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   <dc:title>Simulation of butterfly flapping with the method of dipole domains</dc:title>
   <dc:creator>Dynnikova, Galina Ya.</dc:creator>
   <dc:creator>Guvernyuk, Sergey V.</dc:creator>
   <dc:creator>Syrovatskiy, Dmitry A.</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>Computational methods in mechanics</dc:subject>
   <dc:subject>Particle methods (Numerical analysis)</dc:subject>
   <dc:subject>Mesh-free numerical method, three dimensional flow, dipole particles, butterfly model, mechanism of the thrust performance</dc:subject>
   <dc:subject>Elements finits, Mètode dels</dc:subject>
   <dc:description>A numerical mesh-free method of dipole domains [1,2] is used for simulation of a butterfly flapping model. This method is based on the representation of a vortex field by the set of dipole particles. The vector function D describes density of dipole moments in accordanse with Navier-Stokes or Euler equations [3]. The butterfly model consists of two flat plates with a common edge performing harmonic oscillations in two planes. New mechanism of the thrust performing is proposed.</dc:description>
   <dc:date>2019</dc:date>
   <dc:type>Conference report</dc:type>
   <dc:identifier>978-84-121101-1-1</dc:identifier>
   <dc:identifier>https://hdl.handle.net/2117/186482</dc:identifier>
   <dc:language>eng</dc:language>
   <dc:rights>Open Access</dc:rights>
   <dc:format>6 p.</dc:format>
   <dc:format>application/pdf</dc:format>
   <dc:publisher>CIMNE</dc:publisher>
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