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Turbo-Electric BLI Aircraft Design Insights by pRoBoTRoGe OP is a document available to read on EtoBox.

This document presents an analytical method for estimating the fuel burn reduction benefits of boundary layer ingestion (BLI) for turbo-electric propulsive fuselage aircraft. The method uses a power balance approach to compare the mechanical power required by conventional propulsors versus BLI propulsors. The method is applied to explore the design space of a short-to-medium range tube-and-wing aircraft with a partial turbo-electric propulsion system featuring fuselage BLI. The analysis identifies key param

Author

pRoBoTRoGe OP

Language

EN