Abstract
The use of high-bypass-ratio engines in civil aviation has resulted in the occurrence of an additional noise source associated with noise of interaction between a jet and an airplane wing. A theoretical model is proposed for predicting the characteristics of interaction noise based on the near-field parameters for an isolated jet. The required near-field characteristics were obtained experimentally in the AC-2 anechoic chamber of the Central Aerohydrodynamic Institute (TsAGI) using a system of azimuthal microphone arrays. Noise in the far-field zone was also measured for both an isolated jet and a jet with a closely located plate simulating a wing. The results of comparing the directivities and spectra of interaction noise obtained using the proposed model and measured experimentally are in good agreement.
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Original Russian Text © O.P. Bychkov, G.A. Faranosov, 2018, published in Akusticheskii Zhurnal, 2018, Vol. 64, No. 4, pp. 437–453.
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Bychkov, O.P., Faranosov, G.A. An Experimental Study and Theoretical Simulation of Jet-Wing Interaction Noise. Acoust. Phys. 64, 437–452 (2018). https://doi.org/10.1134/S1063771018030041
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DOI: https://doi.org/10.1134/S1063771018030041