| dc.contributor.author | Tendero Ventanas, Juan Ángel | |
| dc.contributor.author | Paredes González, Pedro | |
| dc.contributor.author | Roura Sues, Miquel | |
| dc.contributor.author | Govindarajan, Rama | |
| dc.contributor.author | Theofilis, Vassilios | |
| dc.contributor.other | Ingeniería Mecánica y Diseño Industrial | es_ES |
| dc.date.accessioned | 2025-01-29T08:09:24Z | |
| dc.date.available | 2025-01-29T08:09:24Z | |
| dc.date.issued | 2013-06-22 | |
| dc.identifier.uri | http://hdl.handle.net/10498/34991 | |
| dc.description.abstract | To better understand destruction mechanisms of wake-vortices behind aircraft, the point vortex method for stability (inviscid) used by Crow 1970 is here compared with viscous modal global stability analysis of the linearized Navier-Stokes equations acting on a two-dimensional basic flow, i.e. BiGlobal stability analysis.
The fact that the BiGlobal method is viscous, and uses a finite area vortex model, gives rise to results somewhat different from the point vortex model. It adds more parameters to the problem, but is more realistic. | es_ES |
| dc.format | application/pdf | es_ES |
| dc.language.iso | eng | es_ES |
| dc.publisher | American Institute of Aeronautics and Astronautics | es_ES |
| dc.rights | Attribution-NonCommercial-NoDerivatives 4.0 Internacional | * |
| dc.rights.uri | http://creativecommons.org/licenses/by-nc-nd/4.0/ | * |
| dc.source | AIAA 2013-2820 | es_ES |
| dc.title | BiGlobal and Point Vortex Methods for the Instability Analysis of Wakes | es_ES |
| dc.type | conference output | es_ES |
| dc.identifier.url | http://arc.aiaa.org/doi/10.2514/6.2013-2820 | |
| dc.rights.accessRights | open access | es_ES |
| dc.identifier.doi | 10.2514/6.2013-2820 | |
| dc.relation.projectID | info:eu-repo/grantAgreement/MICINN//TRA2009-13648/ES/Metodologias Computacionales Para La Prediccion De Inestabilidades Globales Hidrodinamicas Y Aeroacusticas En Flujos Complejos/ | es_ES |
| dc.type.hasVersion | SMUR | es_ES |