Отправить статью по E-mail Numerical investigation of the aerodynamic and acoustical properties of a shrouded rotor
- Авторы: Abalakin I.V.1, Anikin V.A.2, Bakhvalov P.A.1, Bobkov V.G.1, Kozubskaya T.K.1
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Учреждения:
- Keldysh Institute of Applied Mathematics
- Design office ”Kamov”
- Выпуск: Том 51, № 3 (2016)
- Страницы: 419-433
- Раздел: Article
- URL: https://journals.rcsi.science/0015-4628/article/view/155243
- DOI: https://doi.org/10.1134/S0015462816030145
- ID: 155243
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Аннотация
The problem of shrouded rotor rotation is numerically solved basing on the Navier–Stokes equations in a noninertial coordinate system. The configuration considered is a model helicopter tail rotor.The calculations are performed using edge-based reconstruction (EBR) schemes on unstructured tetrahedral grids with the variables determined at gridpoints. The numerical results on the aerodynamic forces and the acoustic radiation intensity and direction in the far field are presented and analyzed.
Об авторах
I. Abalakin
Keldysh Institute of Applied Mathematics
Автор, ответственный за переписку.
Email: veld13@gmail.com
Россия, Miusskaya pl. 4, Moscow, 125047
V. Anikin
Design office ”Kamov”
Email: veld13@gmail.com
Россия, ul. 8 Marta 8-A, Lyubertsy, Moscow oblast, 111625
P. Bakhvalov
Keldysh Institute of Applied Mathematics
Email: veld13@gmail.com
Россия, Miusskaya pl. 4, Moscow, 125047
V. Bobkov
Keldysh Institute of Applied Mathematics
Email: veld13@gmail.com
Россия, Miusskaya pl. 4, Moscow, 125047
T. Kozubskaya
Keldysh Institute of Applied Mathematics
Email: veld13@gmail.com
Россия, Miusskaya pl. 4, Moscow, 125047
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