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| Buckling and post-buckling deformations from test and ABAQUS finite element model at the 4 points, A,B,C,D, indicated in the previous image |
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| Buckling of axially compessed cracked composite cylindrical shell as a function of layup angle, θ |
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| Buckling modes of axially compressed composite cylinders depend on the ply layup angle, θ |
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| Leibniz Universitat Hannover, Institut fur Static und Dynamik (ISD): Stability and Probabilistic Design of Composite Structures |
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| Shell buckling test facility at DLR in Braunschweig, Germany |
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| Axially compressed laminated composite cylindrical shell |
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| Axial Compression - End Shortening curves for buckling and postbuckling of a uniformly axially compressed thin laminated composite cylindrical shell |
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| Schematic of load-deflection curves for flat and curved unstiffened panels |
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| "Classical" buckling stress of a thin, monocoque, isotropic, perfect, elastic, uniformly axially compressed plate |
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| Postbuckling behavior of an axially compressed unstiffened rectangular plate |
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| Post-buckling modes for composite laminated cylindrical shells under axial compression, compression-torsion, & torsion |
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| Initial "classical" buckling modes of a near-perfect axially compressed photoelastic cylindrical shell |
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| Axisymmetrically imperfect cylindrical shell and equipment for measuring the profile of the imperfect generators |
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| Imperfection profiles measured along the generators of four axisymmetrically imperfect cylindrical shells |
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| Effect of axisymmetric imperfection amplitude and wavelength on buckling loads of axially compressed elastic cylindrical shells |
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