Summary of Work - The LAVA flow solver is utilized to investigate the design trade space of the SUSAN Electrofan concept’s Propulsion-Airframe Integration (PAI) systems, which include the effects of aero-propulsive coupling and boundary-layer ingestion (BLI). - Simplified infinite wing models are used to study various distributed electric propulsion (DEP) system arrangements, such as over-wing, under-wing, and trailing-edge configurations.


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    Title :

    High-Fidelity Aerodynamic Analysis and Optimization of the SUSAN Electrofan Concept


    Contributors:

    Conference:

    AIAA Aviation Forum ; 2022 ; Chicago, IL, US


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English




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