dc.contributor.author |
A. Thom |
en_US |
dc.contributor.author |
Laura Klanfer |
en_US |
dc.date.accessioned |
2014-10-21T15:53:15Z |
|
dc.date.available |
2014-10-21T15:53:15Z |
|
dc.date.issued |
1951 |
en_US |
dc.identifier.other |
ARC/R&M-2851 |
en_US |
dc.identifier.uri |
https://reports.aerade.cranfield.ac.uk/handle/1826.2/3407 |
|
dc.description.abstract |
This is a detailed study of the effect of the presence of walls on the flow past a symmetrical aerofoil at zero incidence. The low-speed case is considered first, followed by solutions at a Mach number of 0.7. The methods used are essentially arithmetical, but a new approach is used for the compressible case. The manner in which the walls affect the pressure distribution is clearly shown. |
en_US |
dc.relation.ispartofseries |
Aeronautical Research Council Reports & Memoranda |
en_US |
dc.title |
Tunnel-wall effect on an aerofoil at subsonic speeds |
en_US |