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Direct numerical simulation of turbulent flow past a trailing edge and the associated noise generation

Published online by Cambridge University Press:  17 January 2008

RICHARD D. SANDBERG
Affiliation:
School of Engineering Sciences, University of Southampton, Southampton SO17 1BJ, UK
NEIL D. SANDHAM
Affiliation:
School of Engineering Sciences, University of Southampton, Southampton SO17 1BJ, UK

Abstract

Direct numerical simulations (DNS) are conducted of turbulent flow passing an infinitely thin trailing edge. The objective is to investigate the turbulent flow field in the vicinity of the trailing edge and the associated broadband noise generation. To generate a turbulent boundary layer a short distance from the inflow boundary, high-amplitude lifted streaks and disturbances that can be associated with coherent outer-layer vortices are introduced at the inflow boundary. A rapid increase in skin friction and a decrease in boundary layer thickness and pressure fluctuations is observed at the trailing edge. It is demonstrated that the behaviour of the hydrodynamic field in the vicinity of the trailing edge can be predicted with reasonable accuracy using triple-deck theory if the eddy viscosity is accounted for. Point spectra of surface pressure difference are shown to vary considerably towards the trailing edge, with a significant reduction of amplitude occurring in the low-frequency range. The acoustic pressure obtained from the DNS is compared with predictions from two- and three-dimensional acoustic analogies and the classical trailing-edge theory of Amiet. For low frequencies, two-dimensional theory succeeds in predicting the acoustic pressure in the far field with reasonable accuracy due to a significant spanwise coherence of the surface pressure difference and predominantly two-dimensional sound radiation. For higher frequencies, however, the full three-dimensional theory is required for an accurate prediction of the acoustic far field. DNS data are used to test some of the key assumptions invoked by Amiet for the derivation of the classical trailing-edge theory. Even though most of the approximations are shown to be reasonable, they collectively lead to a deviation from the DNS results, in particular for higher frequencies. Moreover, because the three-dimensional acoustic analogy does not provide significantly improved results, it is suggested that some of the discrepancies can be attributed to the approach of evaluating the far-field sound using a Kirchhoff-type integration of the surface pressure difference.

Type
Papers
Copyright
Copyright © Cambridge University Press 2008

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References

Amiet, R. 1975 Acoustic radiation from an airfoil in a turbulent stream. J. Sound Vib. 41 (4), 407420.CrossRefGoogle Scholar
Amiet, R. 1976 a High-frequency thin airfoil theory for subsonic flow. AIAA J. 14 (8), 10761082.CrossRefGoogle Scholar
Amiet, R. 1976 b Noise due to turbulent flow past a trailing edge. J. Sound Vib. 47 (3), 387393.CrossRefGoogle Scholar
Amiet, R. 1978 Effect of the incident surface pressure field on noise due to turbulent flow past a trailing edge. J. Sound Vib. 57 (2), 305306.CrossRefGoogle Scholar
Bodony, D. & Lele, S. 2002 Spatial scale decomposition of shear layer turbulence and the sound sources associated with the missing scales in a large-eddy simulation. AIAA Paper 20022454.Google Scholar
Brooks, T. & Hodgson, T. 1981 Trailing edge noise prediction from measured surface pressures. J. Sound Vib. 78 (1), 69117.CrossRefGoogle Scholar
Carpenter, M. H., Nordström, J. & Gottlieb, D. 1999 A stable and conservative interface treatment of arbitrary spatial accuracy. J. Comput. Phys. 148 (2), 341365.CrossRefGoogle Scholar
Colonius, T., Lele, S. K. & Moin, P. 1993 Boundary conditions for direct computation of aerodynamic sound generation. AIAA J. 31 (9), 15741582.CrossRefGoogle Scholar
Daniels, P. 1977 Viscous mixing at a trailing edge. J. Mech. Appl. Maths 30 (3), 319342.CrossRefGoogle 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.CrossRefGoogle Scholar
Ffowcs Williams, J. & Hall, L. 1970 Aerodynamic sound generation by turbulent flow in the vicinity of a scattering half plane. J. Fluid Mech. 40 (4), 657670.CrossRefGoogle Scholar
Gajjar, J. & Türkyilmazoglu, M. 2000 On the absolute instability of the triple-deck flow over humps and near wedged trailing edges. Phil. Trans. R. Soc. Lond. A 358, 31133128.CrossRefGoogle Scholar
Goldstein, M. E. 1976 Aeroacoustics, 1st edn. McGraw-Hill.Google Scholar
Howe, M. S. 1978 A review of the theory of trailing edge noise. J. Sound Vib. 61 (3), 437465.CrossRefGoogle Scholar
Hu, Z. W., Morfey, C. L. & Sandham, N. D. 2006 Wall pressure and shear stress spectra from direct simulations of channel flow. AIAA J. 44 (7), 15411549.CrossRefGoogle Scholar
Lighthill, M. 1952 a On sound generated aerodynamically I. General theory. Proc. R. Soc. Lond. A 211, 564587.Google Scholar
Lighthill, M. 1952 b On sound generated aerodynamically II. Turbulence as a source of sound. Proc. R. Soc. Lond. A 222, 132.Google Scholar
Manoha, E., Herrero, C., Sagaut, P. & Redonnet, S. 2002 Numerical prediction of airfoil aerodynamic noise. AIAA Paper 20022573.Google Scholar
Marsden, O., Bogey, C. & Bailly, C. 2006 a Direct noise computation around a 3-D NACA0012 airfoil. AIAA Paper 20062503.Google Scholar
Marsden, O., Bogey, C. & Bailly, C. 2006 b Direct noise computation around a 3-D NACA0012 airfoil. AIAA Paper 20052817.Google Scholar
Messiter, A. F. 1970 Boundary-layer flow near the trailing edge of a flat plate. SIAM J. Appl. Maths 18 (1), 241257.CrossRefGoogle Scholar
Oberai, A., Roknaldin, F. & Hughes, J. 2002 Computation of trailing-edge noise due to turbulent flow over an airfoil. AIAA J. 40 (11), 22062216.CrossRefGoogle Scholar
Sandberg, R. D., Jones, L. E. & Sandham, N. D. 2006 A zonal characteristic boundary condition for numerical simulations of aerodynamic sound. In European Conference on Computational Fluid Dynamics, ECCOMAS CFD 2006 (ed. Wesseling, P., Oñate, E. & Périaux, J.).CrossRefGoogle Scholar
Sandberg, R. D. & Sandham, N. D. 2006 Nonreflecting zonal characteristic boundary condition for direct numerical simulation of aerodynamic sound. AIAA J. 44 (2), 402405.CrossRefGoogle Scholar
Sandberg, R. D., Sandham, N. D. & Joseph, P. F. 2007 Direct numerical simulations of trailing-edge noise generated by boundary-layer instabilities. J. Sound Vib. 304 (3–5), 677690.CrossRefGoogle Scholar
Sandham, N., Li, Q. & Yee, H. 2002 Entropy splitting for high-order numerical simulation of compressible turbulence. J. Comput. Phys. 178, 307322.CrossRefGoogle Scholar
Sandham, N., Yao, Y. & Lawal, A. 2003 Large-eddy simulation of transonic flow over a bump. Int. J. Heat Fluid Flow 24, 584595.CrossRefGoogle Scholar
Schlichting, H. 1979 Boundary Layer Theory, 7th edn. McGraw-Hill.Google Scholar
Seror, C., Sagaut, P., Bailly, C. & Juvé, D. 2001 On the radiated noise computed by large-eddy simulation. Phys. Fluids 13, 476487.CrossRefGoogle Scholar
Singer, B., Brentner, K., Lockard, D. & Lilley, G. 2000 Simulation of acoustic scattering from a trailing edge. J. Sound Vib. 230 (3), 541560.CrossRefGoogle Scholar
Smith, F. T. 1982 On the high reynolds number theory of laminar flows. IMA J. Appl. Maths 28 (3), 207.CrossRefGoogle Scholar
Spalart, P. R. 1988 Direct simulation of a turbulent boundary layer up to r θ = 1410. J. Fluid Mech. 187, 6198.CrossRefGoogle Scholar
Spalding, D. B. 1961 A single formula for the law of the wall. Trans. ASME: J. Appl. Mech. 28 (3), 444458.CrossRefGoogle Scholar
Stewartson, K. 1968 On the flow near the trailing edge of a flat plate. Proc. R. Soc. Lond. A 306, 275290.Google Scholar
Wang, M. & Moin, P. 2000 Computation of trailing-edge flow and noise using large-eddy simulation. AIAA J. 38 (12), 22012209.CrossRefGoogle Scholar
White, F. M. 1991 Viscous Fluid Flow. McGraw Hill.Google Scholar