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Some properties of sink-flow turbulent boundary layers

Published online by Cambridge University Press:  29 March 2006

W. P. Jones  and
B. E. Launder
W. P. Jones
Affiliation:
Department of Mechanical Engineering, Imperial College, London Present address: Lehrstuhl für Technische Thermodynamik, Technische Hochschule, Aachen, West Germany.
B. E. Launder
Affiliation:
Department of Mechanical Engineering, Imperial College, London
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Abstract

An experimental study of asymptotic sink-flow turbulent boundary layers is reported. Three levels of acceleration corresponding to values of the acceleration parameter K of 1·5 × 10−6, 2·5 × 10×6 and 3·0 × 10×6 have been examined. In addition to mean velocity profiles, measurements have been obtained of the profiles of longitudinal turbulence intensity, and, for the lowest value of K, of the lateral and transverse components as well. Measurements at selected positions in the boundary layer of the power spectral density indicate that none of the boundary layers exhibit an inertial subrange; for the steepest acceleration, in particular, throughout the boundary layer the spectrum shapes are similar in form to those reported within the viscous sublayer of a high Reynolds number turbulent flow.

Type
Research Article
Information
Journal of Fluid Mechanics , Volume 56 , Issue 2 , 28 November 1972 , pp. 337 - 351
Copyright
© 1972 Cambridge University Press

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References

Badri Narayanan, M. A. & Ramjee, V. 1968 On the criteria for reverse transition in a two-dimensional boundary-layer flow. India Inst. Sci. Rep. AE 68 FM 1.
Bradshaw, P. 1965 A compact null-reading, tilting U-tube micromanometer with a rigid liquid container. J. Sci. Instrum. 42, 677.Google Scholar
Champagne, F. H., Sleicher, C. A. & Wehrmann, O. H. 1967 Turbulence measurements with inclined hot wires. J. Fluid Mech. 28, 153.Google Scholar
Coles, D. E. 1956 The law of the wake in a turbulent boundary layer. J. Fluid Mech. 1, 191.Google Scholar
Coles, D. E. 1957 Remarks on the equilibrium turbulent boundary layer. J. Aero. Sci. 24, 495.Google Scholar
Coles, D. E. 1962 The turbulent boundary layer in a compressible fluid. Rand Rep.403-PR.
Comte-Bellot, G. 1965 Ecoulement turbulent entre deux parois parallèles. Publ. vSci. Tech. Minst. de l'Air.
Herring, H. J. & Norbury, J. F. 1967 Experiments on equilibrium turbulent boundary layers in favourable pressure gradients. J. Fluid Mech. 27, 541.Google Scholar
Jones, W. P. 1967 Strongly accelerated turbulent boundary layers. M.Sc. thesis, University of London.
Jones, W. P. 1971 Laminarization in strongly accelerated boundary layers. Ph.D. thesis, University of London.
Julien, H. L., Kays, W. M. & Moffat, R. J. 1969 The turbulent boundary layer on a porous plate: experiment study of the effects of a favourable pressure gradient. Stanford University, Thermo. Sci. Div. Rep. HMT-4.
Klebanoff, P. S. 1954 N.A.C.A. Tech. Note, no. 3178.
Launder, B. E. & Jones, W. P 1969 Sink-flow turbulent boundary layers. J. Fluid Mech. 38, 817.Google Scholar
Launder, B. E. & Stinchcombe, H. S. 1967 Non-normal similar boundary layers. Imperial College, Mech. Engng Dept. Rep. TWF/TN/21.
Loyd, R. J., Moffat, R. J. & Kays, W. M. 1970 The turbulent boundary layer on a porous plate: an experimental study of the fluid dynamics with strong favourable pressure gradients and blowing. Stanford University, Thermo. Sci. Div. Rep. HMT-13.
McMillan, F. A. 1956 Experiments on pitot tubes in shear flow. Aero. Res. Counc. Rep. no. 3028.
Patel, V. C. 1965 Calibration of Preston tube and limitations of its use in pressure gradients. J. Fluid Mech. 23, 185.Google Scholar
Schraub, F. A. & Kline, S. J. 1965 Stanford University, Mech. Engng Dept. Rep. MD-12.