Results 11 to 20 of about 1,520 (247)

Boundary Layer Ingestion Propulsion: A Review on Numerical Modeling [PDF]

open access: yesJournal of Engineering for Gas Turbines and Power, 2020
The present paper focuses on the numerical modeling approaches adopted in boundary layer ingestion (BLI) studies. Three driving aircraft concepts have been identified, namely propulsive fuselage concept (PFC), rear engines concept (REC), and ...
Luca Menegozzo   +2 more
exaly   +3 more sources

Parameter Sensitivity Study on Inflow Distortion of Boundary Layer Ingested Turbofans [PDF]

open access: yesAerospace, 2022
The inflow distortion to the fan introduced by the ingestion of the fuselage boundary layer is the most critical challenge in realizing the benefits of boundary later ingesting (BLI) concepts.
Xin Zhao   +3 more
doaj   +2 more sources

Optimizing the Landing Stability of Blended-Wing-Body Aircraft with Distributed Electric Boundary-Layer Ingestion Propulsors through a Novel Thrust Control Configuration

open access: yesApplied Sciences
The imperative for energy conservation and environmental protection has led to the development of innovative aircraft designs. This study explored a novel thrust control configuration for blended-wing-body (BWB) aircraft with distributed electric ...
Mingxing Yu   +3 more
doaj   +2 more sources

Unsteady loss mechanisms in a boundary layer ingestion fan under inlet distortion

open access: yesFlow
Boundary layer ingestion (BLI) propulsion can improve aircraft aerodynamic efficiency, but also introduces inlet distortion that affects fan flow and stability.
Junyang Yu   +4 more
doaj   +2 more sources

Numerical analysis of fan noise for the NOVA boundary-layer ingestion configuration

open access: yesAerospace Science and Technology, 2020
Aim of this paper is to investigate the effects of the turbulent flow developing over a fuselage on fan noise for BLI embedded propulsion systems. Such configurations can suffer from inlet flow distortions and ingestion of turbulence at the fan plane ...
Gianluca Romani   +2 more
exaly   +2 more sources

Investigation of the effects of boundary layer ingestion engine integration on aircraft thrust requirement [PDF]

open access: yesCEAS Aeronautical Journal
In order to further the understanding of boundary layer ingestion (BLI) engine integration concepts the DLR project AGATA3S aimed at modelling and evaluating the inhomogeneous inflow into turbofans positioned on either side of the rear fuselage.
A. Vinz, A. Raichle
semanticscholar   +2 more sources

Development of a Multi-Segment Parallel Compressor Model for a Boundary Layer Ingesting Fuselage Fan Stage

open access: yesEnergies, 2021
The present methodological study aims to assess boundary layer ingestion (BLI) as a promising method to improve propulsion efficiency. BLI utilizes the low momentum inflow of the wing or fuselage boundary layer for thrust generation in order to minimize ...
Jonas Voigt, Jens Friedrichs
doaj   +1 more source

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

open access: yesAerospace, 2023
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 ...
Tze Sing Tse, Cesare A. Hall
doaj   +1 more source

Aeroacoustics Assessment of an Hybrid Aircraft Configuration with Rear-Mounted Boundary Layer Ingested Engine

open access: yesApplied Sciences, 2021
Hybrid electric propulsion is a promising solution to reduce aircraft emissions, thus improving the sustainability of the air transport. In this work, a hybrid aircraft configuration with a rear-mounted boundary layer ingestion (BLI) engine has been ...
Francesco Petrosino   +2 more
doaj   +1 more source

Numerical Simulation of Boundary Layer Ingesting (BLI) Inlet/Fan Interaction [PDF]

open access: yes50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, 2014
Future civil transport designs may incorporate engine inlets integrated into the body of the aircraft to take advantage of efficiency increases due to weight and drag reduction. Additional increases in engine efficiency are predicted if the inlet ingests the lower momentum boundary layer flow.
James E. Giuliani   +3 more
openaire   +1 more source

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