Numerical simulation of aerodynamic and acoustic characteristics of a ducted rotor
- Authors: Abalakin I.V.1, Bahvalov P.A.1, Bobkov V.G.1, Kozubskaya T.K.1, Anikin V.A.2
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Affiliations:
- Keldysh Institute of Applied Mathematics
- Kamov JSC
- Issue: Vol 8, No 3 (2016)
- Pages: 309-324
- Section: Article
- URL: https://journals.rcsi.science/2070-0482/article/view/200924
- DOI: https://doi.org/10.1134/S2070048216030030
- ID: 200924
Cite item
Abstract
This work is devoted to the numerical simulation of the problem about a rotor rotation in a duct in a noninertial reference frame based on the Euler equations. The configuration is a model of a tail rotor of a helicopter. The calculations were carried out using highly accurate EBR schemes on unstructured tetrahedral meshes with the variables determined at the nodes. The numerical results on the aerodynamic forces, as well as the intensity and direction of the acoustic radiation in the far field, are presented and analyzed.
About the authors
I. V. Abalakin
Keldysh Institute of Applied Mathematics
Author for correspondence.
Email: ilya.abalakin@gmail.com
Russian Federation, Moscow
P. A. Bahvalov
Keldysh Institute of Applied Mathematics
Email: ilya.abalakin@gmail.com
Russian Federation, Moscow
V. G. Bobkov
Keldysh Institute of Applied Mathematics
Email: ilya.abalakin@gmail.com
Russian Federation, Moscow
T. K. Kozubskaya
Keldysh Institute of Applied Mathematics
Email: ilya.abalakin@gmail.com
Russian Federation, Moscow
V. A. Anikin
Kamov JSC
Email: ilya.abalakin@gmail.com
Russian Federation, Lubertsi, Moscow oblast