2006
DOI: 10.1007/s00419-006-0096-7
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Sound transmission through laminated composite cylindrical shells using analytical model

Abstract: Composite structures are often used in aircraft because of advantages offered by a high strength to weight ratio. Sound transmission through an infinite laminated composite cylindrical shell is studied in the context of the transmission of airborne sound into aircraft interior. The shell is immersed in an external fluid medium and contains an internal fluid, and airflow in an external fluid medium moves with a constant velocity. The different parameters were used to see how laminate specification affected nois… Show more

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Cited by 47 publications
(30 citation statements)
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“…By collecting the equations of motion (6)(7)(8) and boundary condition (16)(17), a system of five equations consist of P 0 , U n , V n , W n , A n and B n is obtained. Finally the solutions for <U n , V n , W n , A n , B n > vector are expressed by P 0 which can be eliminated later.…”
Section: Resultsmentioning
confidence: 99%
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“…By collecting the equations of motion (6)(7)(8) and boundary condition (16)(17), a system of five equations consist of P 0 , U n , V n , W n , A n and B n is obtained. Finally the solutions for <U n , V n , W n , A n , B n > vector are expressed by P 0 which can be eliminated later.…”
Section: Resultsmentioning
confidence: 99%
“…On the internal and external shell surfaces, the particle velocities of the acoustic media in the radial direction have to be equal to the normal velocity of the shell [7]. Applying Newton's second law, the equations which describe the effect of acoustic pressure on the motion of the shell can be derived as:…”
Section: Boundary Conditions At the Fluid-structure Interfacesmentioning
confidence: 99%
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“…Analytical and experimental studies are conducted by Lee and Kim sound transmission through the infinitely long circular cylindrical shell 12 . Daneshjou et al 13,14 obtained an exact solution to calculation of the transmission loss of orthotropic and laminated composite cylindrical shells by considering all three displacements of the shell. Harris 15 studied acoustic emission through flat panels.…”
Section: Introductionmentioning
confidence: 99%