Structural analysis of aircraft fuselage section and determination of boundary conditions and fatigue spectrum loading of its curved stiffened panels

• Κύριος συγγραφέας: Κορδάς, Παναγιώτης
• Άλλοι συγγραφείς: Kordas, Panagiotis
• Γλώσσα: English
• Έκδοση: 2022
• Θέματα: Stiffened panel; Test-rigs; Virtual modeling; Fatigue spectrum; Ενισχυμένο κέλυφος; Δοκιμαστική διάταξη; Εικονικό μοντέλο; Φάσμα κόπωσης

The primary objective of this thesis is the determination of the optimum experimental configurations for the experimental investigation of curved stiffened panels behavior. A test rig of this type should be capable of simulating the structural response of aircraft fuselage sections under static and...