elib
DLR-Header
DLR-Logo -> http://www.dlr.de
DLR Portal Home | Impressum | Datenschutz | Kontakt | English
Schriftgröße: [-] Text [+]

New approaches in CPACS-based preliminary design of aircraft fuselage structures using Python

Walther, Jan-Niclas und Petsch, Michael und Kohlgrüber, Dieter (2016) New approaches in CPACS-based preliminary design of aircraft fuselage structures using Python. 6th EASN International Conference, 18.-21. Okt. 2016, Porto, Portugal.

Dieses Archiv kann nicht den Volltext zur Verfügung stellen.

Kurzfassung

Combining the expertise of many institutes, an increasingly sophisticated interdisciplinary aircraft design process is being developed at DLR, using the CPACS data format (Nagel et al., 2012; Scherer and Kohlgrüber, 2014) as a means of exchanging results. Within this process, TRAFUMO (Scherer et al., 2013) (Transport Aircraft Fuselage Model), developed at the Institute of Structures and Design (DLR-BT), is currently the established tool for automatic generation and subsequent sizing of global finite element fuselage models using Ansys and the Python programming language. Recent efforts to increase tool performance and to open up the modelling chain for a wider range of finite element solvers have led to a lot of functionality being shifted from specific routines in Ansys to Python. This includes the automatic creation of global finite element models based on geometric and structural data from CPACS and the conversion of models between different codes. Taking advantage of the modular and object-oriented nature of Python, each new module has been implemented independently with a well-defined central data format in place for storing and exchanging information, thus laying the groundwork for a new all-Python model generation chain, which provides more flexibility at significantly improved runtimes. In the presented paper, the overall structure of the newly developed model generation chain will be introduced. Additionally, the development status of several key modules, such as geometry processor, finite element generator and converter will be discussed in detail, with special attention paid to the interfaces between modules.

elib-URL des Eintrags:https://elib.dlr.de/107844/
Dokumentart:Konferenzbeitrag (Vortrag)
Titel:New approaches in CPACS-based preliminary design of aircraft fuselage structures using Python
Autoren:
AutorenInstitution oder E-Mail-AdresseAutoren-ORCID-iDORCID Put Code
Walther, Jan-NiclasJan-Niclas.Walther (at) dlr.dehttps://orcid.org/0000-0001-5738-658XNICHT SPEZIFIZIERT
Petsch, MichaelMichael.Petsch (at) dlr.dehttps://orcid.org/0000-0002-2743-375XNICHT SPEZIFIZIERT
Kohlgrüber, DieterDieter.Kohlgrueber (at) dlr.dehttps://orcid.org/0000-0002-6626-0927NICHT SPEZIFIZIERT
Datum:2016
Referierte Publikation:Ja
Open Access:Nein
Gold Open Access:Nein
In SCOPUS:Nein
In ISI Web of Science:Nein
Status:veröffentlicht
Stichwörter:CPACS, preliminary aircraft design, fuselage structures, finite element model conversion, B-spline surfaces, Python
Veranstaltungstitel:6th EASN International Conference
Veranstaltungsort:Porto, Portugal
Veranstaltungsart:internationale Konferenz
Veranstaltungsdatum:18.-21. Okt. 2016
Veranstalter :EASN Association
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 - Simulation und Validierung (alt)
Standort: Stuttgart
Institute & Einrichtungen:Institut für Bauweisen und Strukturtechnologie > Strukturelle Integrität
Hinterlegt von: Walther, Jan-Niclas
Hinterlegt am:19 Dez 2016 10:52
Letzte Änderung:29 Mär 2023 00:29

Nur für Mitarbeiter des Archivs: Kontrollseite des Eintrags

Blättern
Suchen
Hilfe & Kontakt
Informationen
electronic library verwendet EPrints 3.3.12
Gestaltung Webseite und Datenbank: Copyright © Deutsches Zentrum für Luft- und Raumfahrt (DLR). Alle Rechte vorbehalten.