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Aerodynamická analýza a návrh úprav podvozkové gondoly letounu L 410 NG / Aerodynamic analysis and design modifications of L 410 NG aircraft landing gear nacelle

This diploma thesis deals with the flow analysis around the landing gear nacelle of L 410 and with its following aerodynamical optimalization. In the first part the calibration is performed on the known geometry which was tested in wind tunnel. The following parts contain own design of the optimal geometry, design of the computional mesh with its numerical solution and results evaluation.

Identiferoai:union.ndltd.org:nusl.cz/oai:invenio.nusl.cz:230743
Date January 2013
CreatorsPukl, Marek
ContributorsHradil, Jiří, Popela, Robert
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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