Aerodynamic investigation of a morphing wing for micro air vehicle by means of PIV

Bardera, Rafael; Rodríguez Sevillano, A.; García Magariño, A.

Publicación:
Aerodynamic investigation of a morphing wing for micro air vehicle by means of PIV

dc.contributor.author	Bardera, Rafael
dc.contributor.author	Rodríguez Sevillano, A.
dc.contributor.author	García Magariño, A.
dc.contributor.funder	Ministerio de Defensa
dc.contributor.orcid	García Magariño, A. [0000-0002-6039-8407]
dc.date.accessioned	2021-04-29T08:03:53Z
dc.date.available	2021-04-29T08:03:53Z
dc.date.issued	2020-10
dc.description.abstract	A wind tunnel tests campaign has been conducted to investigate the aerodynamic flow around a wing morphing to be used in a micro air vehicle. Non-intrusive whole field measurements were obtained by using PIV, in order to compare the velocity and turbulence intensity maps for the modified and the original version of an adaptive wing designed to be used in a micro air vehicle. Four sections and six angles of attack have been tested. Due to the low aspect ratio of the wing and the low Reynold number tested of 6.4 × 104, the influence of the 3D effects has been proved to be important. At high angles of attack, the modified model prevented the detachment of the stream, increased the lift of the wing and reduced the turbulence intensity level on the upper surface of the airfoil and in the wake.	es
dc.description.sponsorship	Funding: This research was funded by Ministry of Defense under the project Termofluidodinámica, IGB 99001	es
dc.identifier.citation	Fluids, 5 (4), art. no. 191 (2020)	es
dc.identifier.doi	10.3390/fluids5040191
dc.identifier.other	https://www.mdpi.com/2311-5521/5/4/191
dc.identifier.uri	http://hdl.handle.net/20.500.12666/431
dc.language.iso	eng	es
dc.publisher	MDPI	es
dc.rights	Attribution-NonCommercial-NoDerivatives 4.0 International	es
dc.rights.accessRights	info:eu-repo/semantics/openAccess
dc.rights.uri	https://creativecommons.org/licenses/by-nc-nd/4.0/
dc.subject	Morphing	es
dc.subject	Wing Camber	es
dc.subject	Ailerons	es
dc.subject	Micro air vehicle	es
dc.subject	Aerodynamics	es
dc.title	Aerodynamic investigation of a morphing wing for micro air vehicle by means of PIV	es
dc.type	info:eu-repo/semantics/article	es
dc.type.coar	http://purl.org/coar/resource_type/c_6501
dc.type.hasVersion	info:eu-repo/semantics/publishedVersion
dspace.entity.type	Publication