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Advanced Modeling of Air- and Rotorcraft in a Multi-Disciplinary Environment at Early Design Stages

Schwinn, Dominik (2015) Advanced Modeling of Air- and Rotorcraft in a Multi-Disciplinary Environment at Early Design Stages. In: Summary of Proceedings. NAFEMS World Congress 2015, 2015-06-21 - 2015-06-24, San Diego, CA, USA. ISBN 978-1-910643-24-2.

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Kurzfassung

The development of new air- and rotorcraft is very challenging. The design process is divided into three consecutive phases: Conceptual, preliminary and detailed design phase which combine various disciplines featuring different objectives, e.g. static versus crashworthy design. This paper focuses on the preliminary design stage. The aim of the presented work is a significant reduction of the time spent on model generation in a multi-disciplinary design environment. Moreover, automation is desired to couple different disciplines respectively tools, hence, reducing the error probability compared to manual processing. In the preliminary design phase a basic aircraft configuration which has been developed during the conceptual design serves to conduct trade studies. Objective of this stage is to enhance this basic aircraft configuration establishing an appropriate design that meets customer requirements including performance, weight, producibility and cost. This phase is of particular interest since the basic layout of the primary structure is defined here. Up to date, semi-analytical methods are commonly deployed during preliminary design. Though these methods lead to adequate results for major structural components, the evaluation of new aircraft configurations is still very challenging. One philosophy to improve preliminary design is to introduce the use of Finite Element Methods (FEM) at this early design stage benefitting from the constantly increasing computational power. To efficiently use FEM, fast and easy model generation methods are required. These methods also need to have the ability to cope with the generation of alternative design concepts (e.g. blended wing body, compound helicopter). In order to accelerate and simplify these modeling processes, the standardized data format CPACS (Common Parameterized Aircraft Configuration Schema) is used in combination with automated modeling tools. In this paper fully parameterized and automated process chains for the generation and analyses of air- and rotorcraft fuselage structures will be presented. The tools used within these processes will be introduced and basic applications will be shown to demonstrate the versatility, effectivity and the gain in efficiency. Applications range from initial distribution of primary structure over static analysis to evaluation of crashworthiness.

elib-URL des Eintrags:https://elib.dlr.de/97158/
Dokumentart:Konferenzbeitrag (Vortrag)
Titel:Advanced Modeling of Air- and Rotorcraft in a Multi-Disciplinary Environment at Early Design Stages
Autoren:
AutorenInstitution oder E-Mail-AdresseAutoren-ORCID-iDORCID Put Code
Schwinn, Dominikdominik.schwinn (at) dlr.dehttps://orcid.org/0000-0003-2341-9632NICHT SPEZIFIZIERT
Datum:Juni 2015
Erschienen in:Summary of Proceedings
Referierte Publikation:Ja
Open Access:Ja
Gold Open Access:Nein
In SCOPUS:Nein
In ISI Web of Science:Nein
ISBN:978-1-910643-24-2
Status:veröffentlicht
Stichwörter:aircraft design, parameterized modeling, fuselage design, crashworthiness
Veranstaltungstitel:NAFEMS World Congress 2015
Veranstaltungsort:San Diego, CA, USA
Veranstaltungsart:internationale Konferenz
Veranstaltungsbeginn:21 Juni 2015
Veranstaltungsende:24 Juni 2015
Veranstalter :NAFEMS Ltd.
HGF - Forschungsbereich:Luftfahrt, Raumfahrt und Verkehr
HGF - Programm:Luftfahrt
HGF - Programmthema:Flugzeuge
DLR - Schwerpunkt:Luftfahrt
DLR - Forschungsgebiet:L AR - Aircraft Research
DLR - Teilgebiet (Projekt, Vorhaben):L - Strukturen und Werkstoffe (alt)
Standort: Stuttgart
Institute & Einrichtungen:Institut für Bauweisen und Strukturtechnologie > Strukturelle Integrität
Hinterlegt von: Schwinn, Dominik
Hinterlegt am:19 Nov 2015 10:12
Letzte Änderung:24 Apr 2024 20:02

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