Effect of surface suction on crossflow instability and transition occuring near a swept attachment-line
| dc.contributor.author | Smith, A. | en_UK |
| dc.contributor.author | Poll, D. I. A. | |
| dc.date | 1998 | en_UK |
| dc.date.accessioned | 2005-11-23T12:20:23Z | |
| dc.date.available | 2005-11-23T12:20:23Z | |
| dc.date.issued | 1998 | en_UK |
| dc.description.abstract | 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. | en_UK |
| dc.description.sponsorship | Cranfield University | en_UK |
| dc.format.extent | 1963 bytes | |
| dc.format.extent | 2187998 bytes | |
| dc.format.mimetype | text/plain | |
| dc.format.mimetype | application/pdf | |
| dc.identifier.uri | http://hdl.handle.net/1826/204 | |
| dc.language.iso | en_UK | en_UK |
| dc.relation.ispartofseries | College of Aeronautics Report;9802 | en_UK |
| dc.relation.ispartofseries | CU/CoA;9802 | en_UK |
| dc.title | Effect of surface suction on crossflow instability and transition occuring near a swept attachment-line | en_UK |
| dc.type | Technical Report | en_UK |