5. Bar Stress Near Tension Face Equal to εy + 0.003
Figure 9 - Strains, Forces, and Moment Arms (εs = 0.00507 in./in.)
In ACI 318-19 provisions, this control point corresponds to the tension-controlled strain limit of ɛy + 0.003 (used to be 0.005 in ACI 318-14). It is the strain at the tensile limit of the transition zone for ϕ, used to define a tension-controlled section.
Additional resources concerning code provision changes in ACI 318-19 can be found in “ACI 318-19 Code Revisions Impact on StructurePoint Software” technical article.
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 10 - Cracked Column Section Properties (εs = 0.00507 in./in.)
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.