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dc.date.accessioned 2018-05-23T14:21:54Z
dc.date.available 2018-05-23T14:21:54Z
dc.date.issued 2005-12
dc.identifier.uri http://sedici.unlp.edu.ar/handle/10915/66978
dc.description.abstract Boundary layer wind tunnel experiments have been conducted to explore differences in the aerodynamic behavior of two autostable or reflexed airfoils, with different positive camber submitted to three different incoming flows with the same mean velocity but with different turbulence characteristics. The variations of lift and drag coefficients due to the path of turbulent structures with different scales are presented. The experiments were performed at a mean speed of 10 m/sec, corresponding to a Reynolds Number of 205000. en
dc.format.extent 301-306 es
dc.language en es
dc.subject aerodynamics; turbulence; low Reynolds number airfoils en
dc.subject Turbulencia es
dc.title About the turbulent scale dependent response of reflexed airfoils en
dc.type Articulo es
sedici.identifier.uri http://www.scielo.org.ar/scielo.php?script=sci_arttext&pid=S0327-07932005000400007 es
sedici.identifier.issn 0327-0793 es
sedici.creator.person Delnero, Juan Sebastián es
sedici.creator.person Colman Lerner, Jorge León es
sedici.creator.person Boldes, Ulfilas es
sedici.creator.person Martínez, Mariano Álvaro es
sedici.creator.person Marañón Di Leo, Julio es
sedici.creator.person Bacchi, Federico es
sedici.subject.materias Ingeniería Aeronáutica es
sedici.description.fulltext true es
mods.originInfo.place Facultad de Ingeniería es
sedici.subtype Articulo es
sedici.rights.license Creative Commons Attribution-NonCommercial 4.0 International (CC BY-NC 4.0)
sedici.rights.uri http://creativecommons.org/licenses/by-nc/4.0/
sedici.description.peerReview peer-review es
sedici.relation.journalTitle Latin American Applied Research es
sedici.relation.journalVolumeAndIssue vol. 35, no. 4 es


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Creative Commons Attribution-NonCommercial 4.0 International (CC BY-NC 4.0) Except where otherwise noted, this item's license is described as Creative Commons Attribution-NonCommercial 4.0 International (CC BY-NC 4.0)