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Návrh zatahovacího podvozku pro letoun NG4 / The design of retractable landing gear for NG4 aircraftBartoněk, Jaroslav January 2011 (has links)
This diploma thesis describes the design of retractable landing gear for the NG-4 ultralight aircraft. Its main part consists of general principle of gear retraction, kinematics analysis, load calculation and structural analysis, material selection and means of controlling by pilot. The thesis contents marginally the typology of aircraft landing gears and their evolution.
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