dc.contributor.author |
G. G. Brebner |
en_US |
dc.contributor.author |
J. A. Bagley |
en_US |
dc.date.accessioned |
2014-10-21T15:53:23Z |
|
dc.date.available |
2014-10-21T15:53:23Z |
|
dc.date.issued |
1952 |
en_US |
dc.identifier.other |
ARC/R&M-2886 |
en_US |
dc.identifier.uri |
https://reports.aerade.cranfield.ac.uk/handle/1826.2/3446 |
|
dc.description.abstract |
Results are given of pressure measurements and boundary-layer traverses on a two-dimensional wing with 10 per cent RAE 101 section at Reynolds numbers of 1.6 x 10power6 and 3.2 x 10power6. These results, which have been integrated to give lift, drag and aerodynamic-centre characteristics, are used to check some calculation methods for the growth of the turbulent boundary layer and for the effect of a known boundary layer on the pressure distribution. It is concluded that the calculation of the boundary layer still needs a little refinement before it is accurate enough to predict viscosity effects on pressure distribution, lift, drag and aerodynamic centre; but that these effects can be calculated if the actual boundary-layer characteristics are known. |
en_US |
dc.relation.ispartofseries |
Aeronautical Research Council Reports & Memoranda |
en_US |
dc.title |
Pressure and boundary-layer measurements on a two-dimensional wing at low speed |
en_US |