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Bird-Like Wing Conguration for Pitch Control of a Tailless Aircraft
Linköpings universitet, Institutionen för ekonomisk och industriell utveckling, Mekanisk värmeteori och strömningslära. Linköpings universitet, Tekniska högskolan.
Linköpings universitet, Institutionen för ekonomisk och industriell utveckling, Mekanisk värmeteori och strömningslära. Linköpings universitet, Tekniska högskolan.
Linköpings universitet, Institutionen för ekonomisk och industriell utveckling, Mekanisk värmeteori och strömningslära. Linköpings universitet, Tekniska högskolan.ORCID-id: 0000-0001-5526-2399
2012 (engelsk)Konferansepaper, Publicerat paper (Annet vitenskapelig)
Abstract [en]

A numerical study of a small bird-like aircraft has been performed. The aim of the study was to investigate how a swing wing (actualized through a constant span morphing wing) can be used for pitch control of a tailless aircraft. The results show that a swing wing can be successfully used, and that the aircraft can be maintained in a trimmed state by only small adjustments of part of the wing. A comparison was also made with a Vortex lattice method, but these results significantly deviated from those obtained with CFD. Copyright © 2012 by the American Institute of Aeronautics and Astronautics, Inc.

sted, utgiver, år, opplag, sider
2012.
Emneord [en]
Aerodynamics, Conceptual design, CFD
HSV kategori
Identifikatorer
URN: urn:nbn:se:liu:diva-75568DOI: 10.2514/6.2012-248OAI: oai:DiVA.org:liu-75568DiVA, id: diva2:508298
Konferanse
50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
Tilgjengelig fra: 2012-03-08 Laget: 2012-03-08 Sist oppdatert: 2016-03-14

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