Hostname: page-component-78c5997874-ndw9j Total loading time: 0 Render date: 2024-11-05T08:04:33.073Z Has data issue: false hasContentIssue false
  • English
  • Français

Laminar streamwise corner flow with suction

Published online by Cambridge University Press:  04 July 2016

H. A. El-Gamal  and
W. H. Barclay
H. A. El-Gamal
Affiliation:
University College London
W. H. Barclay
Affiliation:
University College London
Get access Rights & Permissions [Opens in a new window]

Extract

The flow along the corner formed by two semi-infinite intersecting flat plates is considered in which the corner line is parallel to the streamlines of a uniform incident flow and a uniform suction is applied at the plate surfaces.

Type
Technical Note
Information
The Aeronautical Journal , Volume 79 , Issue 778 , October 1975 , pp. 466 - 469
Copyright
Copyright © Royal Aeronautical Society 1975 

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. Griffith, A. A. and Meredith, F. W. The possible improvement in aircraft performance due to the use of boundary layer suction. RAE Rep No E3501, March 1936.Google Scholar
2. Rubin, S. G. Incompressible flow along a corner. J. Fluid Mech, Vol 26, Part 1, 1966.Google Scholar
3. Rubin, S. G. and Grossman, B. Viscous flow along a corner: Numerical solution of the corner layer equations. Quart Appl Math, Vol 29, No 2, July 1971.Google Scholar