This diploma thesis describes the design of winglets for LS-3 glider. The method for determination of main winglet parameters based on selected criterion is presented as well as comparation of performace of original wing and final modification. It also includes analysis of wing loading and resetting of speed and weight limits for flying with winglets.
Identifer | oai:union.ndltd.org:nusl.cz/oai:invenio.nusl.cz:229455 |
Date | January 2011 |
Creators | Koutník, Tomáš |
Contributors | Šošovička, Róbert, Popela, Robert |
Publisher | Vysoké učení technické v Brně. Fakulta strojního inženýrství |
Source Sets | Czech ETDs |
Language | Czech |
Detected Language | English |
Type | info:eu-repo/semantics/masterThesis |
Rights | info:eu-repo/semantics/restrictedAccess |
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