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               <dc:title>Multicom onent design of rotor-stator-nozzle (RSN) propulsor on azipods</dc:title>
               <dc:creator>Marinich, Nikolai V.</dc:creator>
               <dc:creator>Yakolev, Aleksey Yu.</dc:creator>
               <dc:creator>Ovchinnikov, Nikolay A.</dc:creator>
               <dc:creator>Veikonnheimo, Tomi</dc:creator>
               <dc:subject>Àrees temàtiques de la UPC::Matemàtiques i estadística::Anàlisi numèrica::Mètodes en elements finits</dc:subject>
               <dc:subject>Finite element method</dc:subject>
               <dc:subject>Marine engineering</dc:subject>
               <dc:subject>Nozzled rotor, Post-swirl stator, Computational Methods, Design, Optimization,  CFD calculation, Experiment</dc:subject>
               <dc:subject>Enginyeria naval</dc:subject>
               <dc:description>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.</dc:description>
               <dc:date>2017</dc:date>
               <dc:type>Conference report</dc:type>
               <dc:rights>Open Access</dc:rights>
               <dc:publisher>CIMNE</dc:publisher>
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