Low speed aerodynamic characteristics of 60 degrees rounded leading-edge delta wing with vortex flaps
| dc.contributor.author | Rinoie, K. | en_UK |
| dc.date | 1996 | en_UK |
| dc.date.accessioned | 2005-11-23T12:21:27Z | |
| dc.date.available | 2005-11-23T12:21:27Z | |
| dc.date.issued | 1996 | en_UK |
| dc.description.abstract | Low speed wind tunnel studies have been conducted to investigate the effect of vortex flaps with a rounded leading-edge on delta wing performance. Measurements were done using the 60º delta wing at a Reynolds number based on the centre line chord 8x10(5). Results indicated that the rounded leading-edge delta wing with 30º vortex flap deflection improves the lift/drag ratio at lift coefficients higher than 0.4, when compared with the sharp leading-edge flat delta wing. The effect of a trailing-edge flap with vortex flaps was also investigated. | en_UK |
| dc.description.sponsorship | The University | en_UK |
| dc.format.extent | 1963 bytes | |
| dc.format.extent | 1302767 bytes | |
| dc.format.mimetype | text/plain | |
| dc.format.mimetype | application/pdf | |
| dc.identifier.uri | https://hdl.handle.net/1826/229 | |
| dc.language.iso | en_UK | en_UK |
| dc.relation.ispartofseries | College of Aeronautics Report;9611 | en_UK |
| dc.relation.ispartofseries | CU/CoA/R;9611 | en_UK |
| dc.title | Low speed aerodynamic characteristics of 60 degrees rounded leading-edge delta wing with vortex flaps | en_UK |
| dc.type | Technical Report | en_UK |