Results 11 to 20 of about 2,626,634 (290)

Turboelectric Distributed Propulsion System Modelling [PDF]

open access: yes, 2013
The Blended-Wing-Body is a conceptual aircraft design with rear-mounted, over wing engines. Turboelectric distributed propulsion system with boundary layer ingestion has been considered for this aircraft.
Liu, Chengyuan
core   +7 more sources

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

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

Energy-Based Aerodynamic Analysis on the Blended-Wing-Body Aircraft with Boundary Layer Ingestion

open access: yesInternational Journal of Aerospace Engineering, 2022
This study is aimed at evaluating the energy saving benefit and its limitation of the boundary layer ingestion (BLI) applied to a transonic blended-wing-body (BWB) aircraft.
Wenyuan Zhao, Yanlai Zhang, Jianghao Wu
doaj   +1 more source

Boundary-Layer-Ingesting Inlet Flow Control [PDF]

open access: yes44th AIAA Aerospace Sciences Meeting and Exhibit, 2006
An experimental study was conducted to provide the first demonstration of an active flow control system for a flush-mounted inlet with significant boundary-layer ingestion in transonic flow conditions. The effectiveness of the flow control in reducing the circumferential distortion at the engine fan-face location was assessed using a 2.5% -scale model ...
Lewis R. Owens   +2 more
openaire   +3 more sources

Improvement of the Parallel Compressor Model and Application to Inlet Flow Distortion

open access: yesInternational Journal of Turbomachinery, Propulsion and Power, 2021
This paper introduces a semi-analytical approach which enables one to deal with distorted inflow in axial fans or compressors. It is inspired by the classical parallel compressor (PC) theory but relies on a local flow-loading coefficient formalism. It is
Emmanuel Benichou   +3 more
doaj   +1 more source

Non-Axisymmetric Stator Design for Boundary Layer Ingesting Fans [PDF]

open access: yesVolume 1: Aircraft Engine; Fans and Blowers; Marine; Honors and Awards, 2017
In a Boundary Layer Ingesting (BLI) fan system the inlet flow field is highly non-uniform. In this environment, an axisymmetric stator design suffers from a non-uniform distribution of hub separations, increased wake thicknesses and casing losses. These additional loss sources can be reduced using a non-axisymmetric design that is tuned to the radial ...
Hall, Cesare, Gunn, Ewan
openaire   +2 more sources

Aerodynamic Shape Optimization of an Aircraft Propulsor Air Intake with Boundary Layer Ingestion

open access: yesApplied Mechanics, 2022
The growth of the airline industry has highlighted the need for more environmentally conscious aviation, leading to the conceptualization of more fuel-efficient aircraft.
Ayesh Sudasinghe   +4 more
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

Design and Optimization of a Boundary Layer Ingesting Propulsor

open access: yesVolume 2A: Turbomachinery, 2020
Abstract The boundary layer ingestion concept has the potential to improve propulsion efficiency that will lead to better fuel economy of commercial aircraft. This design concept has been explored by NASA as the Single-aisle Turboelectric Aircraft with Aft Boundary-Layer propulsor “STARC-ABL.” This paper discusses the 1D-3D aerodynamic ...
Mark Turner   +3 more
openaire   +2 more sources

Home - About - Disclaimer - Privacy