Aerodynamics and Power Balance of a Distributed Aft-Fuselage Boundary Layer Ingesting Aircraft

This paper presents a first investigation into the aerodynamics and performance breakdown of a distributed aft-fuselage boundary layer ingesting (BLI) tube-and-wing aircraft using fully coupled Unsteady Reynolds-Averaged Navier-Stokes (URANS) calculations that resolve the complete fan and installati...

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Bibliographic Details
Main Authors: Tze Sing Tse, Cesare A. Hall
Format: Article
Language:English
Published: MDPI AG 2023-01-01
Series:Aerospace
Subjects:
Online Access:https://www.mdpi.com/2226-4310/10/2/122