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Miniature Pressure Probe for Measuring the Surface-Shear-Stress Vector in Turbulent Flow

Published online by Cambridge University Press:  07 June 2016

N. Pontikos
Affiliation:
Department of Aeronautics, Imperial College, London
P. Bradshaw
Affiliation:
Department of Aeronautics, Imperial College, London
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Summary

If two small fences are arranged approximately at right angles in plan view, the magnitude and direction of surface shear stress can be deduced from measurements of the pressure difference across each fence. Fence heights as small as 0.05 mm are easily achieved. The device is simpler to use than null-seeking arrangements, and is accurate even in the presence of strong pressure gradients, which are shown to have large effects on other types of surface obstacle in three-dimensional flow.

Type
Research Article
Copyright
Copyright © Royal Aeronautical Society. 1981

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References

1 Konstantinov, N.I. and Dragnysh, G.L., The measurement of friction stress on a surface. English translation DSIR DTS 1499, 1960.Google Scholar
2 Meier, H.U. and Kreplin, H.P., Experimental investigation of the boundary layer transition and separation on a body of revolution. Z. Flugwiss., Vol. 4, pp 6571, 1980.Google Scholar
3 Patel, V.C., Calibration of the Preston tube and limitations on its use in pressure gradients. J. Fluid Mech., Vol. 23, pp 185208, 1965.CrossRefGoogle Scholar
4 Preston, J.H., The determination of turbulent skin friction by means of Pitot tubes. J. Roy. Aero. Soc., Vol. 58, pp 109121, 1954.Google Scholar
5 Vagt, J.D. and Fernholz, H., Use of surface fences to measure wall shear stress in three-dimensional boundary layers. Aero. Quart., Vol. 26, pp 8791, 1973.Google Scholar
6 Winter, K.G., An outline of the techniques available for the measurement of skin friction in turbulent boundary layers. Prog. Aero. Sci., Vol. 18, pp 157, 1977.Google Scholar