elib
DLR-Header
DLR-Logo -> http://www.dlr.de
DLR Portal Home | Imprint | Privacy Policy | Accessibility | Contact | Deutsch
Fontsize: [-] Text [+]

Aerodynamic Investigation of Propulsion Integration for a Low Noise Hybrid Wing-Body with Podded UHBR Turbo Fan Engines

Keller, Dennis (2024) Aerodynamic Investigation of Propulsion Integration for a Low Noise Hybrid Wing-Body with Podded UHBR Turbo Fan Engines. Journal of Physics: Conference Series, 2716. Institute of Physics (IOP) Publishing. doi: 10.1088/1742-6596/2716/1/012008. ISSN 1742-6588.

Full text not available from this repository.

Official URL: https://iopscience.iop.org/article/10.1088/1742-6596/2716/1/012008

Abstract

The presented work examines the aerodynamic challenges of podded ultra high-bypass engines installed on a short/mid range low noise hybrid wing body configuration. After assessing the initial engine integration design, sensitivity studies regarding the impact of the freestream Mach number, engine position, and the engine incidence angle on the interference drag are discussed. Then, shape modifications of the nacelle and the center-body based on 2D RANS optimizations are presented. The results indicate that in order to reduce the initially massive interference drag, the overall aircraft design either has to allow for a modified engine position or for reshaping of the center-body's upper surface. With the latter, an overall drag reduction of -44 % was achieved.

Item URL in elib:https://elib.dlr.de/209493/
Document Type:Article
Title:Aerodynamic Investigation of Propulsion Integration for a Low Noise Hybrid Wing-Body with Podded UHBR Turbo Fan Engines
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Keller, DennisDennis.Keller (at) dlr.dehttps://orcid.org/0000-0002-1471-9433UNSPECIFIED
Date:2024
Journal or Publication Title:Journal of Physics: Conference Series
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:Yes
In ISI Web of Science:No
Volume:2716
DOI:10.1088/1742-6596/2716/1/012008
Editors:
EditorsEmailEditor's ORCID iDORCID Put Code
UNSPECIFIEDInstitute of Physics (IOP) PublishingUNSPECIFIEDUNSPECIFIED
Publisher:Institute of Physics (IOP) Publishing
Series Name:13th EASN International Conference on: Innovation in Aviation & Space for opening New Horizons 05/09/2023 - 08/09/2023 Salerno, Italy
ISSN:1742-6588
Status:Published
Keywords:Applied Aerodynamics, Computational Fluid Dynamics, Engine Integration, Blended Wing Body, Hybrid Wing Body, UHBR, RANS
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:Efficient Vehicle
DLR - Research area:Aeronautics
DLR - Program:L EV - Efficient Vehicle
DLR - Research theme (Project):L - Aircraft Technologies and Integration
Location: Braunschweig
Institutes and Institutions:Institute for Aerodynamics and Flow Technology > Transport Aircraft
Deposited By: Keller, Dennis
Deposited On:06 Dec 2024 10:30
Last Modified:13 Oct 2025 10:08

Repository Staff Only: item control page

Browse
Search
Help & Contact
Information
OpenAIRE Validator logo electronic library is running on EPrints
Website and database design: Copyright © German Aerospace Center (DLR). All rights reserved.