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Calculation of the Normal-Stress Distribution in a Curved Wall Jet

Published online by Cambridge University Press:  04 July 2016

R. J. Kind
R. J. Kind*
Affiliation:
Carleton University, Ottawa, Canada West Virginia University
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Extract

In many applications of boundary-layer control by tangential blowing the surface downstream of the blowing slot is likely to be strongly curved. For example, this is the case when blowing around a bluff trailing edge is used to control the circulation around an aerofoil as described in ref. 1. The flow involved in such cases is that of a curved wall jet in an adverse pressure gradient. A knowledge of the radial and tangential pressure distributions in the curved wall jet is required if development of the flow and separation are to be predicted.

Type
Technical Notes
Information
The Aeronautical Journal , Volume 75 , Issue 725 , May 1971 , pp. 343 - 348
Copyright
Copyright © Royal Aeronautical Society 1971 

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References

1. Kind, R. J. and Maull, D. J., An experimental investigation of a low-speed circulation-controlled aerofoil. Aeronautical Quarterly, Vol. XIX, p. 170, 1968.Google Scholar
2. Wygnanski, I. and Newman, B. G. The effect of jet entrainment on lift and moment for a thin aerofoil with blowing. Aeronautical Quarterly, Vol. XV, p. 122, 1964.Google Scholar
3. Kind, R. J., A calculation method for circulation control by tangential blowing around a bluff trailing edge. Aeronautical Quarterly, Vol. XIX, p. 205, 1968.Google Scholar
4. Gartshore, I. S. and Newman, B. G. The turbulent wall jet in an arbitrary pressure gradient. Aeronautical Quarterly, Vol. XX, p. 25, 1969.Google Scholar
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8. Kind, R. J. A proposed method of circulation control. Ph.D. dissertation, University of Cambridge, 1967.Google Scholar