Figure 4. Panel AXIAL1: Development of the buckling pattern as function of axial compression under 85 kN, 93.5 kN, and 115 kN, and after collapse at 235 kN.
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Figure 4. Panel AXIAL1: Development of the buckling pattern as function of axial compression under 85 kN, 93.5 kN, and 115 kN, and after collapse at 235 kN.
From the same paper as the previous 2 slides
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