The object of thesis is a new full metal wing design of L-23 Super Blanik glider for L-23 NG project. Thesis includes calculation of flight envelope according to CS 22, wing load, wing design and stress analysis of important part of construction. The final part of thesis include weight estimation and comparison with existing design.
| Identifer | oai:union.ndltd.org:nusl.cz/oai:invenio.nusl.cz:232027 |
| Date | January 2015 |
| Creators | Bilík, David |
| Contributors | Urík, Tomáš, Schoř, Pavel |
| 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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