Abstract
The results of experimental laboratory studies of an acoustic field inside the stiffened shell are presented; the shell simulates an aircraft fuselage compartment under its excitation by a diffusion sound field. The soundproofing capacity of the model compartment under diffusion excitation is experimentally evaluated.
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Original Russian Text © A.Ya. Zverev, V.V. Chernykh, 2009, published in Izvestiya VUZ. Aviatsionnaya Tekhnika, 2009, No. 2, pp. 66–68.
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Zverev, A.Y., Chernykh, V.V. Determination of a soundproofing capacity of the model aircraft fuselage compartment. Russ. Aeronaut. 52, 235–239 (2009). https://doi.org/10.3103/S1068799809020160
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DOI: https://doi.org/10.3103/S1068799809020160