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National Repository of Grey Literature 4 records found  Search took 0.01 seconds. 
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
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 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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