Numerical Modeling of the Influence of the Relative Positions of a Propeller and Pylon on Turboprop Aircraft Noise


Citar

Texto integral

Acesso aberto Acesso aberto
Acesso é fechado Acesso está concedido
Acesso é fechado Somente assinantes

Resumo

The influence of the position of the pylon on the characteristics of propeller noise has been studied as applied to environmental noise calculations for future aircraft. Components related to propeller noise itself and 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. A numerical 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. A noise calculation procedure by the integral Ffowcs Williams and Hawkings method has been implemented with the use of the Green’s function for the convective wave equation.

Sobre autores

V. Titarev

Federal Research Center “Computer Science and Control”, Russian Academy of Sciences; Central Aerohydrodynamic Institute (TsAGI), Moscow Research Complex

Email: aeroacoustics@tsagi.ru
Rússia, Moscow, 119333; Moscow, 107005

G. Faranosov

Central Aerohydrodynamic Institute (TsAGI), Moscow Research Complex; Perm National Research Polytechnic University

Autor responsável pela correspondência
Email: aeroacoustics@tsagi.ru
Rússia, Moscow, 107005; Perm, 614990

S. Chernyshev

Central Aerohydrodynamic Institute (TsAGI), Moscow Research Complex

Email: aeroacoustics@tsagi.ru
Rússia, Moscow, 107005

A. Batrakov

Kazan National Research Technical University n.a. A.N. Tupolev,

Email: aeroacoustics@tsagi.ru
Rússia, Kazan, 420111

Arquivos suplementares

Arquivos suplementares
Ação
1. JATS XML

Declaração de direitos autorais © Pleiades Publishing, Ltd., 2018