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Unsteady Aerodynamic Vortex Lattice of Moving Aircraft
KTH, School of Engineering Sciences (SCI), Aeronautical and Vehicle Engineering, Aerodynamics.
2011 (English)Independent thesis Advanced level (degree of Master (Two Years)), 20 credits / 30 HE creditsStudent thesis
Abstract [en]

It is aim of this thesis to develop a potential ow solver for unsteady aerodynamics in MATLAB environment. In order to achieve this target a vortex lattice method based has been developed. The validation of this program involves two dierent stages. Initially, it is compared with classical experiments and a well tested code. In a second step, the program is compared with wind tunnel experiments for two dierent aircraft's con gurations, classical and with canard. In the end it will be demonstrated that the present method achieves good agreement in both stages.

Place, publisher, year, edition, pages
2011. , 70 p.
Series
Trita-AVE, ISSN 1651-7660 ; 2011:74
National Category
Aerospace Engineering
Identifiers
URN: urn:nbn:se:kth:diva-48928OAI: oai:DiVA.org:kth-48928DiVA: diva2:458876
Subject / course
Aeronautical Engineering
Educational program
Master of Science - Aerospace Engineering
Uppsok
Technology
Examiners
Available from: 2011-11-24 Created: 2011-11-24 Last updated: 2011-11-24Bibliographically approved

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CiteExportLink to record
Permanent link

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Citation style
  • apa
  • harvard1
  • ieee
  • modern-language-association-8th-edition
  • vancouver
  • Other style
More styles
Language
  • de-DE
  • en-GB
  • en-US
  • fi-FI
  • nn-NO
  • nn-NB
  • sv-SE
  • Other locale
More languages
Output format
  • html
  • text
  • asciidoc
  • rtf