Moerland, Erwin und Pfeiffer, Till und Böhnke, Daniel und Jepsen, Jonas und Freund, Sebastian und Liersch, Carsten M. und Chiozzotto, Gabriel und Klein, Carsten und Scherer, Julian und Hasan, Yasim Julian und Flink, Jan (2017) On the Design of a Strut-Braced Wing Configuration in a Collaborative Design Environment. In: 17th AIAA Aviation Technology, Integration, and Operations Conference. AIAA Aviation Forum 2017 - 17th AIAA Aviation Technology, Integration, and Operations Conference, 2017-06-05 - 2017-06-09, Denver, United States of America. doi: 10.2514/6.2017-4397.
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Offizielle URL: https://arc.aiaa.org/doi/abs/10.2514/6.2017-4397
Kurzfassung
Due to its drag saving potential through application of high aspect ratio wings, the strut-braced wing configuration is considered a promising candidate as a next generation single-aisle aircraft. This potential is reflected in the results of the renowned Sugar and Albatross projects of Boeing and ONERA. In the course of DLRs project future enhanced aircraft configurations (FrEACs), a strut-braced wing configuration is examined with focus on the interaction of aerodynamics, loads, structures and aeroelastics. The present study outlines the applied design process for the strut-braced wing configuration in DLRs collaborative design environment and highlights lessons learnt from an organizational and technical point of view. It proves that the level of confidence in the design process is largely increased by effectively combining both the explicit and implicit knowledge of the heterogeneous specialists involved. The explicit knowledge is incorporated through automated execution of the specialists tools in structured simulation workflows. Implicit knowledge of the specialists is required to interpret results both in the respective disciplinary context as well as on overall aircraft design level. Applying the collaborative design process enables statements on the possible gain of strut-braced wing over conventional tube and wing configurations. The paper describes the applied collaborative design procedure, shows results concerning the physical aspects of the strut-braced wing configuration and concludes by providing lessons learnt and an outlook into the application of collaborative design.
elib-URL des Eintrags: | https://elib.dlr.de/117576/ | ||||||||||||||||||||||||||||||||||||||||||||||||
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Dokumentart: | Konferenzbeitrag (Vortrag) | ||||||||||||||||||||||||||||||||||||||||||||||||
Titel: | On the Design of a Strut-Braced Wing Configuration in a Collaborative Design Environment | ||||||||||||||||||||||||||||||||||||||||||||||||
Autoren: |
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Datum: | Juni 2017 | ||||||||||||||||||||||||||||||||||||||||||||||||
Erschienen in: | 17th AIAA Aviation Technology, Integration, and Operations Conference | ||||||||||||||||||||||||||||||||||||||||||||||||
Referierte Publikation: | Ja | ||||||||||||||||||||||||||||||||||||||||||||||||
Open Access: | Nein | ||||||||||||||||||||||||||||||||||||||||||||||||
Gold Open Access: | Nein | ||||||||||||||||||||||||||||||||||||||||||||||||
In SCOPUS: | Nein | ||||||||||||||||||||||||||||||||||||||||||||||||
In ISI Web of Science: | Nein | ||||||||||||||||||||||||||||||||||||||||||||||||
DOI: | 10.2514/6.2017-4397 | ||||||||||||||||||||||||||||||||||||||||||||||||
Status: | veröffentlicht | ||||||||||||||||||||||||||||||||||||||||||||||||
Stichwörter: | Collaborative Engineering, Multidisciplinary Design, strut-braced wing | ||||||||||||||||||||||||||||||||||||||||||||||||
Veranstaltungstitel: | AIAA Aviation Forum 2017 - 17th AIAA Aviation Technology, Integration, and Operations Conference | ||||||||||||||||||||||||||||||||||||||||||||||||
Veranstaltungsort: | Denver, United States of America | ||||||||||||||||||||||||||||||||||||||||||||||||
Veranstaltungsart: | internationale Konferenz | ||||||||||||||||||||||||||||||||||||||||||||||||
Veranstaltungsbeginn: | 5 Juni 2017 | ||||||||||||||||||||||||||||||||||||||||||||||||
Veranstaltungsende: | 9 Juni 2017 | ||||||||||||||||||||||||||||||||||||||||||||||||
Veranstalter : | American Institute of Aeronautics and Astronautics (AIAA) | ||||||||||||||||||||||||||||||||||||||||||||||||
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 - Konzepte und Integration (alt), L - Simulation und Validierung (alt), L - Flugphysik (alt), L - Strukturen und Werkstoffe (alt) | ||||||||||||||||||||||||||||||||||||||||||||||||
Standort: | Braunschweig , Göttingen , Hamburg , Köln-Porz , Stuttgart | ||||||||||||||||||||||||||||||||||||||||||||||||
Institute & Einrichtungen: | Lufttransportsysteme > Integrierter Luftfahrzeugentwurf Institut für Faserverbundleichtbau und Adaptronik > Strukturmechanik Institut für Aerodynamik und Strömungstechnik > Transportflugzeuge Institut für Aeroelastik > Lastanalyse und Entwurf Institut für Antriebstechnik > Triebwerk Institut für Bauweisen und Strukturtechnologie > Strukturelle Integrität Institut für Flugsystemtechnik > Flugdynamik und Simulation Institut für Simulations- und Softwaretechnik > Verteilte Systeme und Komponentensoftware | ||||||||||||||||||||||||||||||||||||||||||||||||
Hinterlegt von: | Moerland, Erwin | ||||||||||||||||||||||||||||||||||||||||||||||||
Hinterlegt am: | 08 Jan 2018 12:44 | ||||||||||||||||||||||||||||||||||||||||||||||||
Letzte Änderung: | 24 Apr 2024 20:21 |
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