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Summary of unconventional aircraft concepts
Nečas, David ; Šošovička, Róbert (referee) ; Lajza, Ondřej (advisor)
This bachelor´s thesis deals with civil aircrafts of unconventional conceptions, which got into serial production. The thesis will be divided according to categories of aircrafts, whereas in every category with the exception of large transport aircrafts one conventional and two unconventional aircrafts will be specified for comparing various properties. Military aircraft will be mentioned only marginally because of the representative of significant unconventional conception.
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Electrically powered plane conceptual design
Ševčík, Igor ; Sklenář, Filip (referee) ; Popela, Robert (advisor)
The master’s thesis deals with conceptual design of a new electrically powered aircraft as assignment for Evektor, s.r.o. company. In the first part of thesis there is more detailed elaboration of small aircraft statistics and their comparison. Thesis then concentrates on assigned parameters and requirements for design. Next section continues with the most important part of thesis, which is optimization of wing used for aircraft design and also analysis of its characteristics. The problematics of preliminary verification of flight performances as well as aircraft dimension design and follow-up weight analysis with consideration of power cells placement is described thereafter. A few different flight configurations is taken into consideration within weight analysis. Final part contains evaluation of optimization and design process.
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Electrically powered plane conceptual design
Ševčík, Igor ; Sklenář, Filip (referee) ; Popela, Robert (advisor)
The master’s thesis deals with conceptual design of a new electrically powered aircraft as assignment for Evektor, s.r.o. company. In the first part of thesis there is more detailed elaboration of small aircraft statistics and their comparison. Thesis then concentrates on assigned parameters and requirements for design. Next section continues with the most important part of thesis, which is optimization of wing used for aircraft design and also analysis of its characteristics. The problematics of preliminary verification of flight performances as well as aircraft dimension design and follow-up weight analysis with consideration of power cells placement is described thereafter. A few different flight configurations is taken into consideration within weight analysis. Final part contains evaluation of optimization and design process.
|
|
|
Summary of unconventional aircraft concepts
Nečas, David ; Šošovička, Róbert (referee) ; Lajza, Ondřej (advisor)
This bachelor´s thesis deals with civil aircrafts of unconventional conceptions, which got into serial production. The thesis will be divided according to categories of aircrafts, whereas in every category with the exception of large transport aircrafts one conventional and two unconventional aircrafts will be specified for comparing various properties. Military aircraft will be mentioned only marginally because of the representative of significant unconventional conception.
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