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Výpočet zatížení vztlakových klapek letounu L410NG a porovnání s letovým měřením / Computational analysis of high lift devices loads for L410 aircraft and its comparison to experimental data

The computational model design of a twin-engine, turbo-propeller, commuter aircraft and its two landing configuration analysis is the subject of the Master‘s thesis. The solution contents calibration part, creation of a computational mesh, global aerodynamics characteristics definition and detailed high lift devices load of L410 NG aircraft. The acquired results are compared to wind tunnel data. The comparison of accuracy and advantages of CFD is involved as well.

Identiferoai:union.ndltd.org:nusl.cz/oai:invenio.nusl.cz:232015
Date January 2015
CreatorsFlorián, Martin
ContributorsKoutník, Tomáš, Doupník, Petr
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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