This paper describes analytical and experimental studies of noise transmission through aircraft panels. The theoretical solutions of the governing acoustic-structural equations are developed utilizing modal decomposition and a Galerkin-type procedure. Single, discretely stiffened, and double wall panels are considered. Theoretical predictions are compared with experimental measurements and differences are identified.
Noise transmission through aircraft panels
01.01.1984
Aufsatz (Konferenz)
Keine Angabe
Englisch
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