This master thesis shows, how can be the modified lifting line theory used for preliminary glider design an for wing loads determination. It is shown, that relatively accurate results can be obtained at less computational cost in comparison with CFD methods
Identifer | oai:union.ndltd.org:nusl.cz/oai:invenio.nusl.cz:229448 |
Date | January 2011 |
Creators | Schoř, Pavel |
Contributors | Daněk, Vladimír, 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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