| dc.creator |
Emslie, K. |
|
| dc.creator |
Hosking, L. |
|
| dc.creator |
Marshall, W. S. D. |
|
| dc.date |
2012-09-11T10:28:04Z |
|
| dc.date |
2012-09-11T10:28:04Z |
|
| dc.date |
1953-02 |
|
| dc.date.accessioned |
2022-05-09T10:17:20Z |
|
| dc.date.available |
2022-05-09T10:17:20Z |
|
| dc.identifier |
http://dspace.lib.cranfield.ac.uk/handle/1826/7559 |
|
| dc.identifier.uri |
https://reports.aerade.cranfield.ac.uk/handle/1826.2/4742 |
|
| dc.description |
Visual methods have been used together with a yawmeter to illustrate conditions of flow in the boundary layer over a sweptback wing. It was found out that at moderate incidences a marked outflow in the boundary layer was developed. Continues … |
|
| dc.language |
en |
|
| dc.publisher |
College of Aeronautics, Cranfield |
|
| dc.relation |
College Reports |
|
| dc.relation |
69 |
|
| dc.title |
Some experiments on the flow in the boundary layer of a 45 degrees sweptback untapered wing of aspect ratio 4 |
|
| dc.type |
Report |
|