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Designing A Conventional Aircraft
KTH, School of Engineering Sciences (SCI).
2014 (English)Independent thesis Basic level (degree of Bachelor), 10 credits / 15 HE creditsStudent thesis
Abstract [en]

This paper is explaining the important design phases of dimensioning an unmanned conventional aircraft from scratch and will also design one according to a few chosen requirements. The design phases discussed will be all from wing dimensioning to stability and spin recovery, aircraft performance requirements and how to select a motor which overcomes these. As well as the optimal rate of climb for improved efficiency is discussed. In the end an aircraft which manages the set requirements and is stable in pitch managing spin recovery with no problem will have been dimensioned.

Place, publisher, year, edition, pages
2014. , 48 p.
National Category
Aerospace Engineering
Identifiers
URN: urn:nbn:se:kth:diva-153225OAI: oai:DiVA.org:kth-153225DiVA: diva2:752131
Educational program
Master of Science in Engineering - Vehicle Engineering
Available from: 2014-10-07 Created: 2014-10-02 Last updated: 2014-10-07Bibliographically approved

Open Access in DiVA

Arash Sonei Kandidatexam(2273 kB)1985 downloads
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File name FULLTEXT01.pdfFile size 2273 kBChecksum SHA-512
871d8b75676adf7946b4e2303242272e2072e2775055919fd30bbce0c98d69415415f8391d756d35d892779cbfec902c315e14764f14d2ae41e801a7a841b2a5
Type fulltextMimetype application/pdf

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CiteExportLink to record
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  • apa
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