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Conceptual study of very light twin jet aircraft
Smýkal, Michal ; Zikmund, Pavel (oponent) ; Urík, Tomáš (vedoucí práce)
The topic of the thesis is a conceptual study of very light twin jet aircraft. The comparison of present aircrafts is made, as well as their engines, and description of proposed solution, aircraft mass analysis, basic aerostatic calculations, flight and gust envelope, development costs and basic design of main parts of the aircraft.
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ALTERNATIVE PROPULSION FOR AIRCRAFT OF GENERAL AVIATION CATEGORY
Kaddour, Mirvat ; Hlinka, Jiří (oponent) ; Rousek, Miroslav (oponent) ; Třetina, Karel (vedoucí práce)
Air transport as all other transport contributes in producing emissions greenhouse gases, which is the main reason of climate changes. The doctoral thesis is focusing on possibility of using alternative energy source (fuel, motor) in aviation in order to reduce emission produced by aircraft. The area that has been working on is general aviation in particular aircraft of categories LSA and VLA. Three options, alternative source of energy, will be discussed. First is using LPG fuel, another is electric motors, and last adding catalytic converter to the exhaust system. For each of them will be mentioned there advantages and disadvantage, the main change in aircraft propulsion or exhaust system, and the different in aircraft performance due to these changes.
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ALTERNATIVE PROPULSION FOR AIRCRAFT OF GENERAL AVIATION CATEGORY
Kaddour, Mirvat ; Hlinka, Jiří (oponent) ; Rousek, Miroslav (oponent) ; Třetina, Karel (vedoucí práce)
Air transport as all other transport contributes in producing emissions greenhouse gases, which is the main reason of climate changes. The doctoral thesis is focusing on possibility of using alternative energy source (fuel, motor) in aviation in order to reduce emission produced by aircraft. The area that has been working on is general aviation in particular aircraft of categories LSA and VLA. Three options, alternative source of energy, will be discussed. First is using LPG fuel, another is electric motors, and last adding catalytic converter to the exhaust system. For each of them will be mentioned there advantages and disadvantage, the main change in aircraft propulsion or exhaust system, and the different in aircraft performance due to these changes.
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Conceptual study of very light twin jet aircraft
Smýkal, Michal ; Zikmund, Pavel (oponent) ; Urík, Tomáš (vedoucí práce)
The topic of the thesis is a conceptual study of very light twin jet aircraft. The comparison of present aircrafts is made, as well as their engines, and description of proposed solution, aircraft mass analysis, basic aerostatic calculations, flight and gust envelope, development costs and basic design of main parts of the aircraft.
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