| dc.creator |
Babister, A. W. |
|
| dc.date |
2012-06-14T13:55:48Z |
|
| dc.date |
2012-06-14T13:55:48Z |
|
| dc.date |
1951-03 |
|
| dc.date.accessioned |
2022-05-09T10:17:18Z |
|
| dc.date.available |
2022-05-09T10:17:18Z |
|
| dc.identifier |
http://dspace.lib.cranfield.ac.uk/handle/1826/7227 |
|
| dc.identifier.uri |
https://reports.aerade.cranfield.ac.uk/handle/1826.2/4718 |
|
| dc.description |
This is an interim report giving measurement s that have so far been made of pressure distribution on two untapered wings swept back 45◦, aspect ratio 2 and 4, fitted with both full span and part span trailing edge split flaps. The Reynolds number in these tests was about 0.5x106. |
|
| dc.language |
en |
|
| dc.publisher |
College of Aeronautics, Cranfield. |
|
| dc.relation |
College Report |
|
| dc.relation |
43 |
|
| dc.title |
Measurements of the pressure distribution on swept back wings with trailing edge split flaps: summary of wind tunnel work at the College of Aeronautics 1948 - 50 |
|
| dc.type |
Report |
|