Acoustic scattering by cascades with complex boundary conditions: compliance, porosity and impedance

被引:8
作者
Baddoo, Peter J. [1 ,2 ]
Ayton, Lorna J. [1 ]
机构
[1] Univ Cambridge, Dept Appl Math & Theoret Phys, Ctr Math Sci, Cambridge, England
[2] Imperial Coll London, Dept Math, Huxley Bldg,South Kensington Campus, London SW7 2AZ, England
基金
英国工程与自然科学研究理事会;
关键词
wave scattering; wave-structure interactions; RAYLEIGH CONDUCTIVITY; AERODYNAMIC NOISE; SOUND GENERATION; FLOW; FREQUENCIES; PLATE; MODEL; GUST; EDGE;
D O I
10.1017/jfm.2020.417
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
We present a solution for the scattered field caused by an incident wave interacting with an infinite cascade of blades with complex boundary conditions. This extends previous studies by allowing the blades to be compliant, porous or satisfy a generalised impedance condition. Beginning with the convected wave equation, we employ Fourier transforms to obtain an integral equation amenable to the Wiener-Hopf method. This Wiener-Hopf system is solved using a method that avoids the factorisation of matrix functions. The Fourier transform is inverted to obtain an expression for the acoustic potential function that is valid throughout the entire domain. We observe that the principal effect of complex boundary conditions is to perturb the zeros of the Wiener-Hopf kernel, which correspond to the duct modes in the inter-blade region. We focus efforts on understanding the role of porosity, and present a range of results on sound transmission and generation. The behaviour of the duct modes is discussed in detail in order to explain the physical mechanisms behind the associated noise reductions. In particular, we show that cut-on duct modes do not exist for arbitrary porosity coefficients. Conversely, the acoustic far-field modes are unchanged by modifications to the boundary conditions. We apply our solution to a cascade of perforated plates and see that a fractional open area of 1 % is sufficient to significantly attenuate backscattering. The solution is essentially analytic (the only numerical requirements are matrix inversion and root finding) and is therefore extremely rapid to compute.
引用
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页数:45
相关论文
共 38 条
[1]  
[Anonymous], 1934, J R Aeronaut Soc, DOI [DOI 10.1017/S0368393100109915, 10.1017/S0368393100109915]
[2]  
[Anonymous], 1998, Cambridge Monographs on Mechanics
[3]   The importance of the unsteady Kutta condition when modelling gust-aerofoil interaction [J].
Ayton, Lorna J. ;
Gill, J. R. ;
Peake, N. .
JOURNAL OF SOUND AND VIBRATION, 2016, 378 :28-37
[4]   Acoustic scattering by a finite rigid plate with a poroelastic extension [J].
Ayton, Lorna J. .
JOURNAL OF FLUID MECHANICS, 2016, 791 :414-438
[5]  
Baddoo P. J., ARXIV191107382
[6]   An analytic solution for gust-cascade interaction noise including effects of realistic aerofoil geometry [J].
Baddoo, Peter J. ;
Ayton, Lorna J. .
JOURNAL OF FLUID MECHANICS, 2020, 886
[7]   MATHEMATICAL JUSTIFICATION OF THE RAYLEIGH CONDUCTIVITY MODEL FOR PERFORATED PLATES IN ACOUSTICS [J].
Bendali, Abderrahmane ;
Fares, M'Barek ;
Piot, Estelle ;
Tordeux, Sebastien .
SIAM JOURNAL ON APPLIED MATHEMATICS, 2013, 73 (01) :438-459
[8]   On a two-dimensional mode-matching technique for sound generation and transmission in axial-flow outlet guide vanes [J].
Bouley, Simon ;
Francois, Benjamin ;
Roger, Michel ;
Posson, Helene ;
Moreau, Stephane .
JOURNAL OF SOUND AND VIBRATION, 2017, 403 :190-213
[9]   Fundamental problems with the model of uniform flow over acoustic linings [J].
Brambley, Edward James .
JOURNAL OF SOUND AND VIBRATION, 2009, 322 (4-5) :1026-1037
[10]   Acoustic impedance of a cylindrical orifice [J].
Brandao, Rodolfo ;
Schnitzer, Ory .
JOURNAL OF FLUID MECHANICS, 2020, 892