2020
DOI: 10.1007/s11431-019-1501-3
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Development of acoustic liner in aero engine: a review

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Cited by 40 publications
(18 citation statements)
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“…The minimisation of the objective functions is achieved through a Particle Swarm Optimization (PSO) algorithm, using a swarm with ten individuals per variable. In the proposed approach, the optimisation variables are the equivalent lengths of the cells h i , bounded allowing a range of ∆φ of 2π for each cell, see Equation (3). The bulk modulus and the inertia tensor of each metafluid cell are then evaluated with Equation (9).…”
Section: Resultsmentioning
confidence: 99%
See 1 more Smart Citation
“…The minimisation of the objective functions is achieved through a Particle Swarm Optimization (PSO) algorithm, using a swarm with ten individuals per variable. In the proposed approach, the optimisation variables are the equivalent lengths of the cells h i , bounded allowing a range of ∆φ of 2π for each cell, see Equation (3). The bulk modulus and the inertia tensor of each metafluid cell are then evaluated with Equation (9).…”
Section: Resultsmentioning
confidence: 99%
“…Huge research has been conducted on low noise technologies for engine components to alleviate the aviation-related community noise, e.g., the acoustic liners that extensively cover the inner surfaces of modern turbofan nacelles, being the single-degree-of-freedom liners particularly effective for tonal noise abatement [3], acting on one of the primary sources on aircraft. The evolution of turbofans, however, is leading towards a further increase of the bypass ratio and fan diameters, as confirmed by the comparison between CFM International Leap and CFM-56 or the General Electric GE9x with GE90.…”
Section: Introductionmentioning
confidence: 99%
“…6). Each one covers an area of 10 Â 5 cm 2 , although the operating area is restricted to 7 Â 5 cm 2 . With such dimensions active control can be efficient up to approximately 2 kHz.…”
Section: Methodsmentioning
confidence: 99%
“…Recent aircraft engines developments have been focusing on decreasing the fan's rotation speed, with the aim of reducing their fuel consumption. Consequently, the frequencies of the tonal noise emitted with such architectures are lower than for previous engine generations [1,2]. Absorbing sound within this new frequency range would not be such a challenge if the space and the weight allocated to the acoustic treatment were not limited.…”
Section: Introductionmentioning
confidence: 99%
“…Hence, the sound field due to rotating sources in turbomachines is of great interest, especially, in terms of sound absorbers. The calculation of the sound field and the acoustic energy flow may help to develop and to improve the acoustic absorption performance of micro-perforated duct absorber of axial fans [1][2][3] and acoustic liners, which were integrated into the casing around an aircraft engine [4,5]. For those absorbers, the best absorption performance is obtained if the angle of the acoustic intensity vector corresponds to the normal direction of the absorbing surface.…”
Section: Introductionmentioning
confidence: 99%