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	Conceptual design of air- mobil Podhorský, Matěj ; Zikmund, Pavel (referee) ; Píštěk, Antonín (advisor) The topic of the thesis is a conceptual design of a roadable aircraft. The comparison of existing concepts is made, as well as description of proposed solution, aircraft mass analysis, basic aerostatic calculations, flight and gust envelope calculation and a design of truss construction of the fuselage. The CS-VLA, alternatively ELSA-K, has been used as a certification base. The compliance to this certification specification is one of the goals of this thesis. Detailed record
	Conceptual study of very light twin jet aircraft Smýkal, Michal ; Zikmund, Pavel (referee) ; Urík, Tomáš (advisor) Tématem diplomové práce je koncepční studie lehkého dvoumotorového letounu. Je provedeno srovnání současných letounů, jejich motorů, technický popis navrhovaného řešení, hmotový rozbor, výpočet aerostatických podkladů, výpočet obálky zatížení, nákladů na vývoj a základní konstrukce hlavních součástí. Detailed record
	The design of a twin-engined airplane in the commuter category according to CS-23 regulation Dula, Jan ; Jebáček, Ivo (referee) ; Vaněk, František (advisor) This work's objective is to create a type design of a new commuter class airplane according to CS-23 certification specifications. The design will take under account the EV-55 design to reduce the number of new parts and subassemblies. Part of this thesis are mass balance of the new design, basic airplane dimensions and fuselage dimensions estimates. The critical crossection of the fuselage is analyzed (stress analysis) and the system drawings is worked out. Detailed record
	Design of VUT 081 Kondor aeroplane in double-fuselage variant Suk, Filip ; Vaněk, František (referee) ; Píštěk, Antonín (advisor) The aim of the diploma thesis is to determine loads of the empennages and the engine mount for the engine ROTAX 912iS of the VUT 081 Kondor aircraft. Further the thesis deals with a design of a stabilizer and of beams of empennage with fins. I also present a design of mountings for beams to the center wing box. The design is presented with regard to CS-VLA regulations and the ELSA regulation for modular construction. Detailed record
	Conceptual study of very light twin jet aircraft Smýkal, Michal ; Zikmund, Pavel (referee) ; Urík, Tomáš (advisor) Tématem diplomové práce je koncepční studie lehkého dvoumotorového letounu. Je provedeno srovnání současných letounů, jejich motorů, technický popis navrhovaného řešení, hmotový rozbor, výpočet aerostatických podkladů, výpočet obálky zatížení, nákladů na vývoj a základní konstrukce hlavních součástí. Detailed record
	Conceptual design of air- mobil Podhorský, Matěj ; Zikmund, Pavel (referee) ; Píštěk, Antonín (advisor) The topic of the thesis is a conceptual design of a roadable aircraft. The comparison of existing concepts is made, as well as description of proposed solution, aircraft mass analysis, basic aerostatic calculations, flight and gust envelope calculation and a design of truss construction of the fuselage. The CS-VLA, alternatively ELSA-K, has been used as a certification base. The compliance to this certification specification is one of the goals of this thesis. Detailed record
	Design of VUT 081 Kondor aeroplane in double-fuselage variant Suk, Filip ; Vaněk, František (referee) ; Píštěk, Antonín (advisor) The aim of the diploma thesis is to determine loads of the empennages and the engine mount for the engine ROTAX 912iS of the VUT 081 Kondor aircraft. Further the thesis deals with a design of a stabilizer and of beams of empennage with fins. I also present a design of mountings for beams to the center wing box. The design is presented with regard to CS-VLA regulations and the ELSA regulation for modular construction. Detailed record
	The design of a twin-engined airplane in the commuter category according to CS-23 regulation Dula, Jan ; Jebáček, Ivo (referee) ; Vaněk, František (advisor) This work's objective is to create a type design of a new commuter class airplane according to CS-23 certification specifications. The design will take under account the EV-55 design to reduce the number of new parts and subassemblies. Part of this thesis are mass balance of the new design, basic airplane dimensions and fuselage dimensions estimates. The critical crossection of the fuselage is analyzed (stress analysis) and the system drawings is worked out. Detailed record

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