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Drag of a Circular Cylinder with Vortex Generators

Published online by Cambridge University Press:  04 July 2016

P. N. Joubert  and
E. R. Hoffman
P. N. Joubert
Affiliation:
University of Melbourne, Australia
E. R. Hoffman
Affiliation:
University of Melbourne, Australia
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Extract

The following is a report of preliminary tests to determine the effect of vortex generators on the drag of a circular cylinder. It was thought that with suitable placement of the vortex generators on the cylinder, the laminar separation of the boundary layer at subcritical Reynolds numbers might be delayed, and a reduction in drag coefficient obtained.

Type
Technical Notes
Information
The Aeronautical Journal , Volume 66 , Issue 619 , July 1962 , pp. 456 - 457
Copyright
Copyright © Royal Aeronautical Society 1962

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References

1.Gould, D. G. Use of Vortex Generators to Delay Boundary Layer Separation. Unpublished N.A.E. Laboratory Report.Google Scholar
2.Pearcey, H. H. and Stuart, C. M. Methods of Boundary Layer Control for Postponing and Alleviating Buffeting and Other Effects of Shock Induced Separation. I.A.S. S.M.F. Fund Paper No. F.F. 22.Google Scholar
3.Bairstow, . Applied Aerodynamics. 2nd Edit. Longmans.Google Scholar