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![Effect of eccentrically oblique stiffeners and temperature on the nonlinear static and dynamic response of S-FGM cylindrical panels](thumbnails/s211.jpg) |
![Internally stiffened cylindrical shell subjected to an external explosion](thumbnails/s212.jpg) |
![Elements involved in the fuselage drop test](thumbnails/s213.jpg) |
![This is the test specimen](thumbnails/s214.jpg) |
![Getting ready for the fuselage drop test](thumbnails/s215.jpg) |
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Effect of eccentrically oblique stiffeners and temperature on the nonlinear static and dynamic response of S-FGM cylindrical panels |
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Internally stiffened cylindrical shell subjected to an external explosion |
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Elements involved in the fuselage drop test |
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This is the test specimen |
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Getting ready for the fuselage drop test |
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![The fuselage section is dropped](thumbnails/s216.jpg) |
![The dropped fuselage is damaged](thumbnails/s217.jpg) |
![Axially compressed, dented, ring- and stringer-stiffened cylindrical shell](thumbnails/s218.jpg) |
![Vibrating stiffened cylindrical panel with resonators and foam](thumbnails/s219.jpg) |
![Reference design of a uniformly longitudinally compressed longitudinally stiffened plate in which the thickness of all parts is 1.27 mm](thumbnails/s220.jpg) |
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The fuselage section is dropped |
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The dropped fuselage is damaged |
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Axially compressed, dented, ring- and stringer-stiffened cylindrical shell |
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Vibrating stiffened cylindrical panel with resonators and foam |
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Reference design of a uniformly longitudinally compressed longitudinally stiffened plate in which the thickness of all parts is 1.27 mm |
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![Optimization of the longitudinally loaded and stiffened plate in which material voids and tapering of the stiffeners are permitted](thumbnails/s221.jpg) |
![Optimized design of the longitudinally loaded and stiffened plate](thumbnails/s222.jpg) |
![Modeling the effect of a stiffener fillet radius on the prediction of buckling under axial compression](thumbnails/s223.jpg) |
![Lattice cylindrical shell with elliptical cross section](thumbnails/s224.jpg) |
![Buckling of axially compressed lattice cylindrical shells with elliptical cross sections of various narrowness](thumbnails/s225.jpg) |
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Optimization of the longitudinally loaded and stiffened plate in which material voids and tapering of the stiffeners are permitted |
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Optimized design of the longitudinally loaded and stiffened plate |
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Modeling the effect of a stiffener fillet radius on the prediction of buckling under axial compression |
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Lattice cylindrical shell with elliptical cross section |
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Buckling of axially compressed lattice cylindrical shells with elliptical cross sections of various narrowness |
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