Hostname: page-component-cd9895bd7-mkpzs Total loading time: 0 Render date: 2024-12-31T14:00:11.852Z Has data issue: false hasContentIssue false
  • English
  • Français

The Steady Flow Through a Cascade of Closely Spaced Circular Cylinders

Published online by Cambridge University Press:  04 July 2016

B. W. Roberts
B. W. Roberts*
Affiliation:
Department of Mechanical Engineering, The University of Sydney
Get access Rights & Permissions [Opens in a new window]

Extract

Two recent papers by Bradshaw have drawn attention to instabilities in the flow through wind tunnel screens. In Plate 1 of ref. 2 a smoke tunnel photograph shows the manner in which the jets coalesce behind a high blockage, two-dimensional cascade. In the present note, three points relating to this flow will be discussed.

Type
Technical Notes
Information
The Aeronautical Journal , Volume 70 , Issue 669 , September 1966 , pp. 886 - 887
Copyright
Copyright © Royal Aeronautical Society 1966

Access options

Get access to the full version of this content by using one of the access options below. (Log in options will check for institutional or personal access. Content may require purchase if you do not have access.)

References

1.Bradshaw, P.The effect of wind tunnel screens on nominally two-dimensional boundary layers. J. Fluid Mech, Vol. 22, p 4, p 679, 1965.CrossRefGoogle Scholar
2.Bradshaw, P. The effect of wind tunnel screens on “two- dimensional” boundary layers. Nat Phy Labs, Aero Rep no. 1085, 1963.Google Scholar
3.Roberts, B. W. Aeroelastic vibrations in a row of circular cylinders. PhD Dissertation, Cambridge University.Google Scholar
4.Von Bohl, . Das Verhalten Paralleler Luft Strahen. Ing-Archiv, Vol. 11, Heft 4, p 295, 1940.CrossRefGoogle Scholar
5.Sawyer, R. A.The flow due to a two-dimensional jet issuing parallel to a flat plate. J. Fluid Mech, Vol. 9, p 4, p 543, 1960.CrossRefGoogle Scholar