9th AIAA/CEAS Aeroacoustics Conference and Exhibit 2003
DOI: 10.2514/6.2003-3309
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Design and Attenuation Properties of Periodic Checkerboard Liners

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Cited by 14 publications
(9 citation statements)
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“…The impedance is designed as a compromise to provide tolerable noise attenuation throughout the flight regime (e.g., take off, cruise, and landing). NASA has proven that a liner comprised of patches of resonators, differing in impedance, can achieve better attenuation than any uniform liner [2]. An adjustable resonator has been designed that can change its impedance and, thus, its ability to abate sound [3].…”
Section: A Communal System For Noise Reductionmentioning
confidence: 99%
See 1 more Smart Citation
“…The impedance is designed as a compromise to provide tolerable noise attenuation throughout the flight regime (e.g., take off, cruise, and landing). NASA has proven that a liner comprised of patches of resonators, differing in impedance, can achieve better attenuation than any uniform liner [2]. An adjustable resonator has been designed that can change its impedance and, thus, its ability to abate sound [3].…”
Section: A Communal System For Noise Reductionmentioning
confidence: 99%
“…Engine nacelles accomplish noise abatement typically with uniform liners comprised of large numbers of fixed impedance, homogeneous resonators compromised to provide acceptable noise attenuation throughout the flight regime. NASA has improved attenuation with heterogeneous resonators [2] and has developed adjustable resonators [3]. The challenge is to decide impedances to achieve optimal attenuation as acoustic conditions change.…”
Section: Introductionmentioning
confidence: 99%
“…Although current implementations have uniform liners, research has shown that noise attenuation can be increased by liners in which the resonators are divided into segments of differing impedance: a segmented liner. Mani [6] and Watson [7] proved segmented liners can be designed to significantly outperform the best uniform liner for a given acoustic source.…”
Section: Background On Noise Reduction In Aircraft Engine Nacellesmentioning
confidence: 99%
“…During the design optimization and assessment studies of Watson et al, [3][4][5] they observed that the checkerboard liner appeared significantly more sensitive to variations in the impedance values than did the uniform. This trend was also observed in the initial studies involving axially segmented, circumferentially segmented, and checkerboard liners.…”
Section: Introductionmentioning
confidence: 99%
“…It was concluded that the genetic algorithm was the most reliable of the optimization techniques due to its ability to handle multiple local optima generated by the checkerboard liner. In a subsequent study, Watson et al 4 combined the genetic algorithm with a numerical solution to the Helmholtz equation to demonstrate that an optimized 8-segment checkerboard liner gives considerably more attenuation than an optimum uniform or 4-segmented checkerboard liner. However, central processor unit (CPU) time and memory constraints and the occurrence of multiple local optima limited these results to a single frequency.…”
Section: Introductionmentioning
confidence: 99%