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

Disciplinary Sub-Processes to Assess Low-Speed Performance and Noise Characteristics within an Aircraft Design Environment

Fröhler, Benjamin and Hesse, Christian and Atanasov, Georgi and Wassink, Philip (2020) Disciplinary Sub-Processes to Assess Low-Speed Performance and Noise Characteristics within an Aircraft Design Environment. Deutscher Luft- und Raumfahrtkongress 2020, 01.-03.09.2020, Online. (In Press)

Full text not available from this repository.

Abstract

The overall aircraft assessment is based on a wide range of disciplinary methodologies. In addition, a consistent aircraft design must be provided for the beginning of the aircraft design process. For this purpose, the DLR in-house conceptual aircraft design tool openAD has been developed for initialization and subsequent synthesis of results with higher fidelity. Within the aircraft design process, three disciplinary methods are introduced to improve the quality and accuracy of the performed design studies. These methods include engine performance, low speed performance and acoustics characteristics of an aircraft, which allows the predictions of the aircraft performance and noise level during the take-off and landing phase. The engine performance calculation is based on a thermodynamic cycle model and is an extension in openAD. Subsequently, the aircraft and engine performance are fed into the low speed performance tool LSperfo, which estimates the take-off and landing trajectory including the thrust requirements, flight path and aerodynamic forces. The aircraft and engine data are further passed to a noise tool, which predicts the aircraft model noise emission at relevant aircraft certification points. To demonstrate the result validity of the aircraft design environment and its disciplinary tools, a DLR interpretation of a turboprop engine aircraft (ATR 72 similar) is used. Since the tools are based on simple physical models, a proper calibration on appropriate reference aircraft needs be ensured for most overall aircraft design studies. Nevertheless, the results show a good estimation for take-off and landing field length as well as the noise level of the reference cases provided in this paper.

Item URL in elib:https://elib.dlr.de/140229/
Document Type:Conference or Workshop Item (Speech)
Title:Disciplinary Sub-Processes to Assess Low-Speed Performance and Noise Characteristics within an Aircraft Design Environment
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iD
Fröhler, BenjaminBenjamin.Froehler (at) dlr.deUNSPECIFIED
Hesse, ChristianChristian.Hesse (at) dlr.deUNSPECIFIED
Atanasov, GeorgiGeorgi.Atanasov (at) dlr.deUNSPECIFIED
Wassink, PhilipPhilip.Wassink (at) dlr.deUNSPECIFIED
Date:September 2020
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:In Press
Keywords:Conceptual aircraft design, multidisciplinary design and analysis, low speed performance, Aircraft noise prediction
Event Title:Deutscher Luft- und Raumfahrtkongress 2020
Event Location:Online
Event Type:national Conference
Event Dates:01.-03.09.2020
Organizer:Deutsche Gesellschaft für Luft- und Raumfahrt - Lilienthal-Oberth e.V.
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:fixed-wing aircraft
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Concepts and Integration (old)
Location: Hamburg
Institutes and Institutions:Institute of System Architectures in Aeronautics > Aircraft Design and System Integration
Deposited By: Fröhler, Benjamin
Deposited On:12 Jan 2021 13:23
Last Modified:12 Jan 2021 13:23

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.