An aircraft strut made of 2024 T4 aluminum alloy has a length of 450 mm. Its ends are fixe...
An aircraft strut made of 2024 T4 aluminum alloy has a length of 450 mm. Its ends are fixed. It has a channel cross section shown in Figure P12.28. Determine the design axial load for the column based on a factor of safety of 2.0 on the tangent modulus buckling load.
FIGURE P12.28
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