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An Experiment on Flat Plate Turbulent Boundary Layer Flow—The Effect of Local Fluid Addition on Friction and Velocity Distribution

Published online by Cambridge University Press:  04 July 2016

Henry Barrow
Henry Barrow*
Affiliation:
Department of Mechanical Engineering, University of Liverpool
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Extract

For a Flat Surface at zero incidence in a deep uniform stream, the total frictional drag F per unit width of the surface can be calculated from the well known equation

Using the momentum principle in the usual way, it can be shown that when fluid is added locally to the flow through the surface, the total frictional drag F1 is given by

Type
Technical Notes
Information
The Aeronautical Journal , Volume 62 , Issue 566 , February 1958 , pp. 135 - 138
Copyright
Copyright © Royal Aeronautical Society 1958

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References

1.Eckert, E. R. G. (1950). Introduction to the Transfer of Heat and Mass. (First Edition). McGraw-Hill Book Co. Inc., p. 75, 1950.Google Scholar
2.Eckert, E. R. G., Diaguila, A. J. and Donoughe, P. L. (1955). Experiments on Turbulent Flow Through Channels Having Porous Rough Surfaces With or Without Air Injection. N.A.C.A. T.N. 3339, 1955.Google Scholar
3.Fluid Motion Panel of the Aeronautical Research Committee and Others. Modern Developments in Fluid Dynamics. Edited by Goldstein, S.. Clarendon Press, Oxford, Vol. 2, Chapter 12.Google Scholar
4.Klebanoff, P. S. and Diehl, Z. W. (1951). Some Features of Artificially Thickened Fully Developed Turbulent Boundary Layers With Zero Pressure Gradient. N.A.C.A. T.N. 2475, 1951.Google Scholar
5.Preston, J. H. (1950). The Three-Quarter Radius Pitot Tube Flow Meter. Engineering, p. 400, October 1950.Google Scholar
6.Preston, J. H. (1957). The Minimum Reynolds Numbers for Turbulent Boundary Layers and the Functions of Transition Devices. A.R.C. 19,006, F.M. 2,494, A.I. Report, Unclassified, 1957.Google Scholar