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Numerical model of propeller vortex wakes for calculation of induced velocities

dc.contributor.authorDuarte, Rogério
dc.contributor.authorCampos, J. A. C. Falcão de
dc.date.accessioned2013-07-23T15:12:24Z
dc.date.available2013-07-23T15:12:24Z
dc.date.issued1997
dc.description.abstractA numerical model for partial alignment of propeller vortex wakes with the flow is investigated. A lifting line representation of the propeller blades is used combined with the vortex lattice discretization method. The model takes into account radial contraction and axial variation of the pitch of the trailing vortices. The convergence of the iterative pitch alignment procedure and the influence of the number of vortex elements is studied in the case of an optimum moderately loaded propeller. The effects of axial variation of pitch and contraction are investigated for the same optimum circulation distribution case. The model is applied to the vortex wake of propeller DTRC 4119 and results are compared with experimental data.por
dc.identifier.urihttp://hdl.handle.net/10400.26/4565
dc.language.isoengpor
dc.peerreviewednopor
dc.subjectPropellerpor
dc.subjectVortex wakepor
dc.subjectInduced velocitiespor
dc.titleNumerical model of propeller vortex wakes for calculation of induced velocitiespor
dc.typeconference object
dspace.entity.typePublication
oaire.citation.conferencePlaceGuimarãespor
oaire.citation.titleV Encontro Nacional de Mecânica Computacionalpor
person.familyNameDuarte
person.givenNameRogério
person.identifier.ciencia-idEA18-DF0E-51DD
person.identifier.orcid0000-0002-3880-5440
rcaap.rightsopenAccesspor
rcaap.typeconferenceObjectpor
relation.isAuthorOfPublication71a72905-326d-4290-9d48-bc22414709a3
relation.isAuthorOfPublication.latestForDiscovery71a72905-326d-4290-9d48-bc22414709a3

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