_tans@mail.ru
Қазақстан, Karaganda, 100028
N. Shuyushbayeva
Ualikhanov Kokshetau State University
Email: nazgulya_tans@mail.ru
Қазақстан, Kokshetau, 020000
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