| dc.contributor.author | Roberts, Steven Dwight | |
| dc.date.accessioned | 2014-09-29T19:41:09Z | |
| dc.date.available | 2014-09-29T19:41:09Z | |
| dc.date.issued | 1997-07-01 | |
| dc.identifier.uri | https://hdl.handle.net/11244/12365 | |
| dc.description.abstract | This study was conducted to provide new knowledge and tools for investigating control of unsteady leading edge vortex flows typically found on highly swept aircraft planforms. Methods for controlling the unsteady strength and spatial characteristics ofthe vortices in the flowfield using leading edge flaps were modeled and compared to existing experimental data. The model has also provided a method for investigating new ideas in control ofunsteady separated vortical flows. | |
| dc.format | application/pdf | |
| dc.language | en_US | |
| dc.publisher | Oklahoma State University | |
| dc.rights | Copyright is held by the author who has granted the Oklahoma State University Library the non-exclusive right to share this material in its institutional repository. Contact Digital Library Services at lib-dls@okstate.edu or 405-744-9161 for the permission policy on the use, reproduction or distribution of this material. | |
| dc.title | Model for Evaluating Control of Unsteady Leading Edge Vortex Flows | |
| dc.type | text | |
| osu.filename | Thesis-1997-R647m.pdf | |
| osu.accesstype | Open Access | |
| dc.type.genre | Thesis | |
