dc.contributor.author |
D.G. Mabey |
en_US |
dc.contributor.author |
G.P. Ilott |
en_US |
dc.date.accessioned |
2014-10-20T11:05:05Z |
|
dc.date.available |
2014-10-20T11:05:05Z |
|
dc.date.issued |
1967 |
en_US |
dc.identifier.other |
ARC/CP-1006 |
en_US |
dc.identifier.uri |
https://reports.aerade.cranfield.ac.uk/handle/1826.2/1019 |
|
dc.description.abstract |
Wind tunnel measurements of lift, pitching moment and drag on one plane and two cambered wings of "mild ogee" planfom (p = 8/15) are reported. These measurements are supplemented by vapour screen and oil flow observations. The wings were designed by slender wing theory for attached flow along the leading-edge at particular values of lift and pitching moment. The design and measured attachment conditions agreed fairly well. The non-linear lift developed could be related with the type of vortex development above the attachment incidence. |
en_US |
dc.relation.ispartofseries |
Aeronautical Research Council Current Papers |
en_US |
dc.title |
The Longitudinal Characteristics of Three Slender "Mild Ogee" Wings at Mach Numbers from 0.4 to 2.0 |
en_US |