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dc.contributor.authorLorite-Díez, Manuel
dc.contributor.authorJiménez González, José Ignacio
dc.contributor.authorPastur, Luc
dc.contributor.authorCadot, Olivier
dc.contributor.authorMartínez Bazán, Carlos
dc.date.accessioned2025-01-20T08:29:41Z
dc.date.available2025-01-20T08:29:41Z
dc.date.issued2020-03-24
dc.identifier.citationJournal of Wind Engineering and Industrial Aerodynamicses_ES
dc.identifier.urihttps://hdl.handle.net/10481/99617
dc.description.abstractThe use of rear cavities at the base of a square-back Ahmed body has been experimentally evaluated as a passive control device under cross-wind conditions with yaw angles lower tha 10 degrees, by means of pressure, force and velocity measurements. A comparative study has been performed at a Reynolds number Re = 100000, considering the reference square-back body (i.e. the body without any passive control device), and the same body implementing both straight and curved cavities as add-on devices. It is shown that the performance of a straight cavity, which is widely acknowledged as a robust drag reduction device for car models, is hindered under moderate cross-wind conditions, and does not constitute an efficient control strategy, especially when compared with a curved cavity. In particular, when the freestream is aligned with the body, the curved cavity provides a stronger attenuation of the fluctuating nature and the bi-stable dynamics of the wake (characteristic of the wake behind a square-back Ahmed body) than the straight one. Besides, the reduced size of the near wake, which is provoked by ow re-orientation and the reduced span between the rear edges of the curved cavity, leads to an important base pressure recovery, that translates into relative reductions of the drag of 9.1% in comparison with the reference case (i.e. 2.6%, with respect to the straight cavity). The results are considerably improved under cross-wind conditions, since the increase with the yaw angle of the force is particularly intense for the body with the straight cavity and attenuated for the model with the curved cavity. Thus, the relative reduction of the drag coefficient with respect to the reference body becomes negligible for the straight device at a yaw angle of 10 degrees, while it still represents approximately a 10% for the curved cavity. Furthermore, ow visualizations show that the wake is deflected as the incident ow is increasingly yawed, leading to the formation of a single leeward vortex core that approaches progressively the body, decreasing the base pressure. This phenomenon is minored when a curved cavity is implemented, increasing the low pressure induced at the body base.es_ES
dc.description.sponsorshipThis work has been partially supported by the Spanish MINECO and European Funds under projects DPI2017-89746-R and DPI2017-88201-C3-2-R. Moreover, J.I.J.G. and M.L.D want to thank the Spanish MECD for the financial support provided, respectively, under José Castillejo grant CAS18/00379 and Fellowship FPU 014/02945es_ES
dc.language.isoenges_ES
dc.publisherElsevieres_ES
dc.rightsAttribution-NonCommercial-NoDerivatives 4.0 Internacional*
dc.rights.urihttp://creativecommons.org/licenses/by-nc-nd/4.0/*
dc.subjectDrag reductiones_ES
dc.subjectAerodynamics es_ES
dc.subjectAhmed bodyes_ES
dc.titleDrag reduction on a three-dimensional blunt body with different rear cavities under cross-wind conditionses_ES
dc.typejournal articlees_ES
dc.rights.accessRightsopen accesses_ES
dc.identifier.doihttps://doi.org/10.1016/j.jweia.2020.104145
dc.type.hasVersionAMes_ES


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Attribution-NonCommercial-NoDerivatives 4.0 Internacional
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