<?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>2026-04-14T06:15:50Z</responseDate><request verb="GetRecord" identifier="oai:www.recercat.cat:2117/329640" metadataPrefix="marc">https://recercat.cat/oai/request</request><GetRecord><record><header><identifier>oai:recercat.cat:2117/329640</identifier><datestamp>2026-02-07T01:00:40Z</datestamp><setSpec>com_2072_1033</setSpec><setSpec>col_2072_452949</setSpec></header><metadata><record xmlns="http://www.loc.gov/MARC21/slim" xmlns:dcterms="http://purl.org/dc/terms/" xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance" xmlns:doc="http://www.lyncode.com/xoai" xsi:schemaLocation="http://www.loc.gov/MARC21/slim http://www.loc.gov/standards/marcxml/schema/MARC21slim.xsd">
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      <subfield code="a">Mola, Andrea</subfield>
      <subfield code="e">author</subfield>
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      <subfield code="a">Tezzele, Marco</subfield>
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      <subfield code="a">Gadalla, Mahmoud</subfield>
      <subfield code="e">author</subfield>
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      <subfield code="a">Valdenazzi, Federica</subfield>
      <subfield code="e">author</subfield>
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      <subfield code="a">Grassi, Davide</subfield>
      <subfield code="e">author</subfield>
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      <subfield code="a">Padovan, Roberta</subfield>
      <subfield code="e">author</subfield>
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      <subfield code="a">Rozza, Gianluigi</subfield>
      <subfield code="e">author</subfield>
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      <subfield code="c">2019</subfield>
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      <subfield code="a">In this work, we present the results of a ship propeller design optimization campaign&#xd;
&#xd;
carried out in the framework of the research project PRELICA, funded by the Friuli Venezia Giulia  &#xd;
regional  government.   The  main  idea  of  this  work  is  to  operate  on  a  multidisciplinary &#xd;
level to identify propeller shapes that lead to reduced tip vortex-induced pressure and increased &#xd;
efficiency without altering the thrust.  First, a specific tool for the bottom-up construction of &#xd;
parameterized propeller blade geometries has been developed.  The algorithm proposed operates with &#xd;
a user defined number of arbitrary shaped or NACA airfoil sections, and employs arbitrary degree &#xd;
NURBS to represent the chord, pitch, skew and rake distribution as a function of the blade radial &#xd;
coordinate.  The control points of such curves have been modified to generate, in a fully automated &#xd;
way, a family of blade geometries depending on as many as 20 shape parameters. Such geometries have &#xd;
then been used to carry out potential flow simulations with the Boundary Element Method based &#xd;
software PROCAL. Given the high number of parameters considered, such a preliminary stage allowed &#xd;
for a fast evaluation of the performance of several hundreds of shapes.  In addition, the data &#xd;
obtained from the potential flow simulation allowed for the appli- cation of a parameter space &#xd;
reduction methodology based on active subspaces (AS) property, which suggested that the main &#xd;
propeller performance indices are, at a first but rather accurate approximation, only depending on &#xd;
a single parameter which is a linear combination of all the original geometric ones.  AS analysis &#xd;
has also been used to carry out a constrained optimization exploiting response surface method in &#xd;
the reduced parameter space, and a sensitivity analysis based on such surrogate model.  The few &#xd;
selected shapes were finally used to set up high fidelity&#xd;
&#xd;
RANS simulations and select an optimal shape.</subfield>
   </datafield>
   <datafield tag="653" ind2=" " ind1=" ">
      <subfield code="a">Àrees temàtiques de la UPC::Matemàtiques i estadística::Anàlisi numèrica::Mètodes en elements finits</subfield>
   </datafield>
   <datafield tag="653" ind2=" " ind1=" ">
      <subfield code="a">Finite element method</subfield>
   </datafield>
   <datafield tag="653" ind2=" " ind1=" ">
      <subfield code="a">Marine engineering</subfield>
   </datafield>
   <datafield tag="653" ind2=" " ind1=" ">
      <subfield code="a">Propeller  Optimization,  Shape  Parameterization,  Parameter  Space  Reduction,  Active Subspaces</subfield>
   </datafield>
   <datafield tag="653" ind2=" " ind1=" ">
      <subfield code="a">Enginyeria naval</subfield>
   </datafield>
   <datafield ind2="0" ind1="0" tag="245">
      <subfield code="a">Efficient reduction in shape parameter space dimension for ship propeller blade design</subfield>
   </datafield>
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