<?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>2026-04-17T03:29:06Z</responseDate><request verb="GetRecord" identifier="oai:www.recercat.cat:2117/331899" metadataPrefix="marc">https://recercat.cat/oai/request</request><GetRecord><record><header><identifier>oai:recercat.cat:2117/331899</identifier><datestamp>2026-02-07T01:13:53Z</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">Marinich, Nikolai V.</subfield>
      <subfield code="e">author</subfield>
   </datafield>
   <datafield ind2=" " ind1=" " tag="720">
      <subfield code="a">Yakolev, Aleksey Yu.</subfield>
      <subfield code="e">author</subfield>
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   <datafield ind2=" " ind1=" " tag="720">
      <subfield code="a">Ovchinnikov, Nikolay A.</subfield>
      <subfield code="e">author</subfield>
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      <subfield code="a">Veikonnheimo, Tomi</subfield>
      <subfield code="e">author</subfield>
   </datafield>
   <datafield ind2=" " ind1=" " tag="260">
      <subfield code="c">2017</subfield>
   </datafield>
   <datafield ind2=" " ind1=" " tag="520">
      <subfield code="a">The paper  offers  design  computation  method  of  RSN  propulsor  fitted  with  post-&#xd;
&#xd;
swirl  stator  on  AZIPODs.  The  method  implemented  as  problem  solution  of  non-linear &#xd;
optimization of objective functional with restrictions over the field of infinitely dimensional &#xd;
values (functions being sought for). Numerical solution of this problem is reduced to the finite &#xd;
dimensional problem The shape of internal and external nozzle surface, distribution of pitch, &#xd;
camber,  width  and  thickness  of  rotor  blades  and  post-swirl  stator  geometry  at  radius  &#xd;
are unknown functions of RSN propulsor design. Computational accuracy was validated through &#xd;
CFD-aided calculation of designed propulsors. Comparative analysis with model test results was  &#xd;
implemented  as  well.  The  AZIPOD  XL  propulsor  concept  has  been  developed  by  the&#xd;
&#xd;
present method.</subfield>
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   <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">Nozzled rotor, Post-swirl stator, Computational Methods, Design, Optimization,  CFD calculation, Experiment</subfield>
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   <datafield tag="653" ind2=" " ind1=" ">
      <subfield code="a">Enginyeria naval</subfield>
   </datafield>
   <datafield ind2="0" ind1="0" tag="245">
      <subfield code="a">Multicom onent design of rotor-stator-nozzle (RSN) propulsor on azipods</subfield>
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