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Numerical study of a Boundary Layer Ingesting Propulsion system
Berengué Llonch, Oleguer
Benard, E.; Blanc, F.; Bourdeau, C.
For several years, Airbus has been working with the ONERA in a project called RAPRO aiming to study the in uence that a boundary layer created by an axisymmetric body placed upstream has in the global performances of an engine ingesting this boundary layer. The existing numerical simulations, made during RAPRO's project, shown a decrease of power requirements for a given con guration but this simulations o er no access to the aerodynamic e ects occurring on the engine. The present work presents a numerical study of the aerodynamics of RAPRO's boundary layer ingesting system (BLI). The study will be mostly focused on the setup of a novel CFD model and also on the fan's performances when it encounters a non-uniform ow, with the existence of a boundary layer, created by an object placed upstream.
Àrees temàtiques de la UPC::Aeronàutica i espai::Aerodinàmica
Àrees temàtiques de la UPC::Física::Física de fluids::Flux de fluids
Aerodynamics
Propulsion systems
Aeronautics
Boundary layer
Computational fluid dynamics
Aerodinàmica
Sistemes de propulsió
Aeronàutica
Capa límit (Dinàmica de fluids)
Dinàmica de fluids -- Simulació per ordinador
Attribution-NonCommercial-NoDerivs 3.0 Spain
http://creativecommons.org/licenses/by-nc-nd/3.0/es/
info:eu-repo/semantics/bachelorThesis
Universitat Politècnica de Catalunya
         

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