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Winglet Effect on Induced Drag for a Cessna 172 Wing
KTH, School of Engineering Sciences (SCI).
KTH, School of Engineering Sciences (SCI).
KTH, School of Engineering Sciences (SCI).
2014 (English)Independent thesis Basic level (degree of Bachelor), 10 credits / 15 HE creditsStudent thesis
Abstract [en]

The perfect wing is a dream that many airplane manufactures have been striving to achieve since the beginning of the airplane. The goals are usually the same for everyone;

- Increase lift

- Reduce drag

- Minimize weight

A combination of these goals lead to a decrease in fuel consumption, which in turn reduces pollution in our atmosphere with the added bonus of an increase in economic revenue. One way to improve performance is to modify the tip of the wing structure, which has become a common sight on today’s airplanes. With the help of computational programs, the effects on drag due to wingtip devices can be previewed.

Place, publisher, year, edition, pages
2014. , 37 p.
National Category
Aerospace Engineering
Identifiers
URN: urn:nbn:se:kth:diva-152908OAI: oai:DiVA.org:kth-152908DiVA: diva2:751994
Educational program
Master of Science in Engineering - Vehicle Engineering
Available from: 2014-10-02 Created: 2014-10-02 Last updated: 2014-10-07Bibliographically approved

Open Access in DiVA

Alexander Schumacher & Erik Sjögren & Tobias Persson kandidatexam(1727 kB)3286 downloads
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File name FULLTEXT01.pdfFile size 1727 kBChecksum SHA-512
cbe85338f836855512f711cc2b24ee15029bb3552a2f003db292d88a233325f2b150878f9f5bddddea28e9e008ca2ad56e97cd9c35421e4d8de60e83e1bf867c
Type fulltextMimetype application/pdf

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CiteExportLink to record
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Citation style
  • apa
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  • Other locale
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