| dc.creator |
Smith, A. |
|
| dc.date |
1998 |
|
| dc.date |
2005-11-23T12:20:23Z |
|
| dc.date |
2005-11-23T12:20:23Z |
|
| dc.date |
1998 |
|
| dc.date.accessioned |
2022-05-09T10:17:08Z |
|
| dc.date.available |
2022-05-09T10:17:08Z |
|
| dc.identifier |
http://hdl.handle.net/1826/204 |
|
| dc.identifier.uri |
https://reports.aerade.cranfield.ac.uk/handle/1826/204 |
|
| dc.description |
The work contained in this report is concerned with the use of transpiration at the leading edge of swept wings to modify and control transition due to cross-flow instability. Transition conditions are identified on both porous and non-porous surfaces, with and without suction, and the effect of two-dimensional excrescences is considered. Throughout, the application of the results to vehicle design is stressed and, where possible, simple design criteria are presented. |
|
| dc.description |
Cranfield University |
|
| dc.format |
1963 bytes |
|
| dc.format |
2187998 bytes |
|
| dc.format |
text/plain |
|
| dc.format |
application/pdf |
|
| dc.language |
en_UK |
|
| dc.relation |
College of Aeronautics Report;9802 |
|
| dc.relation |
CU/CoA;9802 |
|
| dc.title |
Effect of surface suction on crossflow instability and transition occuring near a swept attachment-line |
|
| dc.type |
Technical Report |
|