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On vortex filament methods for linear instability analysis of aircraft wakes

dc.contributor.authorTendero Ventanas, Juan Ángel 
dc.contributor.authorTheofilis, Vassilios
dc.contributor.authorRoura Sues, Miquel
dc.contributor.authorGovindarajan, Rama
dc.contributor.otherIngeniería Mecánica y Diseño Industriales_ES
dc.date.accessioned2025-01-29T07:20:24Z
dc.date.available2025-01-29T07:20:24Z
dc.date.issued2015-06-09
dc.identifier.issn1270-9638
dc.identifier.urihttp://hdl.handle.net/10498/34980
dc.description.abstractLinear stability analysis of vortical systems is discussed in a systematic manner using the classic inviscid vortex filament method. Well-known results are recovered as special cases of a unified linearization procedure. The symmetries of the vortex systems analyzed are exploited to obtain an analytical picture of different classes of growing and decaying eigenmodes. Finally, comparisons with viscous global linear theory reveal the limits of applicability of the vortex filament method for the instability analysis of realistic vortex systems.es_ES
dc.formatapplication/pdfes_ES
dc.language.isoenges_ES
dc.publisherElsevier Masson SASes_ES
dc.rightsAttribution-NonCommercial-NoDerivatives 4.0 Internacional*
dc.rights.urihttp://creativecommons.org/licenses/by-nc-nd/4.0/*
dc.sourceAerospace Science and Technology - 2015, Vol. 44 pp. 51–68es_ES
dc.subjectPoint vortexes_ES
dc.subjectVortex filamentes_ES
dc.subjectAircraft wakees_ES
dc.subjectLinear stability analysises_ES
dc.titleOn vortex filament methods for linear instability analysis of aircraft wakeses_ES
dc.typejournal articlees_ES
dc.identifier.urlhttp://dx.doi.org/10.1016/j.ast.2014.10.018
dc.rights.accessRightsopen accesses_ES
dc.identifier.doi10.1016/j.ast.2014.10.018
dc.type.hasVersionSMURes_ES


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Attribution-NonCommercial-NoDerivatives 4.0 Internacional
This work is under a Creative Commons License Attribution-NonCommercial-NoDerivatives 4.0 Internacional