Hostname: page-component-78c5997874-g7gxr Total loading time: 0 Render date: 2024-11-17T15:10:44.521Z Has data issue: false hasContentIssue false

The acoustic analogy in an annular duct with swirling mean flow

Published online by Cambridge University Press:  10 June 2013

H. Posson*
Affiliation:
Department of Applied Mathematics and Theoretical Physics, University of Cambridge, Wilberforce Road, Cambridge CB3 0WA, UK
N. Peake
Affiliation:
Department of Applied Mathematics and Theoretical Physics, University of Cambridge, Wilberforce Road, Cambridge CB3 0WA, UK
*
Email address for correspondence: [email protected]

Abstract

This paper is concerned with modelling the effects of swirling flow on turbomachinery noise. We develop an acoustic analogy to predict sound generation in a swirling and sheared base flow in an annular duct, including the presence of moving solid surfaces to account for blade rows. In so doing we have extended a number of classical earlier results, including Ffowcs Williams & Hawkings’ equation in a medium at rest with moving surfaces, and Lilley’s equation for a sheared but non-swirling jet. By rearranging the Navier–Stokes equations we find a single equation, in the form of a sixth-order differential operator acting on the fluctuating pressure field on the left-hand side and a series of volume and surface source terms on the right-hand side; the form of these source terms depends strongly on the presence of swirl and radial shear. The integral form of this equation is then derived, using the Green’s function tailored to the base flow in the (rigid) duct. As is often the case in duct acoustics, it is then convenient to move into temporal, axial and azimuthal Fourier space, where the Green’s function is computed numerically. This formulation can then be applied to a number of turbomachinery noise sources. For definiteness here we consider the noise produced downstream when a steady distortion flow is incident on the fan from upstream, and compare our results with those obtained using a simplistic but commonly used Doppler correction method. We show that in all but the simplest case the full inclusion of swirl within an acoustic analogy, as described in this paper, is required.

Type
Papers
Copyright
©2013 Cambridge University Press 

Access options

Get access to the full version of this content by using one of the access options below. (Log in options will check for institutional or personal access. Content may require purchase if you do not have access.)

References

Ali, A. A. & Atassi, H. M. 2002 Scattering of acoustic and vorticity disturbances by an unloaded annular cascade in a swirling flow. In 8th AIAA/CEAS Aeroacoustics Conference and Exhibit, Breckenridge, CO.Google Scholar
Atassi, H. M., Ali, A. A., Atassi, O. V. & Vinogradov, I. V. 2004 Scattering of incidence disturbances by an annular cascade in a swirling flow. J. Fluid Mech. 499, 111138.CrossRefGoogle Scholar
Bender, C. M. & Orszag, S. A. 1978 Advanced Mathematical Methods for Scientists and Engineers. Asymptotic Methods and Perturbation Theory. McGraw-Hill.Google Scholar
Bers, A. N. 1983 Space–time evolution of plasma instabilities – absolute and convective. In Basic Plasma Physics, Handbook of Plasma Physics (ed. Sudan, A. A. & Galeev, R. N.), vol. 1, pp. 451517. North-Holland.Google Scholar
Brambley, E. J. 2007 The acoustics of curved and lined cylindrical ducts with mean flow. PhD thesis, University of Cambridge.Google Scholar
Briggs, R. J. 1964 Electron-Stream Interaction with Plasmas. MIT.CrossRefGoogle Scholar
Carpenter, P. W. 1985 A linearized theory for swirling supersonic jets and its application to shock-cell noise. AIAA J. 23, 19021909.Google Scholar
Carpenter, P. W. & Johannesen, N. H. 1975 An extension of one-dimensional theory to inviscid swirling flow through choked nozzles. Aeronaut. Q. 26, 7187.Google Scholar
Chanaud, R. C. 1965 Observations of oscillatory motion in certain swirling flows. J. Fluid Mech. 21, 111127.Google Scholar
Colonius, T. & Lele, S. K. 2004 Computational aeroacoustics: progress on nonlinear problems of sound generation. Prog. Aeronaut. Sci. 40, 345416.Google Scholar
Colonius, T., Lele, S. K. & Moin, P. 1997 Sound generation in a mixing layer. J. Fluid Mech. 330, 375409.CrossRefGoogle Scholar
Cooper, A. J. & Peake, N. 2002 The stability of a slowly diverging swirling jet. J. Fluid Mech. 473, 389411.Google Scholar
Cooper, A. J. & Peake, N. 2005 Upstream-radiated rotor–stator interaction noise in mean swirling flow. J. Fluid Mech. 523, 219250.Google Scholar
Cooper, A. J. & Peake, N. 2006 Rotor–stator interaction noise in swirling flow: stator sweep and leans effects. AIAA J. 44 (5), 981991.Google Scholar
Curle, N. 1955 The influence of solid boundaries upon aerodynamic sound. Proc. R. Soc. Lond. A 231, 505514.Google Scholar
Doak, P. E. 1972 Analysis of internally generated sound in continuous materials: 2. A critical review of the conceptual adequacy and physical scope of existing theories of aerodynamic noise, with special reference to supersonic jet noise. J. Sound Vib. 25 (2), 263335.Google Scholar
Doak, P. E. 1973 Fundamentals of aerodynamic sound theory and flow duct acoustics. J. Sound Vib. 28 (3), 527561.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
Elhadidi, B. & Atassi, H. M. 2002 High frequency sound radiation from an annular cascade in swirling flows. In 8th AIAA/CEAS Aeroacoustics Conference and Exhibit, Breckenridge, CO.Google Scholar
Elhadidi, B. & Atassi, H. M. 2003 High frequency formulation for interaction noise in annular cascades. In 9th AIAA/CEAS Aeroacoustics Conference and Exhibit, Paper 2003-3133.Google Scholar
Elhadidi, B., Atassi, H. M., Envia, E. & Podboy, G. G. 2000 Evolution of rotor wake in swirling flow. In 6th AIAA/CEAS Aeroacoustics Conference and Exhibit, Lahaina, HI.Google Scholar
Envia, E., Tweedt, D. L., Woodward, R. P., Elliott, D. M., Fite, E. B., Hughes, C. E., Podboy, G. G. & Sutliff, D. L. 2008 An assessment of current fan noise prediction capability. In 14th AIAA/CEAS Aeroacoustics Conference and Exhibit, Vancouver, Canada.Google Scholar
Evers, I. & Peake, N. 2002 On sound generation by the interaction between turbulence and a cascade of airfoils with non-uniform mean flow. J. Fluid Mech. 463, 2552.Google Scholar
Farassat, F. 1977 Discontinuities in aerodynamics and aeroacoustics: the concept and applications of generalized derivatives. J. Sound Vib. 55 (2), 165193.Google Scholar
Farassat, F. 1994 Introduction to generalized functions with applications in aerodynamics and aeroacoustics. Tech. Rep. Technical Paper 3428.Google Scholar
Ffowcs Williams, J. E. & Hawkings, D. L. 1969 Sound generation by turbulence and surfaces in arbitrary motion. Proc. R. Soc. Lond. A 264, 321342.Google Scholar
Glegg, S. A. L. 1999 The response of a swept blade row to a three-dimensional gust. J. Sound Vib. 227 (1), 2964.CrossRefGoogle Scholar
Glegg, S. A. L. & Jochault, C. 1998 Broadband self-noise from a ducted fan. AIAA J. 36 (8), 13871395.Google Scholar
Goldstein, M. E. 1984 Aeroacoustics of turbulent shear flows. Annu. Rev. Fluid. Mech. 16, 263285.Google Scholar
Goldstein, M. E. 1976 Aeroacoustics. McGraw-Hill.Google Scholar
Goldstein, M. E. 2001 An exact form of Lilley’s equation with a velocity quadrupole/temperature dipole source term. J. Fluid Mech. 443, 231236.Google Scholar
Goldstein, M. E. 2003 A generalized acoustic analogy. J. Fluid Mech. 488, 315333.Google Scholar
Goldstein, M. E., Dittmar, J. H. & Gelder, T. F. 1974 Combined quadrupole–dipole model for inlet flow distortion noise from a subsonic fan. NASA Tech. Rep. TM D-7676.Google Scholar
Goldstein, M. E. & Leib, S. J. 2008 The aeroacoustics of slowly diverging supersonic jets. J. Fluid Mech. 600, 291337.CrossRefGoogle Scholar
Goldstein, M. E., Sescu, A. & Afsar, M. Z. 2012 Effect of non-parallel mean flow on the Green’s function for predicting the low frequency sound from turbulent air jets. J. Fluid Mech. 695, 199234.Google Scholar
Golubev, V. V. & Atassi, H. M. 1995 Aerodynamic and acoustic response of a blade row in unsteady swirling flow. In 1st AIAA/CEAS Aeroacoustics Conference and Exhibit, Munich, Germany, vol. I, pp. 167–175.Google Scholar
Golubev, V. V. & Atassi, H. M. 1996 Sound propagation in an annular duct with mean potential swirling flow. J. Sound Vib. 198, 601616.Google Scholar
Golubev, V. V. & Atassi, H. M. 1998 Acoustic-vorticity waves in swirling flows. J. Sound Vib. 209, 203222.Google Scholar
Golubev, V. V. & Atassi, H. M. 2000a Unsteady swirling flows in annular cascades. Part 1. Evolution of incident disturbance. AIAA J. 38 (7), 11421149.Google Scholar
Golubev, V. V. & Atassi, H. M. 2000b Unsteady swirling flows in annular cascades. Part 2. Aerodynamic blade response incident disturbance. AIAA J. 38 (7), 11501158.Google Scholar
Hanson, D. B. 1976Near field noise of high tip speed propellers in forward flight. In 3rd AIAA Aero-Acoustics Conference, Palo Alto, CA.Google Scholar
Hanson, D. B. 2001a Broadband noise of fans. With unsteady coupling theory to account for rotor and stator reflection/transmission effects. Contractor Report CR-211136-REV1. NASA.Google Scholar
Hanson, D. B. 2001b Theory of broadband noise for rotor and stator cascade with inhomogeneous inflow turbulence including effects of lean and sweep. Contractor Report CR-210762. NASA.Google Scholar
Heaton, C. J. & Peake, N. 2005 Acoustic scattering in a duct with mean swirling flow. J. Fluid Mech. 540, 189220.CrossRefGoogle Scholar
Heaton, C. J. & Peake, N. 2006 Algebraic and exponential instability of inviscid swirling flow. J. Fluid Mech. 565, 279318.Google Scholar
Howe, M. S. & Liu, J. T. C. 1977 The generation of sound by vorticity waves in swirling duct flows. J. Fluid Mech. 81, 369383.CrossRefGoogle Scholar
Hughes, C. E., Jeracki, R. J., Woodward, R. P. & Miller, C. J. 2002 Fan noise source diagnostic test – rotor alone aerodynamic performance results. In 8th AIAA/CEAS Aeroacoustics Conference and Exhibit, Breckenridge, CO.Google Scholar
Jones, D. S. 1982 The Theory of Generalised Functions, 2nd edn. Cambridge University Press.Google Scholar
Karabasov, S. A., Afsar, M. Z., Hynes, T. P., Dowling, A. P., McMullan, W. A., Pokora, C. D., Page, G. J. & McGuirk, J. J. 2010 Jet noise – acoustic analogy informed by large eddy simulation. AIAA J. 48 (7), 13121324.Google Scholar
Kerrebrock, J. L. 1977 Small disturbances in turbomachine annuli with swirl. AIAA J. 15 (6), 794803.Google Scholar
Khorrami, M. R. 1991 A Chebyshev spectral collocation method using a staggered grid for the stability of cylindrical flows. Intl J. Numer. Meth. Fluids 12, 825833.Google Scholar
Koch, L. D. 2012 Predicting the inflow distortion tone noise of the NASA Glenn advanced noise control fan with a combined quadrupole–dipole model. In 18th AIAA/CEAS Aeroacoustics Conference and Exhibit, Colorado Springs, CO.Google Scholar
Kousen, K. A. 1995 Eigenmode analysis of ducted flows with radially dependent axial and swirl components. In 1st AIAA/CEAS Aeroacoustics Conference and Exhibit, Munich, Germany.Google Scholar
Kousen, K. A. 1996 Pressure modes in ducted flows with swirl. In 2nd AIAA/CEAS Aeroacoustics Conference and Exhibit, Paper 96-1679.Google Scholar
Lighthill, M. J. 1952 On sound generated aerodynamically: I. General theory. Proc. R. Soc. Lond. A 211 (1107), 564587.Google Scholar
Lilley, G. M. 1974 On the noise from jets. AGARD CP-131.Google Scholar
Lloyd, A. E. D. & Peake, N. 2008 Rotor–stator broadband noise prediction. In 14th AIAA/CEAS Aeroacoustics Conference and Exhibit, Vancouver, Canada.Google Scholar
Lu, H. Y., Ramsay, J. W. & Miller, D. L. 1976 Noise of swirling exhaust jets. In 3rd AIAA Aero-Acoustics Conference, Palo Alto, CA.Google Scholar
Morfey, C. L. 1971 Tone radiation from an isolated subsonic rotor. J. Acoust. Soc. Am. 49 (5), 16901692.Google Scholar
Morfey, C. L. & Wright, M. C. M. 2007 Extensions of Lighthill’s acoustic analogy with application to computational aeroacoustics. Proc. R. Soc. Lond. A 463, 21012127.Google Scholar
Najafi-Yazdi, A., Brès, G. A. & Mongeau, L. 2011 An acoustic analogy formulation for moving sources in uniformly moving media. Proc. R. Soc. Lond. A 467, 144165.Google Scholar
Nallasamy, M. & Envia, E. 2005 Computation of rotor wake turbulence noise. J. Sound Vib. 282, 649678.CrossRefGoogle Scholar
Nijboer, R. J. 2001 Eigenvalues and eigenfunctions of ducted swirling flows. In 7th AIAA/CEAS Aeroacoustics Conference and Exhibit, Maastricht, The Netherlands.Google Scholar
Peake, N. & Parry, A. B. 2012 Modern challenges facing turbomachinery aeroacoustics. Annu. Rev. Fluid. Mech. 44, 227248.Google Scholar
Podboy, G. G., Krupar, M. J., Helland, S. M. & Hughes, C. E. 2002a Steady and unsteady flow field measurements within a NASA 22 inch fan model. In 8th AIAA/CEAS Aeroacoustics Conference and Exhibit, Breckenridge, CO.Google Scholar
Podboy, G. G., Krupar, M. J., Hughes, C. E. & Woodward, R. P. 2002b Fan noise source diagnostic test – LDV measured flow field results. In 8th AIAA/CEAS Aeroacoustics Conference and Exhibit, Breckenridge, CO.Google Scholar
Posson, H. 2008 Fonctions de réponse de grille d’aubes et effet d’écran pour le bruit à large bande des soufflantes. PhD thesis, Ecole Centrale de Lyon.Google Scholar
Posson, H. & Moreau, S. 2011 Rotor-shielding effect on fan-OGV broadband noise prediction. In 17th AIAA/CEAS Aeroacoustics Conference and Exhibit, Portland, OR.Google Scholar
Posson, H., Moreau, S. & Roger, M. 2010a On the use of a uniformly valid analytical cascade response function for broadband noise predictions. J. Sound Vib. 329 (18), 37213743.Google Scholar
Posson, H., Moreau, S. & Roger, M. 2011 Broadband noise prediction of fan outlet guide vane using a cascade response function. J. Sound Vib. 330, 61536183.Google Scholar
Posson, H. & Peake, N. 2012 Acoustic analogy in swirling mean flow applied to predict rotor trailing-edge noise. In 18th AIAA/CEAS Aeroacoustics Conference and Exhibit, Colorado Springs, CO.Google Scholar
Posson, H. & Roger, M. 2011 Experimental validation of a cascade response function for fan broadband noise predictions. AIAA J. 49 (9), 19071918.Google Scholar
Posson, H., Roger, M. & Moreau, S. 2010b Upon a uniformly valid analytical rectilinear cascade response function. J. Fluid Mech. 663, 2252.Google Scholar
Reinhard, H. 1982 Equations Différentielles: Fondements et Applications, chap. 6, pp. 257–279. Bordas.Google Scholar
Rienstra, S. W. 1999 Sound transmission in slowly varying circular and annular lined ducts with flow. J. Fluid Mech. 380, 279296.Google Scholar
Roger, M. & Arbey, H. 1985 Relation de dispersion des ondes de pression dans un écoulement tournant. Acustica 59, 95101.Google Scholar
Tam, C. K. W. & Auriault, L. 1998 The wave modes in ducted swirling flows. J. Fluid Mech. 371, 120.Google Scholar
Topol, D. A. 1999 TFaNS tone fan noise design/prediction system. Volume I: System description, CUP3D technical documentation and manual for code developers. Contractor Report CR-1999-208882. NASA.Google Scholar
Tyler, J. M. & Sofrin, T. G. 1962 Axial flow compressor noise studies. SAE Trans. 70, 309332.Google Scholar
Ventres, C. S., Theobald, M. A. & Mark, W. D. 1982 Turbofan noise generation, Volume 1: Analysis. Contractor Report CR-167952. NASA.Google Scholar
Yu, Y. K. & Chen, R. H. 1997 A study of screech tone noise of supersonic swirling jets. J. Sound Vib. 205, 698705.Google Scholar