Effects of Cavity Resonances on Sound Transmission into a Thin Cylindrical Shell
In the context of the transmission of airborne noise into an aircraft fuselage, a mathematical model is presented for the effects of internal cavity resonances on sound transmission into a thin cylindrical shell. The "noise reduction" of the cylinder is defined and computed, with and without including the effects of internal cavity resonances. As would be expected, the noise reduction in the absence of cavity resonances follows the same qualitative pattern as does transmission loss. Numerical results show that cavity resonances lead to wide fluctuations and a general decrease of noise reduction, especially at cavity resonances. Modest internal absorption is shown to greatly reduce the effect of cavity resonances. The effects of external airflow, internal cabin pressurization, and different acoustical properties inside and outside the cylinder are also included and briefly examined.
L. R. Koval, "Effects of Cavity Resonances on Sound Transmission into a Thin Cylindrical Shell," Journal of Sound and Vibration, Elsevier, Jan 1978.
The definitive version is available at https://doi.org/10.1016/0022-460X(78)90475-3
Mechanical and Aerospace Engineering
International Standard Serial Number (ISSN)
Article - Journal
© 1978 Elsevier, All rights reserved.
01 Jan 1978