Change search
ReferencesLink to record
Permanent link

Direct link
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
URN: urn:nbn:se:kth:diva-153225OAI: 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)1721 downloads
File information
File name FULLTEXT01.pdfFile size 2273 kBChecksum SHA-512
Type fulltextMimetype application/pdf

By organisation
School of Engineering Sciences (SCI)
Aerospace Engineering

Search outside of DiVA

GoogleGoogle Scholar
Total: 1723 downloads
The number of downloads is the sum of all downloads of full texts. It may include eg previous versions that are now no longer available

Total: 310 hits
ReferencesLink to record
Permanent link

Direct link