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Theoretical model of acoustic scattering from a flat plate with serrations

Published online by Cambridge University Press:  18 April 2017

Xun Huang*
Affiliation:
State Key Laboratory of Turbulence and Complex Systems, Aeronautics and Astronautics, College of Engineering, Peking University, Beijing, 100871, China Department of Mechanical and Aerospace Engineering, The Hong Kong University of Science and Technology, Hong Kong, China
*
Email addresses for correspondence: huangxun@pku.edu.cn, huangxun@ust.hk

Abstract

A theoretical model is proposed in this work to study the scattering of sound waves from a serrated flat plat in the presence of a uniform flow, which is of both scientific significance and practical importance. The key contribution is the analytic and rigorous description of the scattering from the laterally periodic serrations by incorporating Fourier series expansions and the Wiener–Hopf method, which collectively give a closed-form analytical solution. To validate and demonstrate the model, a couple of test cases with some representative sinusoidal- and sawtooth-shaped serrations are studied by comparing with a commercial finite element solver. The comparisons show quite good agreement for various set-ups. The subsequent parametric studies further demonstrate the efficiency of the model and the effect of the serrations for noise control. Overall, the proposed theoretical model should be able to assist in studies of low-noise aerofoils and the silent flying capabilities of owls.

Type
Papers
Copyright
© 2017 Cambridge University Press 

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References

Amiet, R. K. 1975 Acoustic radiation from an airfoil in a turbulent stream. J. Sound Vib. 41, 407420.Google Scholar
Ayton, L. J. 2016a Acoustic scattering by a finite rigid plate with a poroelastic extension. J. Fluid Mech. 791, 414438.Google Scholar
Ayton, L. J. 2016b Interaction of turbulence with the leading-edge stagnation point of a thin aerofoil. J. Fluid Mech. 798, 436456.CrossRefGoogle Scholar
Ayton, L. J., Gill, J. R. & Peake, N. 2016 The importance of the unsteady Kutta condition when modelling gustaerofoil interaction. J. Sound Vib. 378, 2837.Google Scholar
Ayton, L. J. & Peake, N. 2013 On high-frequency noise scattering by aerofoils in flow. J. Fluid Mech. 734, 144182.Google Scholar
Brooks, T. F. & Hodgson, T. H. 1981 Trailing edge noise prediction from measured surface pressures. J. Sound Vib. 78 (1), 69117.CrossRefGoogle Scholar
Carley, M. 2006 Scattering by quasi-symmetric pipes. J. Acoust. Soc. Am. 119 (2), 817823.Google Scholar
Chong, T. P. & Dubois, E. 2016 Optimization of the poro-serrated trailing edges for airfoil broadband noise reduction. J. Acoust. Soc. Am. 140 (2), 13611373.Google Scholar
Chong, T. P. & Joseph, F. J. 2013 An experimental study of airfoil instability tonal noise with trailing edge serrations. J. Sound Vib. 332 (24), 63356358.CrossRefGoogle Scholar
Chong, T. P., Vathylakis, A., Joseph, F. J. & Gruber, M. 2013 Self-noise produced by an airfoil with nonflat plate trailing-edge serrations. AIAA J. 51 (11), 26652677.Google Scholar
Dowling, A. P., Ffowcs Williams, J. E. & Goldstein, M. E. 1978 Sound production in a moving stream. Proc. R. Soc. Lond. A. 288 (1353), 321349.Google Scholar
Gabard, G. & Astley, R. J. 2006 Theoretical model for sound radiation from annular jet pipes: far- and near-field solutions. J. Fluid Mech. 549, 315341.Google Scholar
Howe, M. S. 1991a Aerodynamic noise of a serrated trailing edge. J. Fluids Struct. 5, 3345.Google Scholar
Howe, M. S. 1991b Noise produced by a sawtooth trailing edge. J. Acoust. Soc. Am. 90 (1), 482487.Google Scholar
Huang, X., Chan, S., Zhang, X. & Gabriel, S. 2008a Variable structure model for flow-induced tonal noise control with plasma actuators. AIAA J. 46 (1), 241250.CrossRefGoogle Scholar
Huang, X., Chen, X. X., Ma, Z. K. & Zhang, X. 2008b Efficient computation of spinning modal radiation through an engine bypass duct. AIAA J. 46 (6), 14131423.Google Scholar
Huang, X., Zhong, S. Y. & Liu, X. 2014a Acoustic invisibility in turbulent fluids by optimised cloaking. J. Fluid Mech. 749, 460477.CrossRefGoogle Scholar
Huang, X., Zhong, S. Y. & Stalnov, O. 2014b Analysis of scattering from an acoustic cloak in a moving fluid. J. Acoust. Soc. Am. 135, 25712580.Google Scholar
Jaworski, J. W. & Peake, N. 2013 Aerodynamic noise from a poroelastic edge with implications for the silent flight of owls. J. Fluid Mech. 723, 456479.CrossRefGoogle Scholar
Jeon, W. & Lee, D. J. 2008 Acoustic diffraction by a finite airfoil in uniform flow. AIAA J. 46 (12), 29772986.CrossRefGoogle Scholar
Jones, L. & Sandberg, R. 2011 Numerical analysis of tonal airfoil self-noise and acoustic feedback-loops. J. Sound Vib. 330 (25), 61376152.CrossRefGoogle Scholar
Jones, L. E. & Sandberg, R. D. 2012 Acoustic and hydrodynamic analysis of the flow around an aerofoil with trailing-edge serrations. J. Fluid Mech. 706, 295322.Google Scholar
Lilley, G. M.1998 A study of the silent flight of the owl. AIAA Paper, 1998–2340.Google Scholar
Lilley, G. M. 2001 The prediction of airframe noise and comparison with experiment. J. Sound Vib. 239 (4), 849859.CrossRefGoogle Scholar
Liu, X., Jiang, H. B., Huang, X. & Chen, S. 2016 Theoretical model of scattering from flow ducts with semi-infinite axial liner splices. J. Fluid Mech. 786, 6283.Google Scholar
Lyu, B., Azarpeyvand, M. & Sinayoko, S. 2016 Prediction of noise from serrated trailing edges. J. Fluid Mech. 793, 556588.Google Scholar
Munt, R. M. 1977 The interaction of sound with a subsonic jet issuing from a semi-infinite cylindrical pipe. J. Fluid Mech. 83, 609640.Google Scholar
Narayanan, S., Chaitanya, P., Haeri, S., Joseph, P., Kim, J. W. & Polacsek, C. 2015 Airfoil noise reductions through leading edge serrations. Phys. Fluids 27, 025109.CrossRefGoogle Scholar
Noble, B. 1958 Methods Based on the Wiener–Hopf Technique for the Solution of Partial Differential Equations, pp. 4861. Pergamon.Google Scholar
Peers, E. & Huang, X. 2013 High-order schemes for predicting computational aeroacoustic propagation with adaptive mesh refinement. Acta Mechanica Sin. 29 (2), 111.Google Scholar
Rienstra, S. W. 1984 Acoustic radiation from a semi-infinite annular duct in a uniform subsonic mean flow. J. Sound Vib. 94 (2), 267288.CrossRefGoogle Scholar
Roger, M. & Moreau, S. 2005 Back-scattering correction and further extensions of Amiet’s trailing-edge noise model. Part 1: theory. J. Sound Vib. 286, 477506.CrossRefGoogle Scholar
Stalnov, O., Chaitanya, P. & Joseph, P. F. 2016 Towards a non-empirical trailing edge noise prediction model. J. Sound Vib. 372, 5068.Google Scholar
Tide, P. S. & Srinivasan, K. 2010 Adaptive mesh refinement for chevron nozzle jet flows. Appl. Acoust. 71, 201220.Google Scholar
Vathylakis, A., Chong, T. P. & Joseph, P. F. 2015 Poro-serrated trailing edge devices for airfoil self-noise reduction. AIAA J. 53 (11), 33793394.Google Scholar
Veitch, B. & Peake, N. 2008 Acoustic propagation and scattering in the exhaust flow from coaxial cylinders. J. Fluid Mech. 613, 275307.Google Scholar
Wright, M. C. M. 2008 Lecture Notes on the Mathematics of Acoustics, chap. 5, pp. 109144. Imperial College Press.Google Scholar