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

Petrosino, Francesco and Barbarino, Mattia and Staggat, Martin (2021) Aeroacoustics Assessment of an Hybrid Aircraft Configuration with Rear-Mounted Boundary Layer Ingested Engine. Applied Sciences, 11 (7). Multidisciplinary Digital Publishing Institute (MDPI). doi: 10.3390/app11072936. ISSN 2076-3417.

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Official URL: https://www.mdpi.com/2076-3417/11/7/2936

Abstract

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 investigated. The partial embedding of the engine into the fuselage generates a distortion of the ingested inflow causing additional tonal and broadband BLI noise sources, and, at the same time, alters the existing one, such as the rotor–stator interaction noise (RSI). This work is focused on the tonal RSI noise modeling, with and without the distortion generated by the BLI, and the far-field propagation including the acoustic masking contribution due to the engine–fuselage integration. As the main result, this work shows the contributions of BLI and the engine–aircraft integration on the RSI noise. Both effects should be properly taken into account in the early aircraft design stage for an effective noise reduction even at ground level.

Item URL in elib:https://elib.dlr.de/141535/
Document Type:Article
Title:Aeroacoustics Assessment of an Hybrid Aircraft Configuration with Rear-Mounted Boundary Layer Ingested Engine
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Petrosino, FrancescoUNSPECIFIEDhttps://orcid.org/0000-0002-7454-425XUNSPECIFIED
Barbarino, MattiaUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Staggat, MartinUNSPECIFIEDhttps://orcid.org/0000-0003-4380-0828133662762
Date:25 March 2021
Journal or Publication Title:Applied Sciences
Refereed publication:Yes
Open Access:Yes
Gold Open Access:Yes
In SCOPUS:Yes
In ISI Web of Science:Yes
Volume:11
DOI:10.3390/app11072936
Publisher:Multidisciplinary Digital Publishing Institute (MDPI)
Series Name:Applied Sciences
ISSN:2076-3417
Status:Published
Keywords:aeroacoustics, boundary layer ingestion, acoustic scattering, engine noise
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:Clean Propulsion
DLR - Research area:Aeronautics
DLR - Program:L CP - Clean Propulsion
DLR - Research theme (Project):L - Future Engines and Engine Integration, L - Virtual Engine
Location: Berlin-Charlottenburg
Institutes and Institutions:Institute of Propulsion Technology > Engine Acoustic
Deposited By: Staggat, Martin
Deposited On:12 Apr 2021 10:59
Last Modified:24 Apr 2023 13:53

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