Národní úložiště šedé literatury Nalezeno 4 záznamů.  Hledání trvalo 0.00 vteřin. 
Loads calculation, stress analysis and bird strike simulation of a composite wing leading edge
Zubrytski, Raman ; Mališ, Michal (oponent) ; Symonov, Volodymyr (vedoucí práce)
This thesis deals with design of slat geometrical and material parameters of the B737-200 aircraft. In this thesis there is created design of the composite slat with respect to a given load cases including bird strike. Analytical calculations are verified by FE analysis in MSC.Nastran/Patran, MSC.Dytran software
Aircraft safety Analysis due to bird strikes
Hrotko, Patrik ; Bartoněk, Jaroslav (oponent) ; Chlebek, Jiří (vedoucí práce)
This bachelor’s thesis deals with the problems of bird strikes. It examines significant factors that contribute to the occurrence of these strikes as well as potential damage to the affected aircraft and on the flight itself. The thesis also looks at legislative documents that specify requirements for the bird strike resistance of aircraft structures. Besides this, it gives an overview of current methods that are employed to ensure biological protection of airports with the aim of reducting the risk of bird strikes and pays attention to the effectivness of these methods.
Aircraft safety Analysis due to bird strikes
Hrotko, Patrik ; Bartoněk, Jaroslav (oponent) ; Chlebek, Jiří (vedoucí práce)
This bachelor’s thesis deals with the problems of bird strikes. It examines significant factors that contribute to the occurrence of these strikes as well as potential damage to the affected aircraft and on the flight itself. The thesis also looks at legislative documents that specify requirements for the bird strike resistance of aircraft structures. Besides this, it gives an overview of current methods that are employed to ensure biological protection of airports with the aim of reducting the risk of bird strikes and pays attention to the effectivness of these methods.
Loads calculation, stress analysis and bird strike simulation of a composite wing leading edge
Zubrytski, Raman ; Mališ, Michal (oponent) ; Symonov, Volodymyr (vedoucí práce)
This thesis deals with design of slat geometrical and material parameters of the B737-200 aircraft. In this thesis there is created design of the composite slat with respect to a given load cases including bird strike. Analytical calculations are verified by FE analysis in MSC.Nastran/Patran, MSC.Dytran software

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