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National Repository of Grey Literature 4 records found  Search took 0.01 seconds. 
Design study of composite rudder of L 410 NG aircraft
 Sokol, Filip ; Löffelmann, František (referee) ; Urík, Tomáš (advisor)
This diploma thesis describes the design of composite structures rudder NG aircraft L410 based on the present Dural-weave construction. According to FAR 23 and circulars certification process is designed composite primary structure of the aircraft. It proposes the construction of a new rudder and selected materials design of a track composite materials. Program MSC Patran is this structure developed FEM model and using Nastran software Compost and the strength check.
Detailed record
Computational analysis of high lift devices loads for L410 aircraft and its comparison to experimental data
 Florián, Martin ; Koutník, Tomáš (referee) ; Doupník, Petr (advisor)
The computational model design of a twin-engine, turbo-propeller, commuter aircraft and its two landing configuration analysis is the subject of the Master‘s thesis. The solution contents calibration part, creation of a computational mesh, global aerodynamics characteristics definition and detailed high lift devices load of L410 NG aircraft. The acquired results are compared to wind tunnel data. The comparison of accuracy and advantages of CFD is involved as well.
Detailed record
Design study of composite rudder of L 410 NG aircraft
 Sokol, Filip ; Löffelmann, František (referee) ; Urík, Tomáš (advisor)
This diploma thesis describes the design of composite structures rudder NG aircraft L410 based on the present Dural-weave construction. According to FAR 23 and circulars certification process is designed composite primary structure of the aircraft. It proposes the construction of a new rudder and selected materials design of a track composite materials. Program MSC Patran is this structure developed FEM model and using Nastran software Compost and the strength check.
Detailed record
Computational analysis of high lift devices loads for L410 aircraft and its comparison to experimental data
 Florián, Martin ; Koutník, Tomáš (referee) ; Doupník, Petr (advisor)
The computational model design of a twin-engine, turbo-propeller, commuter aircraft and its two landing configuration analysis is the subject of the Master‘s thesis. The solution contents calibration part, creation of a computational mesh, global aerodynamics characteristics definition and detailed high lift devices load of L410 NG aircraft. The acquired results are compared to wind tunnel data. The comparison of accuracy and advantages of CFD is involved as well.
Detailed record

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