On the use of an analytical cascade response function to predict sound transmission through an annular cascade

The present study aims at developing and assessing an analytical model for the sound transmission through an annular stator row in a configuration without mean flow. The model reformulates a three-dimensional annular model dedicated to turbulence interaction noise to deal with the case of an incident acoustic mode of an annular duct. It is a strip theory approach coupled with a previously published analytical formulation for the unsteady vane loading in a rectilinear cascade. Three formulations are developed on the basis of different definitions of the incident acoustic waves impinging on the rectilinear cascade. The latter are designed to match most of the properties of the incident mode in the annular case. The formulations are compared with a finite element method solution and with a rectilinear cascade model in configurations with no mean flow. The benchmarks consist in four annular ducts from very high (0.98) to moderate (0.5) hub-to-tip ratio containing a possibly staggered annular cascade. The frequency and the radial mode order of the incident mode are varied. Both pressure field and pressure coefficients are compared.

[1]  Nigel Peake,et al.  The scattering of vorticity waves by an infinite cascade of flat plates in subsonic flow , 1993 .

[2]  Stefan A. Sauter,et al.  Is the Pollution Effect of the FEM Avoidable for the Helmholtz Equation Considering High Wave Numbers? , 1997, SIAM Rev..

[3]  R. S. Muir,et al.  The application of a semi-actuator disk model to sound transmission calculations in turbomachinery, part II: Multiple blade rows , 1977 .

[4]  M. Genito,et al.  Achievements in the numerical modeling of fan noise radiation from aero-engines , 2008 .

[5]  Hélène Posson,et al.  Parametric Study of Gust Scattering and Sound Transmission Through a Blade Row , 2007 .

[6]  Alfredo Bermúdez,et al.  An optimal perfectly matched layer with unbounded absorbing function for time-harmonic acoustic scattering problems , 2007, J. Comput. Phys..

[7]  Stéphane Moreau,et al.  Fan-OGV Broadband Noise Prediction Using a Cascade Response , 2009 .

[8]  R. K. Amiet,et al.  Transmission and reflection of sound by two blade rows , 1974 .

[9]  Stewart A. L. Glegg,et al.  Broadband Self-Noise from a Ducted Fan , 1998 .

[10]  S. Kaji,et al.  Propagation of sound waves through a blade row: II. Analysis based on the acceleration potential method , 1970 .

[11]  Gabriel Reboul,et al.  An equivalent-source model for simulating noise generation in turbofan engines , 2009 .

[12]  Jean-Pierre Berenger,et al.  A perfectly matched layer for the absorption of electromagnetic waves , 1994 .

[13]  Michel Roger,et al.  On a uniformly valid analytical rectilinear cascade response function , 2010, Journal of Fluid Mechanics.

[14]  Hélène Posson,et al.  Experimental Validation of a Cascade Response Function for Fan Broadband Noise Predictions , 2011 .

[15]  Nigel Peake,et al.  The interaction between a high-frequency gust and a blade row , 1992, Journal of Fluid Mechanics.

[16]  Donald B. Hanson,et al.  Broadband Noise of Fans: With Unsteady Coupling Theory to Account for Rotor and Stator Reflection/Transmission Effects , 2013 .

[17]  W. D. Mark,et al.  Turbofan noise generation. Volume 1: Analysis , 1982 .

[18]  L. Thompson A review of finite-element methods for time-harmonic acoustics , 2006 .

[19]  Stéphane Moreau,et al.  On the use of a uniformly valid analytical cascade response function for fan broadband noise predictions , 2010 .

[20]  Stewart A. L. Glegg,et al.  The response of a swept blade row to a three-dimensional gust , 1999 .

[21]  S. Kaji,et al.  Generation of sound by rotor-stator interaction , 1970 .

[22]  R. Amiet,et al.  Transmission and Reflection of Sound by a Blade Row , 1971 .

[23]  Matti Lassas,et al.  On the existence and convergence of the solution of PML equations , 1998, Computing.

[24]  Patrick Amestoy,et al.  MUMPS : A General Purpose Distributed Memory Sparse Solver , 2000, PARA.

[25]  S. Kaji,et al.  Propagation of sound waves through a blade row: I. Analysis based on the semi-actuator disk theory , 1970 .

[26]  Hélène Posson Fonctions de réponse de grille d’aubes et effet d’écran pour le bruit à large bande des soufflantes. , 2008 .

[27]  L. Thompson,et al.  A Residual Based Variational Method for Reducing Dispersion Error in Finite Element Methods , 2005 .

[28]  M. Roger,et al.  Acoustic Radiation Modeling of Engine Exhaust. Comparisons Between Analytical and Numerical Methods , 2004 .

[29]  Hafiz M. Atassi,et al.  Passive Control for Turbofan Tonal Noise , 2005 .

[30]  Michel Roger,et al.  Broadband noise prediction of fan outlet guide vane using a cascade response function , 2011 .

[31]  A. Hirschberg,et al.  An introduction to acoustics , 1992 .

[32]  Christopher K. W. Tam,et al.  Perfectly Matched Layer as an Absorbing Boundary Condition for the Linearized Euler Equations in Open and Ducted Domains , 1998 .

[33]  Hafiz M. Atassi,et al.  Scattering of Acoustic Waves by a Rotor , 2008 .

[34]  Donald B. Hanson Coupled 2-dimensional cascade theory for noise and unsteady aerodynamics of blade row interaction in turbofans. Volume 1: Theory development and parametric studies , 1994 .

[35]  Stewart A. L. Glegg Broadband Fan Noise Generated by Small Scale Turbulence , 1998 .

[36]  G. Horvay,et al.  Sound transmission through blade , 1970 .

[37]  Stéphane Moreau,et al.  Prediction of sound transmission through an annular cascade Using an analytical cascade response function , 2010 .

[38]  Nigel Peake,et al.  Resonant acoustic frequencies of a tandem cascade. Part 1. Zero relative motion , 1999 .

[39]  Donald Hanson,et al.  Turbulence/cascade interaction - Spectra of inflow, cascade response, and noise , 1998 .

[40]  W. Koch,et al.  On the transmission of sound waves through a blade row , 1971 .

[41]  Hafiz M. Atassi,et al.  Acoustic and Hydrodynamic Response of an Annular Cascade to Inflow Disturbances in Swirling Flows , 2003 .

[42]  W. Sears,et al.  Reflection and Transmission of Oblique Sound Waves by a Blade Row , 1969 .

[43]  Stéphane Moreau,et al.  Rotor-shielding effect on fan-OGV broadband noise prediction , 2011 .