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	Damage tolerance evaluation of L410 NG aircraft lower wing integrally stiffened panel Vlček, Dalibor ; Juračka, Jaroslav (referee) ; Augustin, Petr (advisor) Master’s thesis deals with the damage tolerance evaluation of L410 NG aircraft lower wing integrally stiffened panel including crack growth and residual strength analyses and inspection program proposal. Presented DT evaluation has been done using FE model of the wing and AFGROW software. Detailed record
	Aircraft structure Damage Tolerance analysis method aided by AFGROW software Rakovský, Kristián ; Juračka, Jaroslav (referee) ; Nágel‘, Martin (advisor) Diplomová práce se zabývá návrhem metodiky výpočtu závislého šíření trhlin ve více konstrukčních částech s využitím programu AFGROW. Prezentována metodika, která také zahrnuje stanovení zbytkové pevnosti, byla aplikována v damage tolerance analýzách vybraných míst na konstrukci křídla L 410 NG. Detailed record
	Damage tolerance analysis of wing to fuselage joint of L 410 NG airplane Duchoň, Peter ; Mališ, Michal (referee) ; Augustin, Petr (advisor) Master's thesis deals with the damage tolerance analysis of wing-to-fuselage joint of L 410 NG airplane. Thesis includes determination of the load distribution to the individual attachments of wing-to-fuselage joint, residual strength analysis and residual fatigue life analysis of the most loaded attachment lugs, calculation of fatigue crack growth curves in the attachment solids and inspection program proposal. This analysis was performed using FE model of the wing and central part of the fuselage and AFGROW software. Detailed record
	Aircraft structure Damage Tolerance analysis method aided by AFGROW software Rakovský, Kristián ; Juračka, Jaroslav (referee) ; Nágel‘, Martin (advisor) Diplomová práce se zabývá návrhem metodiky výpočtu závislého šíření trhlin ve více konstrukčních částech s využitím programu AFGROW. Prezentována metodika, která také zahrnuje stanovení zbytkové pevnosti, byla aplikována v damage tolerance analýzách vybraných míst na konstrukci křídla L 410 NG. Detailed record
	Damage tolerance analysis of wing to fuselage joint of L 410 NG airplane Duchoň, Peter ; Mališ, Michal (referee) ; Augustin, Petr (advisor) Master's thesis deals with the damage tolerance analysis of wing-to-fuselage joint of L 410 NG airplane. Thesis includes determination of the load distribution to the individual attachments of wing-to-fuselage joint, residual strength analysis and residual fatigue life analysis of the most loaded attachment lugs, calculation of fatigue crack growth curves in the attachment solids and inspection program proposal. This analysis was performed using FE model of the wing and central part of the fuselage and AFGROW software. Detailed record
	Damage tolerance evaluation of L410 NG aircraft lower wing integrally stiffened panel Vlček, Dalibor ; Juračka, Jaroslav (referee) ; Augustin, Petr (advisor) Master’s thesis deals with the damage tolerance evaluation of L410 NG aircraft lower wing integrally stiffened panel including crack growth and residual strength analyses and inspection program proposal. Presented DT evaluation has been done using FE model of the wing and AFGROW software. Detailed record

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