The environmental concern on the impact of civil air transportation has become a primary driving force for the research and development towards new technologies that could provide a reduction in the emissions. In the context of civil aircraft transportation, Boundary Layer Ingestion (BLI) is among the most promising solutions. Such architecture is characterized by a high level of integration between the airframe and propulsors, making the design process becomes a major challenge. The present work deals with a complete CFD based design and optimization of a propulsive fuselage concept, both in terms of airframe shape and fan design.

Fullscale Optimization and Fan Design of a Rear BLI Shrouded Propulsor

Magrini A.;Benini E.
2023

Abstract

The environmental concern on the impact of civil air transportation has become a primary driving force for the research and development towards new technologies that could provide a reduction in the emissions. In the context of civil aircraft transportation, Boundary Layer Ingestion (BLI) is among the most promising solutions. Such architecture is characterized by a high level of integration between the airframe and propulsors, making the design process becomes a major challenge. The present work deals with a complete CFD based design and optimization of a propulsive fuselage concept, both in terms of airframe shape and fan design.
2023
AIAA SciTech Forum and Exposition, 2023
AIAA SciTech Forum and Exposition, 2023
   Supporting Understanding of Boundary Layer Ingesting Model Experiment
   SUBLIME
   European Commission
   Horizon 2020 Framework Programme
   864803
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Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/11577/3535563
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