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

Parametric Modeling of a Long-Range Aircraft under Consideration of Engine-Wing Integration

Schulze, Matthias and Neumann, Jens and Klimmek, Thomas (2020) Parametric Modeling of a Long-Range Aircraft under Consideration of Engine-Wing Integration. Aerospace, 8 (1), pp. 1-20. Multidisciplinary Digital Publishing Institute (MDPI). doi: 10.3390/aerospace8010002. ISSN 2226-4310.

[img] PDF - Published version
9MB

Official URL: https://www.mdpi.com/2226-4310/8/1/2

Abstract

The purpose of this paper is to investigate the influence of the engine position and mass as well as the pylon stiffness on the aeroelastic stability of a long-range wide-body transport aircraft. As reference configuration, DLR's (German Aerospace Center/Deutsches Zentrum für Luft und Raumfahrt) generic aircraft configuration DLR-D250 is taken. The structural, mass, loads, and optimization models for the reference and a modified configuration with different engine and pylon parameters are set up using DLR's automatized aeroelastic design process cpacs-MONA. At first, the cpacs-MONA process with its capabilities for parametric modeling of the complete aircraft and in particular the set-up of a generic elastic pylon model is unfolded. Then, the influence of the modified engine-wing parameters on the flight loads of the main wing is examined. The resulting loads are afterward used to structurally optimize the two configurations component wise. Finally, the results of post-cpacs-MONA flutter analyses performed for the two optimized aircraft configurations with the different engine and pylon characteristics are discussed. It is shown that the higher mass and the changed position of the engine slightly increased the flutter speed. Although the lowest flutter speeds for both configurations occur at a flutter phenomenon of the horizontal tail-plane outside of the aeroelastic stability envelope.

Item URL in elib:https://elib.dlr.de/140161/
Document Type:Article
Title:Parametric Modeling of a Long-Range Aircraft under Consideration of Engine-Wing Integration
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iD
Schulze, MatthiasMatthias.Schulze (at) dlr.dehttps://orcid.org/0000-0001-7172-7723
Neumann, JensJens.Neumann (at) dlr.deUNSPECIFIED
Klimmek, ThomasThomas.Klimmek (at) dlr.dehttps://orcid.org/0000-0002-5573-7355
Date:23 December 2020
Journal or Publication Title:Aerospace
Refereed publication:Yes
Open Access:Yes
Gold Open Access:Yes
In SCOPUS:Yes
In ISI Web of Science:Yes
Volume:8
DOI :10.3390/aerospace8010002
Page Range:pp. 1-20
Editors:
EditorsEmailEditor's ORCID iD
Cestino, Enricoenrico.cestino@polito.itUNSPECIFIED
Publisher:Multidisciplinary Digital Publishing Institute (MDPI)
Series Name:Special Issue "Aeroelasticity, Volume II"
ISSN:2226-4310
Status:Published
Keywords:cpacs-MONA, aeroelastic design, parametric modeling, complete aircraft, elastic pylon, engine-wing integration, aeroelastic stability, tail-flutter
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 - Virtual Aircraft and  Validation
Location: Göttingen
Institutes and Institutions:Institute of Aeroelasticity > Loads Analysis and Aeroelastic Design
Institute of Aeroelasticity > Aeroelastic Simulation
Deposited By: Schulze, Matthias
Deposited On:11 Oct 2021 09:53
Last Modified:15 Oct 2021 10:17

Repository Staff Only: item control page

Browse
Search
Help & Contact
Information
electronic library is running on EPrints 3.3.12
Copyright © 2008-2017 German Aerospace Center (DLR). All rights reserved.