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Design and shape optimization of morphing winglet for regional jetliner
KTH, School of Engineering Sciences (SCI), Aeronautical and Vehicle Engineering.ORCID iD: 0000-0003-4991-5503
KTH, School of Engineering Sciences (SCI), Aeronautical and Vehicle Engineering.
2013 (English)In: 2013 Aviation Technology, Integration, and Operations Conference, 2013Conference paper, Published paper (Refereed)
Abstract [en]

Aerodynamic shape optimization on a 3D laminar wing with winglet at transonic speed is studied, with two parallel redesigns come out. The inviscid drag is improved and its pressure distribution has been refined. The winglet folded angle also effects the wing loading and its root bending moment.

Place, publisher, year, edition, pages
2013.
Keyword [en]
Aerodynamic shape optimization, Morphing, Root bending moment, Transonic speed, Wing loading, Aviation, Loading
National Category
Engineering and Technology
Identifiers
URN: urn:nbn:se:kth:diva-133283Scopus ID: 2-s2.0-84883662390ISBN: 978-162410225-7 (print)OAI: oai:DiVA.org:kth-133283DiVA: diva2:660981
Conference
2013 Aviation Technology, Integration, and Operations Conference; Los Angeles, CA; United States; 12 August 2013 through 14 August 2013
Note

QC 20131031

Available from: 2013-10-31 Created: 2013-10-29 Last updated: 2013-10-31Bibliographically approved

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Scopus

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Zhang, Mengmeng

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Output format
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