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.contributor.author | Babister, A. W. | |
| dc.date.accessioned | 2012-06-14T13:55:48Z | |
| dc.date.available | 2012-06-14T13:55:48Z | |
| dc.date.issued | 1951-03 | |
| dc.description.abstract | 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. | en_UK |
| dc.identifier.uri | http://dspace.lib.cranfield.ac.uk/handle/1826/7227 | |
| dc.language.iso | en | en_UK |
| dc.publisher | College of Aeronautics, Cranfield. | en_UK |
| dc.relation.ispartofseries | College Report | en_UK |
| dc.relation.ispartofseries | 43 | en_UK |
| 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 | en_UK |
| dc.type | Report | en_UK |