S.K.G
Structural
- Jul 15, 2024
- 20
Hi,
I am trying to design a scaffolding system that uses aluminum beams. I have a copy of the 2005 version of the aluminum design manual and in there, they specify to design a beam for bending you have to check the tension bending, compression bending, and shear bending. However, the final values for each state gives you the value in stress. For example, for tension bending I would get a final answer in units of ksi which means I cannot exactly compare it to the max moment the beam experiences due to the applied load. Would I simply multiply this value by the section modulus of the beam on the bottom (tension side) to get my moment capacity like we do for steel, and the same thing for compression bending (but use the section modulus at the top (compression side))?
I am trying to design a scaffolding system that uses aluminum beams. I have a copy of the 2005 version of the aluminum design manual and in there, they specify to design a beam for bending you have to check the tension bending, compression bending, and shear bending. However, the final values for each state gives you the value in stress. For example, for tension bending I would get a final answer in units of ksi which means I cannot exactly compare it to the max moment the beam experiences due to the applied load. Would I simply multiply this value by the section modulus of the beam on the bottom (tension side) to get my moment capacity like we do for steel, and the same thing for compression bending (but use the section modulus at the top (compression side))?