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Koncepční návrh výkonného kluzáku s pomocným elektrickým pohonem (dle EASA CS-22) / Conceptual design of high performance glider with electric propulsion (in complience with EASA CS-22)

This master's thesis is focused on conceptual design of glider with electric propulsion system following the CS-22 regulation. Statistical analysis of the glider with an auxiliary electric engine has been carried out in order to determine basic design parameters for conceptual design. Based on analytical drag polar, the flight performance parameters are calculated, in particular flight range and influence of the solar panels on the flight range. This thesis also includes preliminary design solution of accumulator placement within the wing.

Identiferoai:union.ndltd.org:nusl.cz/oai:invenio.nusl.cz:400839
Date January 2019
CreatorsHlůšek, Josef
ContributorsSklenář, Filip, Hlinka, Jiří
PublisherVysoké učení technické v Brně. Fakulta strojního inženýrství
Source SetsCzech ETDs
LanguageCzech
Detected LanguageEnglish
Typeinfo:eu-repo/semantics/masterThesis
Rightsinfo:eu-repo/semantics/restrictedAccess

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