BiGlobal and point vortex methods for the instability analysis of wakes


Autoria(s): Tendero Ventanas, Juan Angel; Paredes Gonzalez, Pedro; Theofilis, Vassilios; Roura, Miquel; Govindarajan, Rama
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

http://oa.upm.es/30030/

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