Abstract—
Based on the previously developed analytical model of jet–wing interaction noise, we analyze the results of measuring the azimuthal modes of pressure pulsations in the near field of a free turbulent jet and the azimuthal modes of noise arising from interaction between a jet and a nearby flat plate simulating an airplane wing. The interrelation of the characteristics of the near hydrodynamic and far acoustic fields of pressure pulsations for the jet–plate system is demonstrated. A simplified method is proposed for collecting the necessary information for the model.
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Funding
The part of the study related to processing and analysis of data on the azimuthal structure of the near and far fields was carried out with the financial support of the Ministry of Science and Higher Education of the Russian Federation (unique identifier RFMEFI62818X0011). The part work related to development of a simplified analytical model for its use in the presence of coflow was supported by the Russian Foundation for Basic Research (project no. 18-31-00430).
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Bychkov, O.P., Faranosov, G.A. Analysis of Mode Coupling of Jet Near Field Puslations and Jet–Wing Interaction Noise. Acoust. Phys. 66, 33–43 (2020). https://doi.org/10.1134/S1063771020010029
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DOI: https://doi.org/10.1134/S1063771020010029