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Fluctuations in wall-shear stress and pressure at low streamwise wavenumbers in turbulent boundary-layer flow

Published online by Cambridge University Press:  26 April 2006

D. M. Chase
Affiliation:
Chase Inc., 87 Summer Street, Suite 510, Boston, MA 02110, USA

Abstract

Turbulent boundary-layer fluctuations in the incompressive domain are expressed in terms of fluctuating velocity-product 'sources’ in order to elucidate relative characteristics of fluctuating wall-shear stress and pressure in the subconvective range of streamwise wavenumbers. Appropriate viscous wall conditions are applied, and results are obtained to lowest order in this Strouhal-scaled wavenumber which serves as the expansion parameter. The spectral amplitudes of pressure and of the shear stress component directed along the wavevector both contain additive terms proportional to source integrals with exponential wall-distance weighting characteristic respectively of the irrotational and the rotational fields. At low wavenumbers, barring unexpected relative smallness of the pertinent boundary-layer source term, the rotational terms become dominant. There the wall pressure and shear-stress component have spectra that approach the same non-vanishing, wavevector-white but generally viscous-scale-dependent level and are totally coherent with phase difference ½π. The other, irrotational contributions to the shear-stress and pressure amplitudes likewise bear a simple and previously known, generally wavevector– and frequency-dependent, ratio to one another. In an inviscid limit this contribution to the pressure amplitude reduces to the one obtained previously from inviscid treatments. A representative class of models is introduced for the source spectrum, and the resulting rotational contribution to the spectral density of wall pressure and K-aligned shear stress at low (but incompressive) wavenumbers is estimated. It is suggested that this contribution may predominate and account for measured low-wavenumber levels of wall pressure.

Type
Research Article
Copyright
© 1991 Cambridge University Press

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References

Bender, C. M. & Orszag, S. A., 1978 Advanced Mathematical Methods for Scientists and Engineers. McGraw-Hill.
Bergeron, R. F.: 1973 Aerodynamic sound and the low-wavenumber wall-pressure spectrum of nearly incompressible boundary layer turbulence. J. Acoust. Soc. Am. 54, 123133.Google Scholar
Chase, D. M.: 1980 Modeling the wavevector-frequency spectrum of turbulent-boundary-layer wall pressure. J. Sound Vib. 70, 2957.Google Scholar
Chase, D. M.: 1987 The character of the turbulent wall pressure spectrum at subconvective wavenumbers and a suggested comprehensive model. J. Sound Vib. 112, 125147.Google Scholar
Chase, D. M.: 1990 The wavevector—frequency spectrum of pressure on a smooth plane in turbulent boundary-layer flow at low Mach number. J. Acoust. Soc. Am. (in press).Google Scholar
Chase, D. M. & Noiseux, C. F., 1982 Turbulent wall pressure at low wavenumbers: relation to nonlinear sources in planar and cylindrical flow. J. Acoust. Soc. Am. 72, 975982.Google Scholar
Hariri, H. H. & Akylas, T. R., 1985 The wall-shear-stress contribution to boundary-layer noise. Phys. Fluids 28, 27272729.Google Scholar
Howe, M. S.: 1989 Turbulent boundary layer shear stress fluctuations on smooth and rough walls. BBN Systems and Technologies Corp. TM 1025.Google Scholar
Kraichnan, R. H.: 1956 Pressure fluctuations in turbulent flow over a flat plate. J. Acoust. Soc. Am. 28, 278390.Google Scholar
Phillips, O. M.: 1956 On the aerodynamic surface sound from a plane turbulent boundary layer. Proc. R. Soc. Lond. A A234, 327335.Google Scholar