Figure 11 - Strains, Forces, and Moment Arms (Pure Moment)
This corresponds to the case where the nominal axial load capacity, Pn, is equal to zero. Iterative procedure is used to determine the nominal moment capacity as follows:
Where c is the distance from the fiber of maximum compressive strain to the neutral axis. ACI 318-19 (22.2.2.4.2)
a = Depth of equivalent rectangular stress block
(Compression) ACI 318-19 (22.2.2.4.1)
Figure 12 - Cracked Column Section Properties (Pure Moment)
The area of the reinforcement in this layer is not included in the area (ab) used to compute Cc. As a result, it is NOT necessary to subtract 0.85fc’ from fs5 before computing Fs5:
The area of the reinforcement in this layer is not included in the area (ab) used to compute Cc. As a result, it is NOT necessary to subtract 0.85fc’ from fs4 before computing Fs4:
The same procedure shown above can be repeated to calculate the forces in the remaining reinforcement layers, results are summarized in the following table:
* The area of the reinforcement in this layer has been included in the area (ab) used to compute Cc. As a result, 0.85fc’ is subtracted from fs in the computation of Fs.