| dc.creator |
Rinoie, K. |
|
| dc.date |
1996 |
|
| dc.date |
2005-11-23T12:21:27Z |
|
| dc.date |
2005-11-23T12:21:27Z |
|
| dc.date |
1996 |
|
| dc.date.accessioned |
2022-05-09T10:17:09Z |
|
| dc.date.available |
2022-05-09T10:17:09Z |
|
| dc.identifier |
http://hdl.handle.net/1826/229 |
|
| dc.identifier.uri |
https://reports.aerade.cranfield.ac.uk/handle/1826/229 |
|
| dc.description |
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. |
|
| dc.description |
The University |
|
| dc.format |
1963 bytes |
|
| dc.format |
1302767 bytes |
|
| dc.format |
text/plain |
|
| dc.format |
application/pdf |
|
| dc.language |
en_UK |
|
| dc.relation |
College of Aeronautics Report;9611 |
|
| dc.relation |
CU/CoA/R;9611 |
|
| dc.title |
Low speed aerodynamic characteristics of 60 degrees rounded leading-edge delta wing with vortex flaps |
|
| dc.type |
Technical Report |
|