BiGlobal and point vortex methods for the instability analysis of wakes
| Data(s) |
01/12/2013
|
|---|---|
| Resumo |
To better understand destruction mechanisms of wake-vortices behind aircraft, the point vortex method for stability (inviscid) used by Crow 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 flnite área vortex model, gives rise to results somewhat different from the point vortex model. It adds more parameters to the problem, but is more realistic. |
| Formato |
application/pdf |
| Identificador | |
| Idioma(s) |
eng |
| Publicador |
E.T.S.I. Aeronáuticos (UPM) |
| Relação |
http://oa.upm.es/30030/1/INVE_MEM_2013_164980L.pdf info:eu-repo/semantics/altIdentifier/doi/10.2514/6.2013-2820 |
| Direitos |
http://creativecommons.org/licenses/by-nc-nd/3.0/es/ info:eu-repo/semantics/openAccess |
| Fonte |
31st AIAA Applied Aerodynamics Conference : proceedings | 31st AIAA Applied Aerodynamics Conference | 24/06/2013 - 27/06/2013 | San Diego, CA, USA |
| Palavras-Chave | #Mecánica |
| Tipo |
info:eu-repo/semantics/conferenceObject Ponencia en Congreso o Jornada PeerReviewed |