<?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>2026-04-18T07:36:58Z</responseDate><request verb="GetRecord" identifier="oai:www.recercat.cat:2117/395854" metadataPrefix="oai_dc">https://recercat.cat/oai/request</request><GetRecord><record><header><identifier>oai:recercat.cat:2117/395854</identifier><datestamp>2025-07-22T16:34:16Z</datestamp><setSpec>com_2072_1033</setSpec><setSpec>col_2072_452951</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>Fuselage design and assembly for ONAerospace eVTOL</dc:title>
   <dc:creator>Ros Espinal, Marc</dc:creator>
   <dc:contributor>Universitat Politècnica de Catalunya. Departament de Física</dc:contributor>
   <dc:contributor>Universitat Politècnica de Catalunya. Centre de Cooperació per al Desenvolupament</dc:contributor>
   <dc:contributor>ONAerospace</dc:contributor>
   <dc:contributor>Altmeyer, Sebastian Andreas</dc:contributor>
   <dc:subject>Àrees temàtiques de la UPC::Desenvolupament humà i sostenible::Cooperació per al desenvolupament::Projectes de cooperació</dc:subject>
   <dc:subject>Àrees temàtiques de la UPC::Aeronàutica i espai::Aeronaus</dc:subject>
   <dc:subject>Vertically rising aircraft</dc:subject>
   <dc:subject>Concept design</dc:subject>
   <dc:subject>Body</dc:subject>
   <dc:subject>Wing</dc:subject>
   <dc:subject>Conetail</dc:subject>
   <dc:subject>Vtail</dc:subject>
   <dc:subject>Fatigue points</dc:subject>
   <dc:subject>Materials (aluminum</dc:subject>
   <dc:subject>Composite)</dc:subject>
   <dc:subject>Ribs</dc:subject>
   <dc:subject>Aeronaus</dc:subject>
   <dc:description>The aim of the project is to design a fuselage from zero and the assembly of the aircraft (fuselage, wing, tail and propellers) for ONAerospace.</dc:description>
   <dc:description>Objectius de Desenvolupament Sostenible::9 - Indústria, Innovació i Infraestructura</dc:description>
   <dc:date>2023-10-31</dc:date>
   <dc:type>Master thesis</dc:type>
   <dc:identifier>https://hdl.handle.net/2117/395854</dc:identifier>
   <dc:identifier>PRISMA-181059</dc:identifier>
   <dc:language>eng</dc:language>
   <dc:rights>Open Access</dc:rights>
   <dc:format>application/pdf</dc:format>
   <dc:publisher>Universitat Politècnica de Catalunya</dc:publisher>
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