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Modelos de orden reducido para la predicción de coeficientes aerodinámicos de RPAS con propulsión eléctrica distribuida e ingestión de capa límite





[EN] Distributed electric propulsion (DEP) with boundary layer ingestion (BLI) is a very attractive technological solution to reduce the energy consumption of future aircraft, including remotely piloted small aircraft systems (RPAS). The strong interaction between the aerodynamic behavior of the wing and that of the propulsive propellers when implementing DEP and BLI on the wing of an RPAS complicates the design and study of the RPAS. This work applies model order reduction methods to computational results to simplify the problem and to be able to predict aerodynamic coefficients in different flight conditions of an RPAS TFGM

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