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Morphing Wing Design, from Study to Flight Test
Linköping University, Department of Management and Engineering, Fluid and Mechanical Engineering Systems. Linköping University, The Institute of Technology.
Linköping University, Department of Management and Engineering, Fluid and Mechanical Engineering Systems. Linköping University, The Institute of Technology.
Linköping University, Department of Management and Engineering, Machine Design. Linköping University, The Institute of Technology.
Linköping University, Department of Management and Engineering, Fluid and Mechanical Engineering Systems. Linköping University, The Institute of Technology.
2009 (English)Conference paper, Published paper (Refereed)
Abstract [en]

Mission adaptive wing have been implement in the past, this article present an approach were wingarea reduction of at least 40% has to be achieved. The project goal is to evaluate different concept bythe uses of flying demonstrators. This was realized during a student project over a five month period.

Place, publisher, year, edition, pages
2009.
Keyword [en]
Morphing wing, conceptual design, student project
National Category
Engineering and Technology
Identifiers
URN: urn:nbn:se:liu:diva-62592ISBN: 978-1-61567-101-4 (print)OAI: oai:DiVA.org:liu-62592DiVA: diva2:373470
Conference
47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition, Orlando, Florida, Jan. 5-8, 2009
Funder
Vinnova
Available from: 2010-11-30 Created: 2010-11-30 Last updated: 2012-08-31

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http://toc.proceedings.com/05455webtoc.pdf

Authority records BETA

Jouannet, ChristopherLundström, DavidAmadori, KristianBerry, Patrick

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Citation style
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  • Other style
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Language
  • de-DE
  • en-GB
  • en-US
  • fi-FI
  • nn-NO
  • nn-NB
  • sv-SE
  • Other locale
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Output format
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  • asciidoc
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