dc.contributor.author |
R. D. Mills |
en_US |
dc.date.accessioned |
2014-10-21T15:56:59Z |
|
dc.date.available |
2014-10-21T15:56:59Z |
|
dc.date.issued |
1966 |
en_US |
dc.identifier.other |
ARC/R&M-3515 |
en_US |
dc.identifier.uri |
http://cclib-3.dmz.cranfield.ac.uk:8080/xmlui/handle/123456789/4093 |
|
dc.identifier.uri |
https://reports.aerade.cranfield.ac.uk/handle/1826.2/4093 |
|
dc.description.abstract |
The steady flow incompressible laminar boundary-layer problem
in two-dimensions is posed as an integral equation in Crocco variables in the most general case.
Numerical investigations are then made of the 'similarity' flows. A transformation is utilised which weakens the singularity at the
outer edge of the boundary layer and thereby gives improved numerical results over those obtained from the un-transformed
equation.
An extensive numerical comparison is made with Polhausen's exact analytical solution. Results are also presented in tabular and graphical form illustrating the approach of the boundary-layer characteristics cy, 61, 62, 63 to their asymptotic values for strong suction for a very wide range of similarity flows.
These are in complete agreement with the results obtained by other investigators, and form an extension to the cases previously considered. |
en_US |
dc.relation.ispartofseries |
Aeronautical Research Council Reports & Memoranda |
en_US |
dc.title |
The steady laminar incompressible boundary-layer problem as an integral equation in crocco variables: investigation of the similarity flows |
en_US |