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Multidisciplinary Optimization of Wing Structure Using Parametric Models
Linköpings universitet, Institutionen för ekonomisk och industriell utveckling, Maskinkonstruktion. Linköpings universitet, Tekniska högskolan.
Linköpings universitet, Institutionen för ekonomisk och industriell utveckling, Fluida och mekatroniska system. Linköpings universitet, Tekniska högskolan.
Linköpings universitet, Institutionen för ekonomisk och industriell utveckling, Fluida och mekatroniska system. Linköpings universitet, Tekniska högskolan.
Linköpings universitet, Institutionen för ekonomisk och industriell utveckling, Fluida och mekatroniska system. Linköpings universitet, Tekniska högskolan.
2013 (engelsk)Konferansepaper, Publicerat paper (Annet vitenskapelig)
Abstract [en]

Aircraft design is an inherently multidisciplinary activity that requires integrating different models and tools to reach a well-balanced and optimized product. At Linköping University a design framework is being developed to support the initial design space exploration and the conceptual design phase. Main characteristics of the framework are its flexible database in XML format, together with close integration of automated CAD and other tools, which allows the developed geometry to be directly used in the subsequent preliminary design phase. In particular, the aim of the proposed work is to test the framework by designing, optimizing and studying a transport aircraft wing with respect to aerodynamic, geometry, structural and accessability constraints. The project will provide an initial assessment of the capability of the framework, both in terms of processing speed and accuracy of the results.

sted, utgiver, år, opplag, sider
2013.
HSV kategori
Identifikatorer
URN: urn:nbn:se:liu:diva-88322DOI: 10.2514/6.2013-140ISBN: 978-1-62410-181-6 (tryckt)OAI: oai:DiVA.org:liu-88322DiVA, id: diva2:602325
Konferanse
51st AIAA Aerospace Sciences Meeting, 7-10 January 2013, Grapevine, Texas
Prosjekter
NFFP5Tilgjengelig fra: 2013-01-31 Laget: 2013-01-31 Sist oppdatert: 2014-12-04bibliografisk kontrollert

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