Novel fan configuration for distributed propulsion systems with boundary layer ingestion on an hybrid wing body airframe

Article

Abstract: The performance benefits of directly ingesting the boundary layer (BLI) on air vehicles with distrib

Palabras claves:

conceptual design, Discretized Miller approach, Distortion tolerant fan, Rectilinear fan, Turboelectric distributed propulsion

Autores:

Darío A. Rodríguez, Esteban Valencia, Laskaridis P., Roumeliotis I., Víctor H. Alulema

Fuentes:

scopus