dc.contributor.author |
D. H. Peckham |
en_US |
dc.contributor.author |
S. A. Atkinson |
en_US |
dc.date.accessioned |
2014-10-20T11:02:38Z |
|
dc.date.available |
2014-10-20T11:02:38Z |
|
dc.date.issued |
1960 |
en_US |
dc.identifier.other |
ARC/CP-508 |
en_US |
dc.identifier.uri |
https://reports.aerade.cranfield.ac.uk/handle/1826.2/521 |
|
dc.description.abstract |
This note gives preliminary results of low speed balance measurements and flow visualisation tests, on a wing of aspect ratio 1.0. The wing had a convex parabolic leading-edge shape in plan view, and an unswept trailing edge - such wings are now termed "Gothic". All edges were sharp, the centre section was 12% biconvex, and transverse sections were diamond-shaped. Results of tests on a strictly comparable delta wing are not yet available, but where possible the results are compared with tests on other wings of aspect ratio 1.0 with unswept trailing edges. |
en_US |
dc.relation.ispartofseries |
Aeronautical Research Council Current Papers |
en_US |
dc.title |
Preliminary Results of Low Speed Wind Tunnel Tests on a Gothic Wing of Aspect Ratio 1.0 |
en_US |