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Bird-Like Wing Conguration for Pitch Control of a Tailless Aircraft
Linköping University, Department of Management and Engineering, Applied Thermodynamics and Fluid Mechanics. Linköping University, The Institute of Technology.
Linköping University, Department of Management and Engineering, Applied Thermodynamics and Fluid Mechanics. Linköping University, The Institute of Technology.
Linköping University, Department of Management and Engineering, Applied Thermodynamics and Fluid Mechanics. Linköping University, The Institute of Technology.ORCID iD: 0000-0001-5526-2399
2012 (English)Conference paper, Published paper (Other academic)
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.

Place, publisher, year, edition, pages
2012.
Keyword [en]
Aerodynamics, Conceptual design, CFD
National Category
Aerospace Engineering
Identifiers
URN: urn:nbn:se:liu:diva-75568DOI: 10.2514/6.2012-248OAI: oai:DiVA.org:liu-75568DiVA: diva2:508298
Conference
50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
Available from: 2012-03-08 Created: 2012-03-08 Last updated: 2016-03-14

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Bradley, AndreasGårdhagen, RolandKarlsson, Matts

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