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Studying aeroelastic behavior of aircraft with NeoCASS.: The Danbus configuration
KTH, School of Engineering Sciences (SCI), Aeronautical and Vehicle Engineering.
2011 (English)Independent thesis Advanced level (degree of Master (One Year)), 20 credits / 30 HE creditsStudent thesis
Abstract [en]

This Master Thesis assesses the performance of NeoCASS software as a tool for structural sizing for deformable aircraft at conceptual design level. NeoCASS is a collection of Matlab modules included in CEASIOM. Some testcases (simple wing model, TCR, Danbus, Agard 445.6 wing) are computed to evaluate the aeroelastic behavior and provide additional validation on the structural models NeoCASS computes Finally, Danbus, a new conceptual design aircraft, is analyzed with the software.

Place, publisher, year, edition, pages
2011. , 85 p.
Series
Trita-AVE, ISSN 1651-7660 ; 2011:43
National Category
Engineering and Technology
Identifiers
URN: urn:nbn:se:kth:diva-39370OAI: oai:DiVA.org:kth-39370DiVA: diva2:439828
Subject / course
Aeronautical Engineering
Educational program
Master of Science in Engineering - Vehicle Engineering
Uppsok
Technology
Examiners
Available from: 2011-09-12 Created: 2011-09-09 Last updated: 2011-09-12Bibliographically approved

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CiteExportLink to record
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Citation style
  • apa
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Language
  • de-DE
  • en-GB
  • en-US
  • fi-FI
  • nn-NO
  • nn-NB
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  • Other locale
More languages
Output format
  • html
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  • asciidoc
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