This paper describes analytical and experimental studies of noise t ransmission through aircraft panels. The theoretical solutions of the governing acoustic-structu ral equations are developed util izing modal decomposition and a Gal erki n-type procedure. Single, discretely stiffened, and double wall panels are considered. Theoretical predictions are compared with experimental measurements and differences a re identified.
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Vaičaitis et al. (1985) studied this question.
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