Broadband noise reduction by circular multi-cavity mufflers operating in multimodal propagation conditions

Abstract In this study, sound propagation through a circular duct with non-locally lining is investigated both numerically and experimentally. The liner concept is based on perforated screens backed by air cavities. Dimensions of the cavity are chosen to be of the order or bigger than the wavelength so acoustic waves within the liner can propagate parallel to the duct surface. This gives rise to complex scattering mechanisms among duct modes which renders the muffler more effective over a broader frequency range. This work emanates from the Cleansky European HEXENOR project which aim is to identify the best multi-cavity muffler configuration for reduction of exhaust noise from helicopter turboshaft engines. Here, design parameters are the cavity dimensions in both longitudinal and azimuthal directions. The best cavity configuration must in addition fit weight specifications which implies that the number of walls separating each cavity should be chosen as small as possible. To achieve these objectives, the scattering matrix of the lined duct section is obtained experimentally for two specific muffler configurations operating in multimodal propagation conditions. The good agreement with numerical predictions serves to validate the perforate plate impedance model used in our calculation. Finally, given an incident acoustic pressure which is representative of typical combustion noise spectrum, the best cavity configuration achieving the maximum overall acoustic Transmission Loss is selected numerically. The study also illustrates how the acoustic performances are dependent on the nature of the incident field.

[1]  Ali H. Nayfeh,et al.  Acoustics of Aircraft Engine-Duct Systems , 1975 .

[2]  Irving B. Crandall,et al.  Theory of Vibrating Systems and Sound , 2015 .

[3]  Stéphane Moreau,et al.  Combustion Noise in Modern Aero-Engines , 2014 .

[4]  T. H. Melling,et al.  The acoustic impendance of perforates at medium and high sound pressure levels , 1973 .

[6]  Xiaodong Jing,et al.  Broadband Acoustic Liner Based on the Mechanism of Multiple Cavity Resonance , 2007 .

[7]  David W. Herrin,et al.  Enhancing micro-perforated panel attenuation by partitioning the adjoining cavity , 2010 .

[8]  Vincent Pagneux,et al.  Characteristics of penalty mode scattering by rigid splices in lined ducts. , 2007, The Journal of the Acoustical Society of America.

[9]  Mats Åbom,et al.  A New Type of Muffler Based on Microperforated Tubes , 2011 .

[10]  K. Uno Ingard,et al.  Noise Reduction Analysis , 2009 .

[11]  Azzedine Sitel,et al.  Multiload procedure to measure the acoustic scattering matrix of a duct discontinuity for higher order mode propagation conditions , 2006 .

[12]  Stéphane Lidoine,et al.  Numerical prediction of SDOF-Perforated Plate Acoustic Treatment Impedance. Part 1 : Linear domain , 2007 .

[13]  D. J. Mead Wave propagation and natural modes in periodic systems: I. Mono-coupled systems , 1975 .

[14]  Mohamed Taktak,et al.  An indirect method for the characterization of locally reacting liners. , 2010, The Journal of the Acoustical Society of America.

[15]  Mats Åbom,et al.  On optimal design of mufflers using micro-perforated panels , 2010 .

[16]  E. Perrey-Debain,et al.  Side-branch resonators modelling with Green׳s function methods , 2014 .

[17]  A. W. Guess Calculation of perforated plate liner parameters from specified acoustic resistance and reactance , 1975 .

[18]  Masanobu Namba,et al.  Application of the equivalent surface source method to the acoustics of duct systems with non-uniform wall impedance , 1980 .

[19]  Zhenbo Lu,et al.  An investigation on the characteristics of a non-locally reacting acoustic liner , 2016 .

[20]  Hans Bodén,et al.  On Semi-Empirical Liner Impedance Modeling with Grazing Flow , 2003 .

[21]  D. Maa,et al.  Potential of microperforated panel absorber , 1998 .