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Posouzení letových vlastností a zatížení malého sportovního letounu po modifikaci pohonné jednotky / Engine Rotax 915 for small light aircraft

The thesis deals with the issue of replacement of the Rotax 912 ULS engine with the Rotax 915 iSc3 B engine and its impact on flight performance, characteristics and airframe loads of the WT 9 Dynamic. For accomplish better maneuverability tail surfaces are enlarged. Both versions of airplane with different engines and tails surfaces are quantified with respect to airframe loads and flight characteristics. The output of the diploma thesis can be used for strength design of airplane structure and stress tests of the new modification of the WT 9 Dynamic aircraft.

Identiferoai:union.ndltd.org:nusl.cz/oai:invenio.nusl.cz:417471
Date January 2020
CreatorsHrabovský, Matúš
ContributorsJuračka, Jaroslav, Jebáček, Ivo
PublisherVysoké učení technické v Brně. Fakulta strojního inženýrství
Source SetsCzech ETDs
LanguageSlovak
Detected LanguageEnglish
Typeinfo:eu-repo/semantics/masterThesis
Rightsinfo:eu-repo/semantics/restrictedAccess

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