5. Bar Stress Near Tension Face Equal to εy + 0.003

11 Bar Stresss Near Tension Face Equal to ey+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.

For Concrete:



    ACI 318-19 (Table 21.2.2)

    ACI 318-19 (22.2.2.1)


Where c is the distance from the fiber of maximum compressive strain to the neutral axis.    ACI 318-19 (22.2.2.4.2)

    ACI 318-19 (22.2.2.4.1)

Where:

a = Depth of equivalent rectangular stress block

    ACI 318-19 (Table 22.2.2.4.3)

(Compression)    ACI 318-19 (22.2.2.4.1)

Where:






12 Section

Figure 10 - Cracked Column Section Properties (εs = 0.00507 in./in.)

For Reinforcement:



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:

(Tension)



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:

(Tension)

The same procedure shown above can be repeated to calculate the forces in the remaining reinforcement layers, results are summarized in the following table:

Table 5 - Strains and internal force resultants (fs = fy)

Layer

d, in

ε, in./in.

fs, psi

Fs, kip

Cc, kip

Moment arm (r), in.

Moment, kip-ft

Concrete

---

0.00300

---

---

273.24

6.95

158.36

1

2.64

0.00178

51492

60.00*

---

7.37

36.82

2

4.79

0.00077

22423

46.16*

---

5.21

20.03

3

10.00

-0.00165

-47754

-121.29

---

0.00

0.00

4

15.21

-0.00407

-60000

-152.40

---

-5.21

66.14

5

17.37

-0.00507

-60000

-76.20

---

-7.37

46.77

Axial Force and Bending Moment

Pn, kip

29.50

Mn, kip-ft

328.13

ϕPn, kip

26.55

ϕMn, kip-ft

295.31

* 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.


Where:


(+) = Compression

(-) = Tension





(+) = Counter Clockwise

(-) = Clockwise