Memorias de investigación
Patents:
Computer aided-method for a quick prediction of vortex trajectories on aircraft components checking high pressure gradients and high drag friction components
Year:2016

Research Areas
  • Computacional fluid dynamics,
  • Aerodynamics,
  • Aircraft external noise

Information
Abstract
The present invention refers to a method to assist in the design of components with parts moving relative to a flow, particularly Counter Rotating Open Rotor (CROR) engines installed in aircraft, in their endeavour to reduce noise levels, drag, vibrations, and fatigue loads, due to vortex-surface interaction.
International
Si
Status
Solicitada
application number
EPO Patent Application No. 16382604.3 - 1954
under exploitation
No
Licensee/s
Date
15/12/2016
Owner
Airbus Operations
Participants
  • Autor: Nuno Filipe Da Costa Vinha . UPM
  • Autor: David Vallespin Airbus Operations
  • Autor: Eusebio Valero Sanchez UPM
  • Autor: Valentin de Pablo Airbus Operations

Research Group, Departaments and Institutes related
  • Creador: Centro o Instituto I+D+i: Centro de Investigación en Simulación Computacional
  • Departamento: Matemática Aplicada a la Ingeniería Aeroespacial