Hostname: page-component-cd9895bd7-dzt6s Total loading time: 0 Render date: 2024-12-27T11:27:52.435Z Has data issue: false hasContentIssue false

An Approximate Solution of the Laminar Boundary Layer on a Flat Plate with Uniform Suction

Published online by Cambridge University Press:  28 July 2016

S. J. Peerless
Affiliation:
Imperial College
D. B. Spalding
Affiliation:
Imperial College

Extract

Boundary layer problems may be divided into two classes: (a) those for which similar solutions can be found, i.e. where the boundary conditions are such that similar profiles differing only in scale factor exist at different sections; and (b) those where the boundary conditions do not effect similarity, so that the development of the boundary layer must be calculated in stages. The latter class are known as “continuation problems,” and very few numerical solutions have been obtained because of the labour involved.

Approximate methods of solving continuation problems are known, using the Karman momentum integral method (e.g. Ref. 1) or variants. Some of these methods make use of velocity profiles calculated for “similar” boundary layers. This note presents a new approximate method which uses “similar” profiles but avoids using the momentum integral. Instead of characterising the boundary layer thickness by the “momentum thickness,” which needs to be calculated yet is of less direct interest, the wall shear stress is used; this stress usually has to be calculated in any case and the present method is therefore comparatively simple.

Type
Technical Notes
Copyright
Copyright © Royal Aeronautical Society 1955

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. Goldstein, S. (editor) (1938). Modern Developments in Fluid Dynamics, Vol. I. Oxford University Press, 1938.Google Scholar
2. Emmons, H. W. and Leigh, D. (1953). Tabulation of the Blasius Function with Blowing and Suction. Interim Tech. Rep. No. 9. Harvard University Comb. Aero. Lab., November 1953.Google Scholar
3. Iglisch, R. (1944). Exakte Berechnung der laminaren Grenzschicht an der längsangeströmten ebenen Platte mit homogener Absaugung. Schrift. Deut. Akad. Luft. January 1944.Google Scholar