Structural analysis of aircraft fuselage section and determination of boundary conditions and fatigue spectrum loading of its curved stiffened panels
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...
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| Γλώσσα: | English |
| Έκδοση: |
2022
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| Διαθέσιμο Online: | http://hdl.handle.net/10889/15959 |
