|
|
Stability and controllability of the Z-143 airplane with a more powerful engine
Kochtík, Martin ; Matějů, Jiří (referee) ; Daněk, Vladimír (advisor)
The thesis deals with the calculation and evaluation of the flight characteristics of the aeroplane Z 143 with the power unit Lycoming AEIO-580-B1A. The first part of the text focuses on a general description of the aircraft, its geometric characteristics and calculation of mass and aerodynamic characteristics. In terms of flight performance there are compared the values for contemporary model and developmental aircraft with a more powerful engine. Another part of the work deals with the calculation of properties in terms of stability and manageability. In this section regards the determination of the results of the flight characteristics and their assessment of whether they comply. In the end I discuss the individual results and comment the possible recommendations on correction or improvement of these properties.
|
|
|
Mathematical model verification for flight simulator
Kminiaková, Tatiana ; Zikmund, Pavel (referee) ; Sklenář, Filip (advisor)
The diploma thesis deals with the flight test program which is necessary to obtain the required data for EASA/FAA flight simulator certification. Flight tests are focused on flight performance and characteristics. Required regulations are selected and described. To verify the simulator model and certification parameters a flight test program was created. The flight test program is composed of flight and ground tests. In the final part of the thesis, the flight test evaluation procedure is shown. Each test contains the final valuation or recommendation for simulator model modification.
|
|
|
Engine Rotax 915 for small light aircraft
Hrabovský, Matúš ; Juračka, Jaroslav (referee) ; Jebáček, Ivo (advisor)
The thesis deals with the issue of replacement of the Rotax 912 ULS engine with the Rotax 915 iSc3 B engine and its impact on flight performance, characteristics and airframe loads of the WT 9 Dynamic. For accomplish better maneuverability tail surfaces are enlarged. Both versions of airplane with different engines and tails surfaces are quantified with respect to airframe loads and flight characteristics. The output of the diploma thesis can be used for strength design of airplane structure and stress tests of the new modification of the WT 9 Dynamic aircraft.
|
|
|
Mathematical model verification for flight simulator
Kminiaková, Tatiana ; Zikmund, Pavel (referee) ; Sklenář, Filip (advisor)
The diploma thesis deals with the flight test program which is necessary to obtain the required data for EASA/FAA flight simulator certification. Flight tests are focused on flight performance and characteristics. Required regulations are selected and described. To verify the simulator model and certification parameters a flight test program was created. The flight test program is composed of flight and ground tests. In the final part of the thesis, the flight test evaluation procedure is shown. Each test contains the final valuation or recommendation for simulator model modification.
|
|
|
Engine Rotax 915 for small light aircraft
Hrabovský, Matúš ; Juračka, Jaroslav (referee) ; Jebáček, Ivo (advisor)
The thesis deals with the issue of replacement of the Rotax 912 ULS engine with the Rotax 915 iSc3 B engine and its impact on flight performance, characteristics and airframe loads of the WT 9 Dynamic. For accomplish better maneuverability tail surfaces are enlarged. Both versions of airplane with different engines and tails surfaces are quantified with respect to airframe loads and flight characteristics. The output of the diploma thesis can be used for strength design of airplane structure and stress tests of the new modification of the WT 9 Dynamic aircraft.
|
|
|
Stability and controllability of the Z-143 airplane with a more powerful engine
Kochtík, Martin ; Matějů, Jiří (referee) ; Daněk, Vladimír (advisor)
The thesis deals with the calculation and evaluation of the flight characteristics of the aeroplane Z 143 with the power unit Lycoming AEIO-580-B1A. The first part of the text focuses on a general description of the aircraft, its geometric characteristics and calculation of mass and aerodynamic characteristics. In terms of flight performance there are compared the values for contemporary model and developmental aircraft with a more powerful engine. Another part of the work deals with the calculation of properties in terms of stability and manageability. In this section regards the determination of the results of the flight characteristics and their assessment of whether they comply. In the end I discuss the individual results and comment the possible recommendations on correction or improvement of these properties.
|
guest ::
