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Numerical Modeling of the Influence of the Relative Positions of a Propeller and Pylon on Turboprop Aircraft Noiseстатья Исследовательская статья
- Авторы: Titarev V.A., Faranosov G.A., Chernyshev S.A., Batrakov A.S.
- Журнал: Acoustical Physics
- Том: 64
- Номер: 6
- Год издания: 2018
- Издательство: Maik Nauka/Interperiodica Publishing
- Местоположение издательства: Russian Federation
- Первая страница: 760
- Последняя страница: 773
- DOI: 10.1134/s1063771018060118
- Аннотация: The influence of the position of the pylon on the characteristics of propeller noise has been studiedas applied to environmental noise calculations for future aircraft. Components related to propeller noise itselfand to a signal reflected from a pylon have been separated in the overall noise produced by the propeller–pylon system at the blade passing frequency, and the interference of these signals has been investigated. Anumerical method has been developed based on matching of the following two computational blocks: a rotating domain in the immediate vicinity of the propeller and the outer static domain comprising the pylon. Anoise calculation procedure by the integral Ffowcs Williams and Hawkings method has been implementedwith the use of the Green’s function for the convective wave equation
- Добавил в систему: Титарев Владимир Александрович