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<feed xmlns="http://www.w3.org/2005/Atom" xml:lang="en"><id>http://publicationslist.org/data/j.c.pascoa/atom.xml</id><title>José Páscoa's Publications List</title>
<link rel="self" type="application/atom+xml" href="http://publicationslist.org/data/j.c.pascoa/atom.xml"/><link rel="alternate" type="text/html" href="http://publicationslist.org/j.c.pascoa"/><author><name>José Páscoa</name><uri>http://publicationslist.org/j.c.pascoa</uri></author><icon>$basepathfavicon.ico</icon><subtitle>Recent additions to José Páscoa's PublicationsList.org page</subtitle><logo>http://publicationslist.org/publications.png</logo><updated>2011-03-04T15:31:55Z</updated>

<entry>
<id>http://publicationslist.org/j.c.pascoa/refid1</id>
<updated>2011-03-04T12:17:56Z</updated>
<link rel='alternate' type='text/html' href='http://publicationslist.org/j.c.pascoa#refid1'/>
<title type='html'>Accuracy details in realistic CFD modeling of an industrial centrifugal pump in direct and reverse modes</title>
<summary type='html'>Numerical computation of the flowfield inside a pump is herein used as a numerical laboratory, subject to the
limitations of modeling assumptions and to experimental verification. A numerical computation of the flow inside
a real industrial centrifugal pump is performed that includes a very sophisticated geometry. Conversely to other
computations, in this test case no simplification of the geom...&lt;br/&gt;&lt;br/&gt;Páscoa J. C., Silva F. J., Pinheiro J. S., Martins D. J. (2010)  &lt;i&gt;Journal of Thermal Science&lt;/i&gt; 19: 6 1-9&lt;br/&gt;</summary>
</entry>
<entry>
<id>http://publicationslist.org/j.c.pascoa/refid2</id>
<updated>2011-03-04T12:18:17Z</updated>
<link rel='alternate' type='text/html' href='http://publicationslist.org/j.c.pascoa#refid2'/>
<title type='html'>Performance assessment limits in transonic 3D turbine stage blade rows using a mixing-plane approach</title>
<summary type='html'>3D computations for a highly loaded transonic blade and for a gas turbine stage. Comparison between experimental results and numerical
computations reveals the precision limits of current modeling assumptions. Computations are performed using a time-marching
approach coupled with a mixing-plane model for the exchange of flowfields between stator and rotor domains. Eddy viscosity turbulence
mode...&lt;br/&gt;&lt;br/&gt;Páscoa J. C., Xisto C. M., Göttlich E. (2010)  &lt;i&gt;Journal of Mechanical Science and Technology&lt;/i&gt; 24: 10 2035-2042&lt;br/&gt;</summary>
</entry>
<entry>
<id>http://publicationslist.org/j.c.pascoa/refid3</id>
<updated>2011-03-04T12:18:37Z</updated>
<link rel='alternate' type='text/html' href='http://publicationslist.org/j.c.pascoa#refid3'/>
<title type='html'>A fast iterative inverse method for turbomachinery blade design</title>
<summary type='html'>An improved formulation for an iterative inverse design method is presented. The method
solves the time dependent Euler equations in a numerical domain where the blade sections
are iteratively modified, until a prescribed blade load distribution is reached. The mean
tangential velocity and thickness distributions are imposed as design variables. Each design
iteration starts with a blade sectio...&lt;br/&gt;&lt;br/&gt;Páscoa J. C., Mendes A. C., Gato L.M.C. (2009)  &lt;i&gt;Mechanics Research Communications&lt;/i&gt; 36: 5 537-546&lt;br/&gt;</summary>
</entry>
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