<?xml version="1.0" encoding="UTF-8"?><?xml-stylesheet type="text/xsl" href="static/style.xsl"?><OAI-PMH xmlns="http://www.openarchives.org/OAI/2.0/" xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance" xsi:schemaLocation="http://www.openarchives.org/OAI/2.0/ http://www.openarchives.org/OAI/2.0/OAI-PMH.xsd"><responseDate>2026-04-14T06:54:16Z</responseDate><request verb="GetRecord" identifier="oai:www.recercat.cat:2117/338205" metadataPrefix="oai_dc">https://recercat.cat/oai/request</request><GetRecord><record><header><identifier>oai:recercat.cat:2117/338205</identifier><datestamp>2026-01-21T04:59:21Z</datestamp><setSpec>com_2072_1033</setSpec><setSpec>col_2072_452950</setSpec></header><metadata><oai_dc:dc xmlns:oai_dc="http://www.openarchives.org/OAI/2.0/oai_dc/" xmlns:dc="http://purl.org/dc/elements/1.1/" xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance" xmlns:doc="http://www.lyncode.com/xoai" xsi:schemaLocation="http://www.openarchives.org/OAI/2.0/oai_dc/ http://www.openarchives.org/OAI/2.0/oai_dc.xsd">
   <dc:title>Ferrofluid moving thin films for active flow control</dc:title>
   <dc:creator>Arias Montenegro, Francisco Javier</dc:creator>
   <dc:contributor>Universitat Politècnica de Catalunya. Departament de Mecànica de Fluids</dc:contributor>
   <dc:subject>Àrees temàtiques de la UPC::Enginyeria mecànica::Mecànica de fluids</dc:subject>
   <dc:subject>Àrees temàtiques de la UPC::Aeronàutica i espai::Aerodinàmica</dc:subject>
   <dc:subject>Airplanes -- Wings</dc:subject>
   <dc:subject>Surface active agents</dc:subject>
   <dc:subject>Fluid dynamics</dc:subject>
   <dc:subject>Ferrofluid</dc:subject>
   <dc:subject>Boundary layer separation</dc:subject>
   <dc:subject>Active flow control</dc:subject>
   <dc:subject>Avions -- Ales</dc:subject>
   <dc:subject>Avions -- Materials</dc:subject>
   <dc:subject>Agents tensioactius</dc:subject>
   <dc:subject>Dinàmica de fluids</dc:subject>
   <dc:description>Ferrofluid moving thin films and their possible significance with regard to active flow control for lift and attack angle enhancement are discussed. In this strategy, a very thin film of ferrofluid is strongly attached at the wall of the wing by a normal magnetic field from below and pumped tangentially along the wing. Utilizing a simplified physical model and from the available experimental data on moving walls, the expected lift enhancement and effect on the attack angle were assessed. Additional research and design is required in order to explore the possibilities in the use of ferrofluid moving thin films</dc:description>
   <dc:description>This research was supported by the Spanish Ministry of Economy and Competitiveness under fellowship grant Ramon y Cajal: RYC-2013-13459</dc:description>
   <dc:description>Postprint (author's final draft)</dc:description>
   <dc:date>2021-01-12</dc:date>
   <dc:type>Article</dc:type>
   <dc:identifier>Arias, F.J. Ferrofluid moving thin films for active flow control. "Chinese journal of aeronautics", 2021, vol. 34, núm. 5, p. 115-119</dc:identifier>
   <dc:identifier>1000-9361</dc:identifier>
   <dc:identifier>https://hdl.handle.net/2117/338205</dc:identifier>
   <dc:identifier>10.1016/j.cja.2020.11.008</dc:identifier>
   <dc:language>eng</dc:language>
   <dc:relation>https://www.sciencedirect.com/science/article/pii/S1000936120305471</dc:relation>
   <dc:rights>http://creativecommons.org/licenses/by-nc-nd/3.0/es/</dc:rights>
   <dc:rights>Open Access</dc:rights>
   <dc:rights>Attribution-NonCommercial-NoDerivs 3.0 Spain</dc:rights>
   <dc:format>5 p.</dc:format>
   <dc:format>application/pdf</dc:format>
   <dc:publisher>Elsevier</dc:publisher>
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