National Repository of Grey Literature 8 records found  Search took 0.01 seconds. 
HPH 2 Twin Shark glider loading calculation
Pělucha, Jiří ; Jebáček, Ivo (referee) ; Juračka, Jaroslav (advisor)
The object of diploma thesis is a loading determination for strength calculation of HPH 2 Twin Shark glider matching the requirements of Certification Specification for Sailplanes (CS-22). Loading of the wing, tail section, fuselage and undercarriage is determined in this work.
Competition Aircraft Model Tail Design
Hub, Pavel ; Šurkala, Martin (referee) ; Matějů, Jiří (advisor)
This bachelor’s thesis deals with an empennage design for a new competition aircraft. The introduction gives an overview of the Air Cargo Challenge 2019 competition and conceptual layout of the aircraft. The research part of the thesis is focused on possible tail configurations, tail parameters and a statistical analysis of commercially made aircrafts. The most suitable configurations are then compared in detail, during which basic longitudinal stability calculations are done. In the last part, load is calculated, followed by structural design and bearing components sizing.
Structural design of fuselage and tail for racing model
Skála, Adam ; Hájek, Tomáš (referee) ; Pejchar, Jan (advisor)
This bachelor’s thesis surveys fuselage and empennage improvement of an already existing competition aircraft FabricK. Firstly, the introductory part explains the Air Cargo Challenge contest and describes the model. A research then presents possible empennage designs, which is followed by a brief overview of production F3B aircraft. The practical part of thesis introduces construction project of the empennage and the fuselage as well as a weight distribution analysis. Finally, the concluding part will evaluate the imporvement.
Load Calculation and Stress Analysis of Wing and Tail Unit of Parrot Aircraft
Hemmel, Radek ; Mališ, Michal (referee) ; Jebáček, Ivo (advisor)
Load calculation wing, aileron, flaps, tail unit of Parrot Aircraft according to specification ASTM F 2245-04. Stress analysis coat, stem, flange, rivet and point.
Competition Aircraft Model Tail Design
Hub, Pavel ; Šurkala, Martin (referee) ; Matějů, Jiří (advisor)
This bachelor’s thesis deals with an empennage design for a new competition aircraft. The introduction gives an overview of the Air Cargo Challenge 2019 competition and conceptual layout of the aircraft. The research part of the thesis is focused on possible tail configurations, tail parameters and a statistical analysis of commercially made aircrafts. The most suitable configurations are then compared in detail, during which basic longitudinal stability calculations are done. In the last part, load is calculated, followed by structural design and bearing components sizing.
Structural design of fuselage and tail for racing model
Skála, Adam ; Hájek, Tomáš (referee) ; Pejchar, Jan (advisor)
This bachelor’s thesis surveys fuselage and empennage improvement of an already existing competition aircraft FabricK. Firstly, the introductory part explains the Air Cargo Challenge contest and describes the model. A research then presents possible empennage designs, which is followed by a brief overview of production F3B aircraft. The practical part of thesis introduces construction project of the empennage and the fuselage as well as a weight distribution analysis. Finally, the concluding part will evaluate the imporvement.
HPH 2 Twin Shark glider loading calculation
Pělucha, Jiří ; Jebáček, Ivo (referee) ; Juračka, Jaroslav (advisor)
The object of diploma thesis is a loading determination for strength calculation of HPH 2 Twin Shark glider matching the requirements of Certification Specification for Sailplanes (CS-22). Loading of the wing, tail section, fuselage and undercarriage is determined in this work.
Load Calculation and Stress Analysis of Wing and Tail Unit of Parrot Aircraft
Hemmel, Radek ; Mališ, Michal (referee) ; Jebáček, Ivo (advisor)
Load calculation wing, aileron, flaps, tail unit of Parrot Aircraft according to specification ASTM F 2245-04. Stress analysis coat, stem, flange, rivet and point.

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