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Aerodynamic characterisation of an experimental tilt-wing aircraft
KTH, School of Engineering Sciences (SCI), Aeronautical and Vehicle Engineering, Flight Dynamics.
2016 (English)Independent thesis Advanced level (degree of Master (Two Years)), 20 credits / 30 HE creditsStudent thesis
Abstract [en]

Computational analysis of experimental aircraft prior to test ights can be a valuable tool to estimate ight characteristics and determine areas of elevated caution. It can also provide feedback to software and model developers as to the accuracy of models used when the aircraft is ultimately own. This paper describes the aerodynamic analysis and characterisation of an experimental tilt-wing aircraft with a unique design. The paper covers what analysis is performed as well as results of these aircraft characterisations. Through this analysis a database le is created for use with NASA Design and Analysis of Rotorcraft (NDARC) tool.

Place, publisher, year, edition, pages
2016. , p. 11
Series
TRITA-AVE, ISSN 1651-7660 ; 2016:29
National Category
Engineering and Technology
Identifiers
URN: urn:nbn:se:kth:diva-198526OAI: oai:DiVA.org:kth-198526DiVA, id: diva2:1057237
External cooperation
NASA
Examiners
Available from: 2016-12-16 Created: 2016-12-16 Last updated: 2016-12-16Bibliographically approved

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fulltext(5027 kB)316 downloads
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CiteExportLink to record
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